History and Overview of Rotating Wing Aircraft

Size: px
Start display at page:

Download "History and Overview of Rotating Wing Aircraft"

Transcription

1 History and Overview of Rotating Wing Aircraft Produced by the American Helicopter Society (AHS) International STEM Committee: Free to distribute with attribution Photo by Paolo Rosa

2 History of Rotorcraft Definition of Rotorcraft Any flying machine using rotating wings to provide lift, propulsion, and control that enable vertical flight and hover Rotating wings provide propulsion, but negligible lift and control. Rotating wings provide lift, propulsion, control at same time.

3 History of Rotorcraft Two key configurations developed in parallel Autogiro Close to helicopter, uses many of same mechanical feature Cannot hover Unpowered rotor Helicopter Powered rotor Many configurations have been developed Autogiros flew first! Autogiro innovations enabled development of first helicopters

4 Autogyro How it Works Unpowered Rotor that Spins Due to Wind Blowing Through Rotor Like a Wind Turbine No Need for Anti-Torque Since Not Driven By an Engine Fixed to the Fuselage Lift Relative Wind Thrust Control Surfaces

5 Autogyro How it Works Kind of like parasailing, except rotor provides lift in addition to drag.

6 Helicopter How it Works Powered Rotor Equal and opposite torque applied to rotor acts on fuselage Main Rotor Drive Shaft Rotor Thrust Tail Rotor Thrust Cockpit Tail Boom Landing Skids Engine, Fuel, Transmission, etc. Tail Rotor Controls

7 Helicopter Need for Anti-Torque Engine fixed on body exerts torque on rotor shaft Rotor shaft exerts equal and opposite torque on body Many configurations created around anti-torque problem Autogyros, tip jets, tip propellers, tandem helicopters, tilt wings, tilt rotors, synchcopter -T T

8 Basic Rotor Controls Pitch Bearing Flap and Lag Hinges Pitch Link Rotor Control Servos Swashplate Red = Rotating Blue = Fixed

9 Basic Rotor Controls Cyclic control Changes pitch sinusoidally of all blades around azimuth angle (blade rotation angle) Accomplished by tilting swashplate side to side on gimbal Collective Control Increases/decreases pitch on all blades at all azimuthal locations Accomplished by moving swashplate up and down rotor shaft Blade azimuth angle ψ

10 Key Problems in Early Rotorcraft Development Understanding basic aerodynamics of vertical flight Amount of power to produce fixed amount of lift was unknown First significant application of aerodynamic theory to helicopter rotors came about in the early 1920s Lack of a suitable engine Not until the mid-1920s that engines with sufficient power and with high power to weight ratios suitable for vertical flight became widely available Minimizing weight Early engines made of case iron too heavy! Aluminum not cheap enough for use on aircraft until 1920

11 Key Problems in Early Rotorcraft Development Counteracting rotor torque reaction Tail rotor to counter torque reaction and provide directional control not used on most early designs Igor Sikorsky was the first to successfully use the tail rotor in the single rotor helicopter configuration we know today. Providing stability and control Primary concern was to devise a means of defeating the unequal lift produced on the blades advancing into and retreating from the relative wind when in forward flight Problems overcome only with articulated rotor and cyclic pitch control Conquering high vibrations Vibration was source of many mechanical failures of the rotor and airframe Reflected an insufficient understanding of the dynamic and aerodynamic behavior of rotating-wings

12 History of Rotorcraft

13 Early Concepts Chinese Top 400 B.C.

14 Early Concepts DaVinci Leonardo da Vinci credited with first idea for vertical flight Oversized Archimedes water screw Airscrew consisted of platform with metal helical screw Propellers made of starched linen, frame made of wire Just a sketch

15 Enabling Devices Lomonosov Russian, Mikhail V. Lomonosov Very first self-propelled model of a lifting airscrew flown Coaxial rotor system, spring-driven device Flown freely and climbed to good altitude Intended for lifting thermometers and other instruments into the air

16 Enabling Devices Phillips 1840 s, D Amecourt 1860 s Horatio Phillips, 1840 s Constructed first steam driven vertical flight machine Steam generated by mini-boiler ejected at blade tips First time rotorcraft flew under engine power Ponton D Amecourt, 1860 s Also designed, built, and flew a a number of small steam powered helicopter models Coaxial rotors Pictured on right

17 Enabling Devices Bright Henry Bright, Englishman First helicopter patent granted by the British Patent Office Two counter-rotating coaxial two-bladed rotors Mounted on a vertical shaft

18 Enabling Devices Achenbach Wilheim Achenbach, German Single rotor concept First side thrusting tail rotor to counteract main rotor torque

19 Enabling Devices Forlanini Enrico Forlanini, Italian Steam driven helicopter model, dual counter-rotating propellers Forced superheated steam to a high pressure in a small metal sphere Flew 40 ft for 20 sec

20 Early Contraptions Cornu Paul Cornu, French Bicycle Maker Vertical flight machine carried human off ground for the first time Dual rotor, 24 HP gas engine, belt-driven

21 Early Contraptions Breguet Louis and Jacques Breguet, French Scientists Quad-Rotor gyroplane, 40-hp engine, Briefly carried a pilot off the ground

22 Early Contraptions Sikorsky Igor Sikorsky, Russian Prototype coaxial nonpiloted helicopter Did not fly due to vibration problems and lack of power

23 Early Contraptions Yurev B.N. Yuriev, Russian Developed single main rotor helicopter Included collective pitch, cyclic pitch, and tail rotor Aircraft never flew properly due to lack of power

24 Early Contraptions Ellehammer Jacob Ellehammer, Danish Coaxial rotor helicopter Short blades attached to 2 large circular aluminum rings Top ring like a parachute for failures Aircraft made short hops off the ground

25 Early Contraptions Petroczy 1920 Stephan Petroczy, Austrian, assisted by Theodore Von Karman Build and flew coaxial rotor helicopter Pilot-Observer positioned over the rotors, inflated bags for landing gear Powered by 3 rotary engines Machine only flew tethered to ground

26 Early Contraptions Berliner 1909 to 1920 Emile and Henry Berliner, father and son from United States Developed coaxial and side-by-side rotor helicopters First to observe power required decreases when entering forward flight Side-by-side aircraft: twisted rotor blades Side-by-side aircraft control: Differential shaft tilt, wings in slipstream

27 Early Contraptions Brennan 1920 Louis Brennan, English Single 2 bladed rotor ( needed Rotor driven by propellers on blade tips (no anti-torque Control achieved with servo flaps inboard on rotor Machine flew successfully inside a balloon shed, crashed on Flight 7

28 Early Contraptions Pescara 1920 s Raul Pescara, Argentinan working in spain and france Coaxial helicopter with biplane-type rotors First to use cyclic blade pitch Aircraft achieved short uncontrolled flights

29 Early Contraptions Von Baumhauer 1924 A.G. Von Baumhauer, Dutch Single main rotor helicopter Collective pitch, cyclic pitch See-saw teetering rotor Main and tail rotors not connected difficult directional control Machine made several short semi-controlled hops off ground

30 Autogyro First Flight Juan de la Cierva, Spaniard Hinged Blades, standard fixed wing aircraft controls in rotor slipstream Low speed control difficult, lack of dynamic pressure Required about a 50 ft ground run

31 Autogyro Cyclic Pitch E. Burke Wilford, American First rigid rotor to fly First to use cyclic blade pitch

32 Autogyro Direct Control Juan de la Cierva, Britain Rotor mounted so shaft can be tilted for control Led to elimination of ailerons and stub wings.

33 Autogyro Coming Back Jay Carter, United States Personal Air Vehicle 2-bladed rotor, pusher propeller, tip weights on blades for jump take-off Rotor slowed in forward flight for reduced drag

34 Early Helicopters Bothezat 1922 Georges de Bothezat, United States Quad-rotor, 6 bladed rotors Controlled by collective, differential collective, and cyclic pitch Called the Flying Octopus Flew many times successfully at low altitude and low speed

35 Early Helicopters Oemichen 1924 Etienne Oemichen, French Quad-rotor Helicopter Won FAI award for the first helicopter to fly a 1 km standard circuit Stable and somewhat maneuverable machine

36 Early Helicopters d Ascanio 1930 Corradino d Ascanio, Italy Built and flew successful coaxial helicopter Two bladed rotors, flapping hinges, collective and cyclic pitch Servo tab control on blades Small propellers on fuselage used for additional pitch control

37 Early Helicopters Bleeker 1930 Maitland Bleeker, United States 4-Bladed single rotor helicopter Followed work of Brennan, rotor powered By props on blade tips Servo tab control on blades

38 Early Helicopters Florine 1933 Nicolas Florine, Belgium Built and flew one of the first tandem rotor helicopters Rotors spun in same direction, but tilted differentially for anti-torque Flew for 9 minutes to an altitude of 15 ft

39 Early Helicopters Focke 1936 Henrich Focke, German Built and flew successful side-by-side rotor helicopter Three bladed rotors, flap and lag hinges Longitudinal control via swashplate on rotors Lateral control via differential collective on rotors First helicopter to demonstrate autorotation

40 Early Helicopters Weir Company 1938 Weir Company, Scotland Side-by-Side rotor helicopter Cyclic pitch on blades No collective pitch, altitude controlled by rotor RPM Small propellers on fuselage used for additional pitch control

41 Early Helicopters Flettner 1939 Antoine Flettner, German First synchcopter helicopter First to show autorotation and return to powered flight

42 Early Helicopters Sikorsky 1940 Igor Sikorsky, United States Successful single main rotor helicopter Flapping hinges and cyclic pitch Original machine had 3 small tail rotors, later reduced to one Considered the first practical helicopter

43 Rotorcraft Configurations

44 Single Main Rotor Helicopter

45 Tandem Rotor Helcopter

46 Synchcopter

47 Tilt Wing Aircraft

48 Tilt Rotor Aircraft

49 Tip Jet Driven Rotorcraft

50 Compound Helicopter McDonnell XV 1 Tip jet driven main rotor, very noisy Pusher propellers Large wings First rotorcraft to fly to 200 mph

51 Compound Helicopter Tip jet driven main rotor, very noisy

52 Compound Helicopter

53 Compound Helicopters

54 Compound Helicopter

55 Compound Helicopter

56 Compound Helicopter

57 Compound Helicopter

58 Compound Helicopter

59 Compound Helicopter

60 Compound Helicopter Sikorsky X2 Technology Demonstrator Achieved helicopter speed record of 252 kts (290 mph) on 15 September 2010 Retired on 14 July 2011 after 23 successful flights Led to development of S-97 Raider high-speed scout/attack helicopter

The quest of vertical flight: the development of helicopter

The quest of vertical flight: the development of helicopter The quest of vertical flight: the development of helicopter Thierry M. Faure To cite this version: Thierry M. Faure. The quest of vertical flight: the development of helicopter. Blog Sous les cocardes.

More information

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript

The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, The text included here is an approximate transcript The following slideshow and talk were presented at the Uber Elevate Summit on April 25 th, 2017. The text included here is an approximate transcript of the speech given by Jay Carter, founder and CEO of

More information

Introduction: A History of Helicopter Flight

Introduction: A History of Helicopter Flight CHAPTER 1 Introduction: A History of Helicopter Flight The idea of a vehicle that could lift itself vertically from the ground and hover motionless in the air was probably born at the same time that man

More information

A Technical Essay on the Gyroplane

A Technical Essay on the Gyroplane A Technical Essay on the Gyroplane Anand Saxena * Abstract A study of "Gyroplane" and its historical evolution, general characteristics, flight characteristics, various designs, potential applications

More information

Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics

Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics Robot Dynamics Rotary Wing UAS: Introduction, Mechanical Design and Aerodynamics 151-0851-00 V Marco Hutter, Michael Blösch, Roland Siegwart, Konrad Rudin and Thomas Stastny Robot Dynamics: Rotary Wing

More information

I!"#$%&'"#(')$*+($+$,+-.(/"-$0-!&-00#$

I!#$%&'#(')$*+($+$,+-.(/-$0-!&-00#$ Igor Sikorsky s Inventive Genius Produced 66 Patents Awarded In America. This issue is devoted to his unique conceptual designs that did not progress to production. I!"#$%&'"#(')$*+($+$,+-.(/"-$0-!&-00#$

More information

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols

Preface. Acknowledgments. List of Tables. Nomenclature: organizations. Nomenclature: acronyms. Nomenclature: main symbols. Nomenclature: Greek symbols Contents Preface Acknowledgments List of Tables Nomenclature: organizations Nomenclature: acronyms Nomenclature: main symbols Nomenclature: Greek symbols Nomenclature: subscripts/superscripts Supplements

More information

A practical investigation of the factors affecting lift produced by multi-rotor aircraft. Aaron Bonnell-Kangas

A practical investigation of the factors affecting lift produced by multi-rotor aircraft. Aaron Bonnell-Kangas A practical investigation of the factors affecting lift produced by multi-rotor aircraft Aaron Bonnell-Kangas Bonnell-Kangas i Table of Contents Introduction! 1 Research question! 1 Background! 1 Definitions!

More information

Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter)

Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter) Page-1 Gyroplane questions from Rotorcraft Commercial Bank (From Rotorcraft questions that obviously are either gyroplane or not helicopter) "X" in front of the answer indicates the likely correct answer.

More information

How Do Helicopters Fly? An Introduction to Rotor Aeromechanics

How Do Helicopters Fly? An Introduction to Rotor Aeromechanics Audience: Grades 9-10 Module duration: 75 minutes How Do Helicopters Fly? An Introduction to Rotor Aeromechanics Instructor Guide Concepts: Airfoil lift, angle of attack, rotary wing aerodynamics, hover

More information

A helicopter that flaps its wings

A helicopter that flaps its wings Further scientific news by TU Delft Colophon DO-Archive A helicopter that flaps its wings The Ornicopter flaps its wings like a bird to get into the air by Bennie Mols No other type of aircraft is as manoeuvrable

More information

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999

AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update. Presented to NIAC By Carl Grant November 9th, 1999 AN ADVANCED COUNTER-ROTATING DISK WING AIRCRAFT CONCEPT Program Update Presented to NIAC By Carl Grant November 9th, 1999 DIVERSITECH, INC. Phone: (513) 772-4447 Fax: (513) 772-4476 email: carl.grant@diversitechinc.com

More information

Product Comparison. 480B vs. Robinson R44

Product Comparison. 480B vs. Robinson R44 Product Comparison 480B vs. Robinson R44 480B vs. Robinson R44 Specifications Enstrom 480B Robinson R44 Seats 1/4 or 2/1 1/3 Continuous Engine Power (To Drivetrain) 277 shp/206 kw 205 shp/183 kw Gross

More information

XIV.C. Flight Principles Engine Inoperative

XIV.C. Flight Principles Engine Inoperative XIV.C. Flight Principles Engine Inoperative References: FAA-H-8083-3; POH/AFM Objectives The student should develop knowledge of the elements related to single engine operation. Key Elements Elements Schedule

More information

Copyrighted material Taylor & Francis Not for resale

Copyrighted material Taylor & Francis Not for resale Contents Preface Acknowledgements xi xiii Chapter 1 The earth s atmosphere 1 Atmospheric composition 1 Gases 2 Atmospheric pressure 2 Pressure measurement 2 Temperature 4 Density 4 International Standard

More information

Die Lösungen müssen manuell überpüft werden. Die Buchstaben stimmen nicht mehr überein.

Die Lösungen müssen manuell überpüft werden. Die Buchstaben stimmen nicht mehr überein. HELI Final Test 2015, Winterthur 17.06.2015 NAME: Mark the best answer. A B C D A B C D Die Lösungen müssen manuell überpüft werden. Die Buchstaben stimmen nicht mehr überein. 1 1 Principles of Flight

More information

In response to. 34th Annual AHS International Student Design Competition IIT KANPUR INDIAN INSTITUTE OF TECHNOLOGY, KANPUR

In response to. 34th Annual AHS International Student Design Competition IIT KANPUR INDIAN INSTITUTE OF TECHNOLOGY, KANPUR In response to 34th Annual AHS International Student Design Competition By 2017 VIBHRAM AIRFRAME 4-VIEW ISOMETRIC TOP FRONT SIDE HELICOPTER SYSTEMS OVERVIEW Landing Gear Light weight and high strength

More information

A short Company & Technology Overview

A short Company & Technology Overview A short Company & Technology Overview The Future of Rotary Wings Workshop Centro Alti Studi della Difesa (CASD) Rome, November 22 nd, 2012 An introduction to K4A K4A was founded in 2005 by Engineers and

More information

Development of the Autogiro: A Technical Perspective

Development of the Autogiro: A Technical Perspective JOURNAL OF AIRCRAFT Vol. 41, No. 4, July August 2004 Development of the Autogiro: A Technical Perspective J. Gordon Leishman University of Maryland, College Park, Maryland 20742 The technical challenges

More information

Revised Edition: 2016 ISBN All rights reserved.

Revised Edition: 2016 ISBN All rights reserved. Revised Edition: 2016 ISBN 978-1-280-29746-5 All rights reserved. Published by: Library Press 48 West 48 Street, Suite 1116, New York, NY 10036, United States Email: info@wtbooks.com Table of Contents

More information

INDIAN INSTITUTE OF TECHNOLOGY KANPUR

INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR INDIAN INSTITUTE OF TECHNOLOGY KANPUR Removable, Low Noise, High Speed Tip Shape Tractor Configuration, Cant angle, Low Maintainence Hingelesss, Good Manoeuverability,

More information

A FLYING EJECTION SEAT. By R. H. Hollrock* and J. J. Barzda* ABSTRACT

A FLYING EJECTION SEAT. By R. H. Hollrock* and J. J. Barzda* ABSTRACT ijt'9y%., A FLYING EJECTION SEAT By R. H. Hollrock* and J. J. Barzda* ABSTRACT To increase aircrewmen's chances for safe rescue in combat zones, the armed forces are investigating advanced escape and rescue

More information

Electric Drive - Magnetic Suspension Rotorcraft Technologies

Electric Drive - Magnetic Suspension Rotorcraft Technologies Electric Drive - Suspension Rotorcraft Technologies William Nunnally Chief Scientist SunLase, Inc. Sapulpa, OK 74066-6032 wcn.sunlase@gmail.com ABSTRACT The recent advances in electromagnetic technologies

More information

DEVELOPMENT OF THE AUTOGIRO: ATECHNICAL PERSPECTIVE

DEVELOPMENT OF THE AUTOGIRO: ATECHNICAL PERSPECTIVE DEVELOPMENT OF THE AUTOGIRO: ATECHNICAL PERSPECTIVE J. Gordon Leishman Alfred Gessow Rotorcraft Center Department of Aerospace Engineering Glenn L. Martin Institute of Technology University of Maryland

More information

American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release

American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release SIKORSKY & BOEING JMR TD UPDATE American Helicopter Society Washington, DC 20 November 2013 Approved for Public Release Vertical Lift / FVL Copyright 2010 Boeing. All rights reserved. Boeing Proprietary

More information

Introduction. Fuselage/Cockpit

Introduction. Fuselage/Cockpit Introduction The Moravan Zlin 242L is a fully aerobatic 2 seat aircraft designed to perform all advanced flight maneuvers within an envelope of -3.5 to +6 Gs. Many military and civilian flight-training

More information

Felix Du Temple de la Croix Monoplane 1857

Felix Du Temple de la Croix Monoplane 1857 2 1 Felix Du Temple de la Croix Monoplane 1857 2 Thrust for Flight 3 Unpowered airplanes George Cayle s design (early 19 th century) Samuel P Langley s Airplane (late 19 th century) 4 Langley s Airplane

More information

Clean Sky 2. LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels th December 2012 OUTLINE

Clean Sky 2. LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels th December 2012 OUTLINE Clean Sky 2 LifeCraft Demonstrationt (IADP RC 2 & ITDs) Consultation meetings Brussels 10-14 th December 2012 1 1 LifeCraft - The Compound Demo OUTLINE Presentation of the Compound R/C Concept Impact &

More information

SHIP HYDRODYNAMICS LECTURE NOTES OF PROPULSION PART

SHIP HYDRODYNAMICS LECTURE NOTES OF PROPULSION PART SHIP HYDRODYNAMICS LECTURE NOTES OF PROPULSION PART Course Outline Contents Time Date Week 1. Propulsion Systems a) History and Development of Screw Propeller b) Modern Propulsion Systems i- Fixed pitch

More information

Reducing Landing Distance

Reducing Landing Distance Reducing Landing Distance I've been wondering about thrust reversers, how many kinds are there and which are the most effective? I am having a debate as to whether airplane engines reverse, or does something

More information

Electric VTOL Aircraft

Electric VTOL Aircraft Electric VTOL Aircraft Subscale Prototyping Overview Francesco Giannini fgiannini@aurora.aero 1 08 June 8 th, 2017 Contents Intro to Aurora Motivation & approach for the full-scale vehicle Technical challenges

More information

A CFD-Based Approach to Coaxial Rotor Hover Performance Using Actuator Disks. Jonathan Chiew

A CFD-Based Approach to Coaxial Rotor Hover Performance Using Actuator Disks. Jonathan Chiew A CFD-Based Approach to Coaxial Rotor Hover Performance Using Actuator Disks Jonathan Chiew AE4699 - Spring 007 Dr. Lakshmi Sankar Georgia Institute of Technology Table of Contents Table of Contents Introduction

More information

CHAPTER 11 FLIGHT CONTROLS

CHAPTER 11 FLIGHT CONTROLS CHAPTER 11 FLIGHT CONTROLS CONTENTS INTRODUCTION -------------------------------------------------------------------------------------------- 3 GENERAL ---------------------------------------------------------------------------------------------------------------------------

More information

Innovation Takes Off

Innovation Takes Off Innovation Takes Off Clean Sky 2 Information Day Bonn, 20 February 2014 Fast Rotorcraft IADP: LifeRCraft Compound Rotorcraft Hans Barnerssoi, Airbus Helicopters Innovation Takes Off LifeRCraft 1 - The

More information

(12) Patent Application Publication (10) Pub. No.: US 2010/ A1

(12) Patent Application Publication (10) Pub. No.: US 2010/ A1 (19) United States (12) Patent Application Publication (10) Pub. No.: US 2010/0044499 A1 Dragan et al. US 20100.044499A1 (43) Pub. Date: Feb. 25, 2010 (54) (75) (73) (21) (22) SIX ROTOR HELICOPTER Inventors:

More information

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA

DIRECCION DE PERSONAL AERONAUTICO DPTO. DE INSTRUCCION PREGUNTAS Y OPCIONES POR TEMA 1 TEM: 0639 OM-RT - ircraft Systems - hap. 2 OD_PREG: PREG20098402 (5168) PREGUNT: For gyroplanes with constant-speed propellers, the first indication of carburetor icing is usually decrease in engine

More information

Prop effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession

Prop effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession Prop effects (Why we need right thrust) Torque reaction Spiraling Slipstream Asymmetric Loading of the Propeller (P-Factor) Gyroscopic Precession Propeller torque effect Influence of engine torque on aircraft

More information

Helicopter Experience, Date: August 1-6 Location: Central Connecticut State University

Helicopter Experience, Date: August 1-6 Location: Central Connecticut State University Helicopter Experience, 2010 Date: August 1-6 Location: Central Connecticut State University 1 Out Line Schedule Selection Process What students will receive 2 com For All Details 3 Sunday, August 1, 2010,

More information

Ultralight airplane Design

Ultralight airplane Design Ultralight airplane Design Ultralight airplane definitions: Airworthiness authorities define aircraft as vehicles that can rise or move in the air and enforce strict regulations and requirements for all

More information

Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018

Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018 Key Drivers for evtol Design Christopher Silva From VTOL to evtol Workshop May 24, 2018 Can we use what we already know? Techniques and processes Aircraft / System design theory: Design Thinking, MDAO,

More information

Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the

Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the Model Number : V-173 Model Name : Flying Pancake Model Type: Proof of Concept, Fighter Charles H. Zimmerman promoted his Flying Pancake design from 1933 to 1937 while working for the National Advisory

More information

Better Performance Starts with Better Technology THE BLR ADVANTAGE

Better Performance Starts with Better Technology THE BLR ADVANTAGE Better Performance Starts with Better Technology THE BLR ADVANTAGE Does it work? Ask a Pilot. THE BLR ADVANTAGE BLR Aerospace FastFin and Dual Tailboom Strakes will dramatically improve the performance

More information

ASPECTS REGARDING THE ELECTRIC PROPULSION OF THE UAV MULTICOPTER

ASPECTS REGARDING THE ELECTRIC PROPULSION OF THE UAV MULTICOPTER Review of the Air Force Academy No.3 (35)/2017 ASPECTS REGARDING THE ELECTRIC PROPULSION OF THE UAV MULTICOPTER Vasile PRISACARIU *, Bogdan HERCIU *, Andrei LUCHIAN ** * Henri Coandă Air Force Academy

More information

Innovating the future of disaster relief

Innovating the future of disaster relief Innovating the future of disaster relief American Helicopter Society International 33rd Annual Student Design Competition Graduate Student Team Submission VEHICLE OVERVIEW FOUR VIEW DRAWING INTERNAL COMPONENTS

More information

Product Comparison. F28F vs. Robinson R44

Product Comparison. F28F vs. Robinson R44 Product Comparison F28F vs. Robinson R44 F28F vs. R44 Specs Seats ENSTROM F28F ROBINSON R44 II 3 4 Continuous Engine Power (To Drivetrain) (hp) 225 205 Turbo-Charged? YES Empty Weight (As Configured )

More information

1.1 REMOTELY PILOTED AIRCRAFTS

1.1 REMOTELY PILOTED AIRCRAFTS CHAPTER 1 1.1 REMOTELY PILOTED AIRCRAFTS Remotely Piloted aircrafts or RC Aircrafts are small model radiocontrolled airplanes that fly using electric motor, gas powered IC engines or small model jet engines.

More information

Chapter 3: Aircraft Construction

Chapter 3: Aircraft Construction Chapter 3: Aircraft Construction p. 1-3 1. Aircraft Design, Certification, and Airworthiness 1.1. Replace the letters A, B, C, and D by the appropriate name of aircraft component A: B: C: D: E: 1.2. What

More information

GRWW1 5b Zeppelin airships

GRWW1 5b Zeppelin airships GRWW1 5b Zeppelin airships Airships were the first aircraft capable of controlled powered flight. Prior to WW1 Germany had become a world leader in the construction and operation of rigid lighter-than-air

More information

How to use the Multirotor Motor Performance Data Charts

How to use the Multirotor Motor Performance Data Charts How to use the Multirotor Motor Performance Data Charts Here at Innov8tive Designs, we spend a lot of time testing all of the motors that we sell, and collect a large amount of data with a variety of propellers.

More information

About Helicopters. Journal of Aircraft and Spacecraft Technology. Review

About Helicopters. Journal of Aircraft and Spacecraft Technology. Review Journal of Aircraft and Spacecraft Technology Review About Helicopters 1 Relly Victoria Petrescu, 2 Raffaella Aversa, 3 Bilal Akash, 4 Juan Corchado, 5 Filippo Berto, 2 Antonio Apicella and 1 Florian Ion

More information

Technical data of the Zeppelin NT 07

Technical data of the Zeppelin NT 07 Zeppelin NT The concept of the semi-rigid airship was re-defined with the development of the Zeppelin NT. It is the only kind of airship worldwide that has a rigid internal structure, in contrast to a

More information

How the V-22 Osprey Works

How the V-22 Osprey Works How the V-22 Osprey Works It has long been a dream of aircraft designers to create an airplane that not only can fly long ranges at high speeds and carry heavy cargo, but can also take off, hover and land

More information

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system:

High aspect ratio for high endurance. Mechanical simplicity. Low empty weight. STOVL or STOL capability. And for the propulsion system: Idealized tilt-thrust (U) All of the UAV options that we've been able to analyze suffer from some deficiency. A diesel, fixed-wing UAV could possibly satisfy the range and endurance objectives, but integration

More information

Product Comparison. 480B vs. Eurocopter EC120B

Product Comparison. 480B vs. Eurocopter EC120B Product Comparison 480B vs. Eurocopter EC120B 480B vs. Eurocopter EC120B Specifications Gross Weight = 2,800 lbs Gross Weight = 2,976 lbs Enstrom 480B Eurocopter EC120B Seats 1/4 or 2/1 1/4 or 2/3 Continuous

More information

SebArt professional line

SebArt professional line SebArt professional line Mini L39 1,46m ARF 90mm EDF-6S or P20-K30 turbine ASSEMBLY MANUAL The all new L39 Jet ARF was designed by Italy aerobatic pilot Sebastiano Silvestri. This sport ARF jet-model design

More information

CHAPTER 4 AIRWORTHINESS LIMITATIONS

CHAPTER 4 AIRWORTHINESS LIMITATIONS Section Title CHAPTER 4 AIRWORTHINESS LIMITATIONS 4-10 Airworthiness Limitations..................................... 4.1 4-20 Additional Limitations....................................... 4.3 4-21 Parts

More information

1/10 th Scale Model Tests of a Centre-line Tiltrotor:

1/10 th Scale Model Tests of a Centre-line Tiltrotor: 1/10 th Scale Model Tests of a Centre-line Tiltrotor: Conversion between rotary and fixed wing modes Bob Burrage Director Rotorcraft Operations Ltd., Oxfordshire, United Kingdom bob.burrage@ntlworld.com

More information

Mike Hirschberg, Executive Director AHS International The Vertical Flight Technical Society

Mike Hirschberg, Executive Director AHS International The Vertical Flight Technical Society www.vtol.org Mike Hirschberg, Executive Director AHS International The Vertical Flight Technical Society www.vtol.org Uber graphic April 2017 1 The global Vertical Flight Technical Society Founded in 1943

More information

PAC 750XL PAC 750XL PAC-750XL

PAC 750XL PAC 750XL PAC-750XL PAC 750XL The PAC 750XL combines a short take off and landing performance with a large load carrying capability. The PAC 750XL is a distinctive type. Its design philosophy is reflected in the aircraft's

More information

New Design Concept of Compound Helicopter

New Design Concept of Compound Helicopter New Design Concept of Compound Helicopter PRASETYO EDI, NUKMAN YUSOFF and AZNIJAR AHMAD YAZID Department of Engineering Design & Manufacture, Faculty of Engineering, University of Malaya, 50603 Kuala Lumpur,

More information

Air Buzz. 32nd Annual AHS International Student Design Competition

Air Buzz. 32nd Annual AHS International Student Design Competition Air Buzz 32nd Annual AHS International Student Design Competition Faculty Advisor: Dr. Daniel Schrage, Daniel.Schrage@aerospace.gatech.edu Ezgi Selin Akdemir esakdemir@gmail.com Undergraduate Middle East

More information

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables

Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design. Tables Aircraft Design: A Systems Engineering Approach, M. Sadraey, Wiley, 2012 Chapter 3 Aircraft Conceptual Design Tables No Component Primary function Major areas of influence 1 Fuselage Payload accommodations

More information

Exploration 4: Rotorcraft Flight and Lift

Exploration 4: Rotorcraft Flight and Lift Exploration 4: Rotorcraft Flight and Lift Students use appropriate terminology to describe the various stages of flight and discover that the lift force changes with the amount of air moved by the rotor

More information

German Aerospace Center Flight Operations

German Aerospace Center Flight Operations German Aerospace Center Flight Operations Introduction DLR is Germany s aerospace research center and space agency with about 4700 employees in 31 research institutes distributed over 8 main research centers

More information

L 298/70 Official Journal of the European Union

L 298/70 Official Journal of the European Union L 298/70 Official Journal of the European Union 16.11.2011 MODULE 12. HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS 12.1 Theory of Flight Rotary Wing Aerodynamics 1 2 Terminology; Effects of gyroscopic

More information

High Airspeed Testing of the Sikorsky X2 Technology TM Demonstrator ABSTRACT

High Airspeed Testing of the Sikorsky X2 Technology TM Demonstrator ABSTRACT High Airspeed Testing of the Sikorsky X2 Technology TM Demonstrator D. Walsh, S. Weiner, K. Arifian, T. Lawrence, M. Wilson, T. Millott and R. Blackwell Sikorsky Aircraft Corporation Stratford, CT 665

More information

145 e Technical Data EC145. (Civil Version) EC145. EC145 e

145 e Technical Data EC145. (Civil Version) EC145. EC145 e EC145e Technical Data 2015 145 e Technical Data EC145 (Civil Version) EC145 EC145 e Technical Data 3 Baseline Aircraft Definition GENERAL Energy absorbing fuselage Tail boom with fixed horizontal stabilizer

More information

Appenidix E: Freewing MAE UAV analysis

Appenidix E: Freewing MAE UAV analysis Appenidix E: Freewing MAE UAV analysis The vehicle summary is presented in the form of plots and descriptive text. Two alternative mission altitudes were analyzed and both meet the desired mission duration.

More information

X44 VTOL electric model plane with 4 Brushless motors

X44 VTOL electric model plane with 4 Brushless motors Manual X44 VTOL electric model plane with 4 Brushless motors 9944.100 EN 2-16 Content table Introduction... 4 Service centre... 4 Intended use... 5 Package content... 5 Symbol description... 6 Safety notes...

More information

EXECUTIVE SUMMARY 29 TH ANNUAL AHS INTERNATIONAL DESIGN COMPETITION UNDERGRADUATE CATEGORY

EXECUTIVE SUMMARY 29 TH ANNUAL AHS INTERNATIONAL DESIGN COMPETITION UNDERGRADUATE CATEGORY EXECUTIVE SUMMARY 29 TH ANNUAL AHS INTERNATIONAL DESIGN COMPETITION UNDERGRADUATE CATEGORY Eliya Wing Juan Pablo Afman Michael Avera Michael Burn Christopher Cofelice Peter Johnson Robert Lee Ian Moore

More information

HELICOPTERS. Technical Data

HELICOPTERS. Technical Data HELICOPTERS Technical Data 2017 EC145 3 Baseline Aircraft Definition GENERAL Energy absorbing fuselage Tail boom with fixed horizontal stabilizer and two endplates Upper deck with fittings for main gearbox,

More information

Introduction to Helicopter Aerodynamics and Dynamics Prof. Dr.C. Venkatesan Department of Aerospace Engineering Indian Institute of Technology, Kanpur

Introduction to Helicopter Aerodynamics and Dynamics Prof. Dr.C. Venkatesan Department of Aerospace Engineering Indian Institute of Technology, Kanpur Introduction to Helicopter Aerodynamics and Dynamics Prof. Dr.C. Venkatesan Department of Aerospace Engineering Indian Institute of Technology, Kanpur Lecture No. # 02 For, flying the helicopter we call

More information

10th Australian International Aerospace Congress

10th Australian International Aerospace Congress AUSTRALIAN INTERNATIONAL AEROSPACE CONGRESS Paper presented at the 10th Australian International Aerospace Congress incorporating the 14th National Space Engineering Symposium 2003 29 July 1 August 2003

More information

HELICOPTERS. Technical Data

HELICOPTERS. Technical Data HELICOPTERS Technical Data 2017 EC145 2.7 External Sound Levels Flight Phase Measurements according ICAO Annex 16 ICAO limits at 3,585 kg Measurements according FAR Part 36 FAR 36 limits at 3,585 kg Takeoff

More information

PRA Chapter 40. Boston to San Diego in gyros! Serving Southern Ohio, Northern Kentucky and Eastern Indiana

PRA Chapter 40. Boston to San Diego in gyros! Serving Southern Ohio, Northern Kentucky and Eastern Indiana Welcome to the June 2009 Edition of the Newsletter! Boston to San Diego in gyros! Chirs Kurz and fellow pilot Robert Müntz from Austria are taking the trip without a ground crew, flying MT-03 autogyros!

More information

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA)

ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ELECTRIC POWER TRAINS THE KEY ENABLER FOR CONTRA ROTATING PROPELLERS IN GENERAL AVIATION (& VICE VERSA) ATI D3 EVENT 8 TH MAY 2018 THE EMERGENCE OF ELECTRIFICATION IN AEROSPACE NICK SILLS, CONTRA ELECTRIC

More information

M o d u l e H e l i c o p t e r A e r o d y n a m i c s, S t r u c t u r e s a n d S y s t e m s

M o d u l e H e l i c o p t e r A e r o d y n a m i c s, S t r u c t u r e s a n d S y s t e m s M o d u l e 1 2-0 2 H e l i c o p t e r A e r o d y n a m i c s, S t r u c t u r e s a n d S y s t e m s F l i g h t C o n t r o l S y s t e m s 12-02- 1 T a b l e o f c o n t e n t s I. INTRODUCTION...

More information

Aerodynamic Testing of the A400M at ARA. Ian Burns and Bryan Millard

Aerodynamic Testing of the A400M at ARA. Ian Burns and Bryan Millard Aerodynamic Testing of the A400M at ARA by Ian Burns and Bryan Millard Aircraft Research Association Bedford, England Independent non-profit distributing research and development organisation Set up in

More information

STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES

STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES 16 TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS STRUCTURAL DESIGN AND ANALYSIS OF ELLIPTIC CYCLOCOPTER ROTOR BLADES In Seong Hwang 1, Seung Yong Min 1, Choong Hee Lee 1, Yun Han Lee 1 and Seung Jo

More information

CHAPTER 10 TAIL ROTOR TABLE OF CONTENTS

CHAPTER 10 TAIL ROTOR TABLE OF CONTENTS CHAPTER 10 TAIL ROTOR TABLE OF CONTENTS INTRODUCTION 3 GENERAL 3 HUB ASSEMBLY 3 TRUNION 4 YOKE ASSEMBLY 4 BEARING HOUSING 5 BLADES 5 STRUCTURE 5 BLADE MAJOR PARTS 7 PITCH-CHANGE MECHANISM 7 PITCH HORNS

More information

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE

Airframes Instructor Training Manual. Chapter 6 UNDERCARRIAGE Learning Objectives Airframes Instructor Training Manual Chapter 6 UNDERCARRIAGE 1. The purpose of this chapter is to discuss in more detail the last of the Four Major Components the Undercarriage (or

More information

FUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES

FUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES FUNDAMENTALS OF ROTOR AND POWER TRAIN MAINTENANCE TECHNIQUES AND PROCEDURES DISTRIBUTION RESTRICTION: Approved for public release; distribution is unlimited. HEADQUARTERS, DEPARTMENT OF THE ARMY CHAPTER

More information

( 19 ) United States. ( 12 ) Patent Application Publication ( 10 ) Pub. No. : US 2018 / A : Tayman ( 43 ) Pub. Date : Oct.

( 19 ) United States. ( 12 ) Patent Application Publication ( 10 ) Pub. No. : US 2018 / A : Tayman ( 43 ) Pub. Date : Oct. THE TWO TONTTITUNTUUDMOUNTAIN US 20180281939A1 ( 19 ) United States ( 12 ) Patent Application Publication ( 10 ) Pub. No. : US 2018 / 0281939 A1 Tayman ( 43 ) Pub. Date : Oct. 4, 2018 ( 54 ) VERTICALLY

More information

New Design Approach of Compound Helicopter

New Design Approach of Compound Helicopter New Design Approach of Compound Helicopter PRASETYO EDI, NUKMAN YUSOFF and AZNIJAR AHMAD YAZID Department of Engineering Design & Manufacture, Faculty of Engineering, University of Malaya, 50603 Kuala

More information

It has taken a while to get

It has taken a while to get HOVERING15 99 15 BASICS HOVERING Hovering It has taken a while to get here, but this is what all the building and planning were for to see light under those skids. But this is also the time when you have

More information

The AGUSTA 109 is a high speed, high performance twin engine helicopter, with a single main rotor system and anti-torque tail rotor system.

The AGUSTA 109 is a high speed, high performance twin engine helicopter, with a single main rotor system and anti-torque tail rotor system. Pag 1/5 1. HELICOPTER GENERAL INFORMATION The AGUSTA 109 is a high speed, high performance twin engine helicopter, with a single main rotor system and anti-torque tail rotor system. The twin engine design,

More information

POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE.

POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE. POWER. SAFETY. PERFORMANCE. ALL IN ONE PACKAGE. Some missions require more from a helicopter. More speed. More power. More payload. More productivity. These missions require the MD 600N. This single-turbine

More information

Three View DART T ft. 7.9 ft. 5 ft 14 ft. 2.5 ft. 1.4 ft. 18 ft. 7.8 ft. 1 Radius Clearance. Scale 50:1

Three View DART T ft. 7.9 ft. 5 ft 14 ft. 2.5 ft. 1.4 ft. 18 ft. 7.8 ft. 1 Radius Clearance. Scale 50:1 Three View DART T690 25.1 ft 7.9 ft 1.4 ft 5 ft 14 ft 2.5 ft 7.8 ft 18 ft 1 Radius Clearance Scale 50:1 Introduction In response to the AHS 2012 Request For Proposal for a pylon racing rotorcraft, the

More information

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures..

INDEX. Preflight Inspection Pages 2-4. Start Up.. Page 5. Take Off. Page 6. Approach to Landing. Pages 7-8. Emergency Procedures.. INDEX Preflight Inspection Pages 2-4 Start Up.. Page 5 Take Off. Page 6 Approach to Landing. Pages 7-8 Emergency Procedures.. Page 9 Engine Failure Pages 10-13 Propeller Governor Failure Page 14 Fire.

More information

Thank you for purchasing this product. Please read this manual carefully before use and retain it for your future reference.

Thank you for purchasing this product. Please read this manual carefully before use and retain it for your future reference. Thank you for purchasing this product. Please read this manual carefully before use and retain it for your future reference. Technical parameter of the helicopter Fuselage Length:80MM Gross Weight: about

More information

The Fokker S-14 Mach-trainer for FS9,FSX and Prepar3D

The Fokker S-14 Mach-trainer for FS9,FSX and Prepar3D The Fokker S-14 Mach-trainer for FS9,FSX and Prepar3D Fokker S-14 at Twente airforce base History The Fokker S-14 Mach-trainer was the first purpose designed and built side by side jet trainer. First flight

More information

AERONAUTICAL ENGINEERING

AERONAUTICAL ENGINEERING AERONAUTICAL ENGINEERING SHIBIN MOHAMED Asst. Professor Dept. of Mechanical Engineering Al Ameen Engineering College Al- Ameen Engg. College 1 Aerodynamics-Basics These fundamental basics first must be

More information

Lip wing Lift at zero speed

Lip wing Lift at zero speed Lip wing Lift at zero speed Dusan Stan, July 2014 http://hypertriangle.com/lipwing.php dusan.stan@hypertriangle.com HyperTriangle 2014 Lip_wing_Lift_at_zero_speed_R2.doc Page 1 of 7 1. Introduction There

More information

Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft. Wayne Johnson From VTOL to evtol Workshop May 24, 2018

Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft. Wayne Johnson From VTOL to evtol Workshop May 24, 2018 Designing evtol for the Mission NDARC NASA Design and Analysis of Rotorcraft Wayne Johnson From VTOL to evtol Workshop May 24, 2018 1 Conceptual Design of evtol Aircraft Conceptual design Define aircraft

More information

AS350C, AS350D, AS350D1, AS350B, AS350B1, AS350B2, AS350B3 AND AS350BA DGAC/EASA APPROVED ROTORCRAFT FLIGHT MANUAL when equipped with

AS350C, AS350D, AS350D1, AS350B, AS350B1, AS350B2, AS350B3 AND AS350BA DGAC/EASA APPROVED ROTORCRAFT FLIGHT MANUAL when equipped with Supplement FMS-350(4) FAA/EASA APPROVED ROTORCRAFT FLIGHT MANUAL SUPPLEMENT TO THE EUROCOPTER MODELS AS350C, AS350D, AS350D1, AS350B, AS350B1, AS350B2, AS350B3 AND AS350BA DGAC/EASA APPROVED ROTORCRAFT

More information

70MM YAK-130 STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM

70MM YAK-130 STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM 70MM YAK-130 REALISTIC RETRACT & FLAPS INSTALLED RIGID STRONG DURABLE EPO STABLE SMOOTH FLYING PERFORMANCE FMSMODEL.COM Table of Contents Introductions 3 Contents of Kit 4 Assemble the plane 5 Battery

More information

ELA 07 Cougar. The ELA 07 Cougar joins sportive look and simply irresistible features. Caring for every detail is what makes a brand great.

ELA 07 Cougar. The ELA 07 Cougar joins sportive look and simply irresistible features. Caring for every detail is what makes a brand great. ELA AVIACION The gyroplane The gyroplane was invented in 1923 by the Spanish engineer Juan de la Cierva. It is a type of rotorcraft whose non-driven rotor works in a permanent autorotation regime due to

More information

SERVICE INFORMATION LETTER # 0121 Addition A. Subject; Tracking the Enstrom Rotor System using the Chadwick 2000 balance system.

SERVICE INFORMATION LETTER # 0121 Addition A. Subject; Tracking the Enstrom Rotor System using the Chadwick 2000 balance system. SERVICE INFORMATION LETTER # 0121 Addition A Date: Subject; Tracking the Enstrom Rotor System using the Chadwick 2000 balance system. Models: All models Effectively: All Serial Numbers Experience shows

More information

A copy can be downloaded for personal non-commercial research or study, without prior permission or charge

A copy can be downloaded for personal non-commercial research or study, without prior permission or charge Ferguson, Kevin, and Thomson, Douglas (2014) Flight dynamics investigation of compound helicopter configurations. Journal of Aircraft. ISSN 1533-3868 Copyright 2014 American Institute of Aeronautics and

More information

F9F-2 OPERATIONAL MANUAL

F9F-2 OPERATIONAL MANUAL F9F-2 OPERATIONAL MANUAL 7 different color to meet customer s choice. 2 different material F9F-2/OB: F9F-2/TB: F9F-2/YB: F9F-2/WR: F9F-2/GYR: F9F-2/GRW: F9F-2/BRY: Original Blue Tail Blue Yellow/Blue White/Red

More information