PUMP RATE CHANGE VS. RUN TIME OF A RADIAL SHAFT SEAL

Similar documents
Investigation of Seal Pumping Rate by Using Fluorescent Method

Twin Screw Compressor Performance and Its Relationship with Rotor Cutter Blade Shape and Manufacturing Cost

Extremely High Load Capacity Tapered Roller Bearings

Effect of Preheating Air in Petrol Engine by Using Exhaust Gas Heat Energy

Ansys-CFX Analysis on a Hatch-Back Car with Wheels and without Wheels

Revision 4 May 23, 2018

CFD Investigation of Influence of Tube Bundle Cross-Section over Pressure Drop and Heat Transfer Rate

Cooling Enhancement of Electric Motors

Multi Body Dynamic Analysis of Slider Crank Mechanism to Study the effect of Cylinder Offset

The Experimental Study of the Plateau Performance of the F6L913 Diesel Engine

Flanging and Hemming of Auto Body Panels using the Electro Magnetic Forming technology

BEARING GUIDE. Bearing Guide Created by REV Robotics 2016, Licensed Under CC BY-SA 1

A Micro Power Generation System with Gas Turbine Engine and Piezo Converter -- Modeling, Fabrication and Characterization --

STRYKER VEHICLE ADVANCED PROPULSION WITH ONBOARD POWER

Research in hydraulic brake components and operational factors influencing the hysteresis losses

DEVELOPMENT OF A DUAL PURPOSE VISUALIZATION TECHNIQUE FOR THE STUDY OF ROTATING SHAFT SEALS

Causes of and Countermeasures for Allophone Trouble in a Piston Seal System for Cylinders

Case Study Involving Surface Durability and Improved Surface Finish

technology made in Italy

Is Low Friction Efficient?

THE INFLUENCE OF THE SIZE AND SHAPE OF THE CENTRAL BODY OF A COMBUSTION CHAMBER ON THE TOXICITY OF THE EXHAUST GASES IN THE URSUS 4390 ENGINE

PREDICTION OF PISTON SLAP OF IC ENGINE USING FEA BY VARYING GAS PRESSURE

STUDY ON VEHICLE PULL CHARACTERISTICS ACCORDING TO TIRE TREAD PATTERN

Application of ABAQUS to Analyzing Shrink Fitting Process of Semi Built-up Type Marine Engine Crankshaft

A Prototype Oil-Less Compressor for the International Space Station Refrigerated Centrifuge

Emergency Repair of Runway after Cargo Plane Accident

Orientalmotor. Development of K II Series Hypoid Geared Motor

Simulation and Analysis of Vehicle Suspension System for Different Road Profile

Analysis of Emission characteristics on Compression Ignition Engine using Dual Fuel Mode for Variable Speed

Finite Element Analysis on Thermal Effect of the Vehicle Engine

CYLINDRICAL ROLLER BEARING CATALOG TIMKEN SMALL BORE METRIC SEALS CATALOG

Simulation Analysis of Shock Absorber Lip Seal

Verifying the accuracy of involute gear measuring machines R.C. Frazer and J. Hu Design Unit, Stephenson Building, University ofnewcastle upon Tyne,

Influence of Internal Combustion Engine Parameters on Gas Leakage through the Piston Rings Area

WITH BIO LUBRICANTS JATROPHA OIL, CASTOR OIL, NEEM OIL AND MINERAL OIL (SAE 20W50)

A Study of EGR Stratification in an Engine Cylinder

EFFECTIVENESS OF COUNTERMEASURES IN RESPONSE TO FMVSS 201 UPPER INTERIOR HEAD IMPACT PROTECTION

Investigation of Radiators Size, Orientation of Sub Cooled Section and Fan Position on Twin Fan Cooling Packby 1D Simulation

Regimes of Fluid Film Lubrication

Design of Piston Ring Surface Treatment for Reducing Lubricating Oil Consumption

LOAD SHARING WITH PARALLEL INVERTERS FOR INDUCTION MOTOR DRIVE APPLICATION

Transmission Error in Screw Compressor Rotors

Probabilistic Analysis for Resolving Fatigue Failures of the Connecting Rod Oil Hole

Zurcon U-Cup RU2. Single Acting U-Cup Asymmetric, Double Lip, Compact Material: Zurcon

4th European PV-Hybrid and Mini-Grid Conference, Glyfada, Greece, May 2008

DICHTOMATIK Sealing mechanism

Design of A New Non-Contact Screw Seal and Determination of Performance Characteristics

Paper Number: DETC

Thrusters Health Monitoring of Propulsion and Steering Devices

Test rig for rod seals contact pressure measurement

ImprovingtheFlowRateofSonicPumpbyMeansofParabolicDeflector

THE INFLUENCE OF THE MICROGROOVES ON THE HYDRODYNAMIC PRESSURE DISTRIBUTION AND LOAD CARRYING CAPACITY OF THE CONICAL SLIDE BEARING

CONTROL AND PERFORMANCE OF A DOUBLY-FED INDUCTION MACHINE FOR WIND TURBINE SYSTEMS

Available online at ScienceDirect. Procedia Engineering 68 (2013 ) 70 76

New York Science Journal 2017;10(3)

Continuous Stribeck Curve Measurement Using Pin-on-Disk Tribometer

Design Documentation in ME 2110

NEW CONCEPT OF A ROCKER ENGINE KINEMATIC ANALYSIS

Merkel PRW 1 Double Wiper with Integrated Pressure Relieve. Product Information Merkel Hydraulics

The Gear Whine Noise and vibro-acoustic emission of gear-box

Active Suspensions For Tracked Vehicles

THERMAL MANAGEMENT OF AIRCRAFT BRAKING SYSTEM

November 8, 2018 GAS TURBINE ENGINE SECONDARY FLOW SYSTEMS

FlexiCase Rotary Seals Introduction

Propeller Blade Bearings for Aircraft Open Rotor Engine

FAULT ANALYSIS FOR VOLTAGE SOURCE INVERTER DRIVEN INDUCTION MOTOR DRIVE

CFD Analysis for Designing Fluid Passages of High Pressure Reciprocating Pump

ABB challenges on tribology related technology Tribology Days Nynäs/Sweden

This is a repository copy of Combating automative engine valve recession.

Efficient and Effective bearing performance evaluation

Zwick. Materials testing. Product Information Temperature chambers for AllroundLine

Building and Validating a Rotational Viscometer

THE STUDY ON EFFECT OF TORQUE ON PISTON LATERAL MOTION

1/2" AIR DRIVEN DIAPHRAGM PUMP

Wind Turbine Gear Lubricants

BALL BEARING TESTS TO EVALUATE DUROID REPLACEMENTS

Tapered Roller Bearings. Reliable energy efficient suitable for high loads

DEMONSTRATION OF A HYDROGEN FUEL CELL LOCOMOTIVE

Procedia Engineering 00 (2009) Mountain bike wheel endurance testing and modeling. Robin C. Redfield a,*, Cory Sutela b

Optimization Procedure for Complete Planetary Gearboxes with Torque, Weight, Costs and Dimensional Restrictions Ulrich Kissling 1,a, Inho Bae 1,b

Chandra Prasad B S, Sunil S and Suresha V Asst. Professor, Dept of Mechanical Engineering, SVCE, Bengaluru

Bray/ VAAS Slurry Series Knife Gate Valve 760/762/765/766/767/768 Series Operation and Maintenance Manual

Development of an innovative diaphragm accumulator design and assembly process

Module7:Advanced Combustion Systems and Alternative Powerplants Lecture 32:Stratified Charge Engines

COMPANY PRESENTATION SPECIALISTS IN SEALING SOLUTIONS FOR HEAVY DUTY APPLICATIONS

Scroll Expander for Carbon Dioxide Cycle

Cooldown Measurements in a Standing Wave Thermoacoustic Refrigerator

TECHNICAL CHARACTERISTICS

STICTION/FRICTION IV STICTION/FRICTION TEST 1.1 SCOPE

Friction and Vibration Characteristics of Pneumatic Cylinder

GH-BETTIS SERVICE INSTRUCTIONS DISASSEMBLY & REASSEMBLY FOR MODELS HD521-M4, HD721-M4 AND HD731-M4 DOUBLE ACTING SERIES PNEUMATIC ACTUATORS

Drive Axles SHAIS171. The Dana LMS Hub is available on the following Steer and Drive Axle Models:

Scroll Compressor Oil Pump Analysis

Enhancement of Power Quality in Transmission Line Using Flexible Ac Transmission System

Purge System Designs. Heavy Fouling Applications

Developments in Dry Running Seals for Reciprocating Compressors

Theoretical and Experimental Evaluation of the Friction Torque in Compressors with Straddle Bearings

Hydraulic Pump and Track Motor for Hydrostatic Transmission

IMPROVING SULFURIC ACID PLANT PERFORMANCE THROUGH NEW SHAPE & HIGHER ACTIVITY CATALYSTS

CFD ANALYSIS ON LOUVERED FIN

Transcription:

PUMP RATE CHANGE VS. RUN TIME OF A RADIAL SHAFT SEAL Mark Reimer, Maria Mendizabal ESP International ARTICLE INFO 13 August 2012 ABSTRACT In this study, the pump rate of the seal lip was measured over a period of time to learn how the pump rate of the seal lip modifies over time. Introduction The challenge of sealing against a dynamic surface has been around since the frontier era. The first known seals were leather straps used to retain animal fat on the end of a wheel axel. This crude seal required routine maintenance. The Industrial Revolution spawned the development of engines, transmissions and gearboxes. The seals of the industrial age were organic ropes or packing. These seals were very effective until speeds, temperature and other parameters increased with the development of better transportation systems. In the late 1920 s, a self contained shaft seal was created from oil resistant leather assembled into a metal case. This was the first radial lip seal to take advantage of a metal press fit as an outside diameter seal. After that, radial shaft seals develop; a synthetic, oil-resistant rubber replaced the leather element, forever changing seal design. Radial shaft seals prevent leakage through the generation of a pumping action at the interface of the seal lip and the shaft surface, the pumping direction is a direct correlation to the direction of an asymmetrical contact pressure profile (See Figure 1). This pressure profile is controlled by the geometric design of the lip seal which is designed to create a larger pressure gradient on the oil side of the sealing lip. This pressure gradient is one aspect that contributes to the function of a radial shaft lip seal. A second aspect that contributes to the pumping mechanism of a seal lip is the presence of an oil film layer between the seal surface and the shaft surface. Jagger [1] [2] successfully demonstrated the existence of this oil film layer between the shaft and lip. Figure 1: Dynamic Sealing Mechanism

The third aspect in the sealing mechanism that contributes to the net pumping affect of the seal lip is the formation of asperities on the seal lip surface. As shown by Müller [3], the asperities become aligned at an angle to the rotating shaft causing the oil film to pump towards the oil side of the seal. The existence of the pressure asymmetric pressure profile, fluid film and asperities all contribute to the pumping mechanism of the seal. It is our opinion that the life of a seal lip is modified when one or more of these items are modified. In this study, the affect of lip wear on the seal lip pump rate is investigated. As the seal wears the contact width of the seal lip grows and the asymmetric pressure profile is modified. As well, the elastomer of the seal will harden over time due to its exposure to fluid at temp. Eventually both factors contribute to the occurrence of a seal leak. In this study, we have run a lip seal and measured the change in pump rate over the life of the seal. This is done to demonstrate the loss of pump rate as the seal lip wears and that loss of pump rate will result in a seal leak. Test Seal For this study, a specific seal size was chosen. The seal used in this test was ESP part number TBC29-025004700080-FCS. Figure 3 shows the profile of the seal and Table 1 Figure 3: Helix Style displays the designed bore and shaft sizing for the test seal. To aid in the pumping measurement, the two dust lips shown were removed. The test seal had a bidirectional U style helix (as shown in Figure 2). The helix design parameters are displayed in Table 2. The test seal has a Fluorocarbon lip with a stainless steel garter spring. The seal lip design is a common design widely used in other seals. Figure 2: Test seal profile ID OD Width Lip Material 25.00 mm 47.00 mm 8.00 mm Fluorocarbon Table 1: Seal Parameters Aid Style U Rib Spacing 2 Rib Height 0.05 Helix Angle 30 Number Protrusions 6 Table 2: Helix Parameters

Pumping Rate Test Method A pump rate measurement method similar to the method used in Yang [4] was used in this study. The equipment used is depicted in Figure 4. Here the test seal is placed on the shaft between the internal and external cavity with the oil side of the seal lip towards the internal cavity. The test seal was run for 50 hours for the break in period at 5000 RPM. The shaft diameter was 24.00 mm (0.984 ), the bore diameter 50.0 mm (1.85 ). To measure the pump rate the internal cavity (Figure 4) had a port at the top where the oil pumped by the seal would exit and would be collected for measurement After the break in period the seal ran for 100 hours at 5000 RPM, in John Deere J20C hydraulic oil, at a half shaft level and heated to 110 C. After each 100 hours the exterior and interior cavity was filled with oil, the seal was then run at the desired measurement speed for 30 minutes in order to attain a stable measurement. After that the speed was changed to 2000 RPM and the process was repeat until the max speed of 10000 RPM. Figure 4: Pump Rate Testing Machine

5000 4000 3000 2000 1000 10000 9000 8000 7000 6000 Results The graph in Figure 5 shows the data collected during the test. As shown in the data, the pump rate was very high initially then started to reduce over time. This seal was tested until a leak occurred at the 5000 RPM shaft speed. TBC29-098418500315-FCS Pump Rate g/min 1.8 1.6 1.4 1.2 1 0.8 0.6 0.4 0.2 0 1.6-1.8 1.4-1.6 1.2-1.4 1-1.2 0.8-1 0.6-0.8 0.4-0.6 0.2-0.4 0-0.2 RPM Figure 5: Pump rate vs. Time vs. Shaft speed Conclusions The seal lip pump rate performed as expected and reduced as the seal lip wore. The one thing that we did not do in this study was monitor the seal lip contact width at each 100 hour interval. With that added data we could demonstrate that there is a direct correlation between seal lip pump rate and contact width growth. The other thing that we did not do was monitor the change in elastomer compression set. We are planning a second seal test that will include this information.

Works Cited [1] E. T. Jagger, "Rotary shaft seals: the sealing mechanism of synthetic rubber lip seals running at atmospheric pressure," Proceedings of the IMechE, vol. 171, pp. 597-616, 1957. [2] E. Jagger, "Study of the lubrication of synthetic rubber rotary shaft seals," Proceedings of the IMechE Conference on Lubrication and Wear, pp. 409-415, 1957. [3] H. Müller, "Concepts of sealing mechanism of rubber lip type rotary shaft seals," in Proceedings of 12th International Sealing Conference, 1987. [4] A.-S. Yang, "Parametric study of helix configuration in ribbed lip seal," Tribology International, vol. 53, pp. 98-107, 2012.