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SAE Papers

Paper Number / Title
For more information, click on the Paper Number
Book Number
985561
Reduction of Hydraulic System Pressure Spikes Through Limiting of Servovalve Current Change Rate
 
975651
Evolution of the MD-95 Hydraulic Systm
 
921914
Liquid Tight Insulation for High Temperature Aircraft Ducting
 
902004
A Concurrent Design/Analysis Tool for Aircraft Hydraulic Systems
 
901794
Design, Development, and Demonstration of a High-Pressure, Overcenter, Variable-Displacement Hydraulic Motor
 
902003
Dynamic Hydraulic System Simulation-An Integrated Approach
 
901997
Hydraulic Power Loss Prevention on Commercial Transport Aircraft-Available Technology
 
892261
Rotary Servohinge Actuator
 
881436
A High Pressure Sealing System for Linear Actuators
 
881363
HYTRAN Enhancements that Meet Aerospace Hydraulic-System Analysis Needs
 
881434
Locking Actuators Today and Beyond
 
881364
Software Simulation for Hydraulic Transients
 
881435
The Comparative Analysis and Development of an 8000 PSI Rotary Vane Actuator
 
872446
Computational Fluid Dynamics in Aerospace
 
870749
Small Steps to Big Savings with ECM - (An Old Friend with a New Name)
 
861734
A Systems Approach to Engine Starting System Design
 
861713
Advanced Pneumatic Start Systems for APUs
 
861801
Airbus A320 Side Stick and Fly By Wire — An Update
 
861683
Commercial Supersonic Operations - Ten Years of Experience With Concorde
 
861844
Controlled Pressure Pumps for More Efficient Hydraulic Systems
 
861712
Fast Start APU Technology
 
861736
Minimizing Heat Rejection in Aircraft Accessory Drive Gearboxes
 
861711
Past, Present and Future of Hydraulic APU Start Systems
 
851757
Energy Efficient Actuation Using Variable Displacement Hydraulic Control
 
851913
8000 psi Hydraulic System Seals and Materials Test Program-A Progress Report
 
851908
Air Force Nonflammable Hydraulic System Materials Development
 
851914
Bellows Accumulators for 8000 PSI Hydraulic Systems
 
851911
Hydraulic Pumps for High Pressure Non-Flammable Fluids
 
851910
Lightweight Hydraulic System Technology-8000 PSI Update
 
851795
Mechanical Interface Devices for Automatic Test Equipment
 
851909
Nonflammable Fluid and 8,000 psi Technology for Future Aircraft Hydraulic Systems (22 CFR 125.4 (b) (13) Applicable)
 
831491
A Responsive Compact Hydraulic System for a Remotely Operated Vehicle
 
831487
A310 Hydraulic Power System
 
831489
Application of Microprocessors to Aircraft Fly-By-Wire Hydraulic Actuation Systems, SAE Committee A-6 1983
 
831488
The Boeing 767 Hydraulic System
 
821511
Background for Impulse Testing of Hydraulic Medium and High Pressure Components
 
821512
Rotary Flexure Testing of Hydraulic Tube Connections
 
821510
Status of Standardization for U.S. Aerospace Hydraulic Systems
 
811084
Advanced Generating System Technology
 
801193
Digital Computer Simulation of Aircraft Hydraulic Systems
 
801195
Evolution of an Optical Control System for Aircraft Hydraulics
 
801189
Lightweight Hydraulic System Development and Flight Test
 
801188
New Hydraulic System Technology for Future Aircraft
 
801194
Real-Time Microprocessor Technology Applied to Automatic Braking Systems
 
801190
The Use of Power–Adaptive and Power–Reversible Flight Control Actuation Systems to Achieve Hydraulic Power and System Weight Savings
 
791079
The Practical Aircraft Hydraulic Test Stand
 
771007
Flight Testing an 8000 PSI Lightweight Hydraulic System
 
760860
Non-Elastomeric Rod Seals for Advanced Hydraulic Systems
 
740887
The PHM Hydrofoil Automatic Control System
 
730986
Fluid Power and Control Requirements for the Space Shuttle Orbiting Vehicle
 
720838
Hydraulic and Flight Control System for Space Shuttle Orbiter
 
700792
A New Development in High Speed Variable Delivery Vane Pumps
 
700773
Designing for Deep-Ocean Hydraulics
 
700774
Fluid Systems in Deep Submersibles
 
700789
Future Airplane Hydraulic Distribution System Design Developments and Testing Criteria
 
700790
High-Temperature Polyimide Hydraulic Actuator Rod Seals for Advanced Aircraft
 
700784
New Developments in Fluidics for Aircraft High-Pressure Hydraulic System Applications
 
690658
A New Concept to Provide Emergency Auxiliary Power for Aircraft
 
690659
Emergency Monopropellant Auxiliary Power Units for Large Commercial Aircraft
 
690670
Hydraulic System State-of-the-Art Advances on the 747 Airplane
 
670584
A Computer Technique to Evaluate Routing of Fluid System Plumbing for Aircraft Engines
 
670547
AGD - Concept to Configuration
 
670530
Comparative Evaluation of Flight Control Power Distribution Systems for Hypersonic Aircraft
 
670585
Evolution of the A-7A Hydraulic Tubing Permanent Joint System
 
670528
Flight Control System for The Boeing 2707 Supersonic Transport Airplane
 
670535
Hydraulic Fluids for Deep Submergence
 
670529
Hydraulic Power Units for Supersonic Aircraft
 
670825
Maintaining the Cleanliness of Clean Parts
 
670564
Sheaves: A Growth Contaminant in Hydrocarbon Systems
 
670531
The Hydraulic System of the Concorde
 
670582
The United States SST Controls Development Program
 
660664
Evaluation of Proposed Hydraulic Fluids for the SST
 
660661
HYDRAULIC FLUIDS FOR HIGH ALTITUDE-HIGH TEMPERATURE VEHICLES
 
650317
A Hybrid Digital Hydraulic Servo
 
650318
A New Servovalve Concept - The Ball Valve
 
650345
Control of Contamination in Rocket Booster Hydraulic Systems
 
650306
Design of a Hydraulic Gimbal System for a Moon Mission Booster Stage
 
650307
Development of Fluid Power Techniques for Lunar Environments
 
650347
Development of a Failure Analysis Program for a High Reliability Missile Hydraulic Power Supply
 
650358
Developments in High Strength Tubing
 
650333
Establishing Hydraulic System Operational Contamination Limits
 
650327
Fire-Resistant High Temperature Hydraulic Fluids for the SST
 
650337
Grade A Hermetically Sealed Hydraulic Servo System
 
650315
High Performance Single-Stage Servovalve
 
650336
Modular Hydraulic Servos
 
650329
New Considerations in Hydraulic Fluid Testing
 
650323
New Design Concepts in the DC-9 Hydraulic System
 
650343
Operation and Maintenance Requirements for SST Hydraulic Systems
 
650339
Pneumatic-Hydraulic Power Converter
 
650335
Pulsating Flow Hydraulic Concepts
 
650361
Redundant Damper Servoactuators for the F-111 Airplane
 
650304
Saturn V S-IC Stage Engine Gimbal Actuation System
 
650319
Selection of a Least “Cost” Hydraulic System for Launch Vehicle Engine Position Control
 
650334
Servo Valve Internal Leakage as Affected by Contamination
 
650326
Situation Completely Fluid - Caravelle Jet Transport Hydraulic System, Operation and Maintenance
 
650328
Supersonic Transport Fluid Evaluation Program
 
650341
Technical Considerations in Designing a Hydraulic System for the SST
 
650798
Technological Advancements Resulting from XB-70 Performance Requirements
 
650352
The Effect of Contamination on Fluids and the Effect of the Ingredients of the Fluids on Contamination
 
650305
The Saturn S-II Stage Engine Actuation System
 
650331
Value Engineering of Contamination Control
 

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