SAE Papers

Paper Number	Paper Title	Book Number
985561	Reduction of Hydraulic System Pressure Spikes Through Limiting of Servovalve Current Change Rate
975651	Evolution of the Md-95 Hydraulic System
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 Hydrulic System Simulation--An Integrated Approach
901997	Hydraulic Power Loss Prevention on Commercial Transport Aircraft--Available Technology
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	Commerical 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
700773	Designing for Deep-Ocean Hydraulics
700774	Fluid Systems in Deep Submersibles
700789	Future Airplane Hydraulic Distribution System Design Developments and Testing Criteria
700792	High-Speed Variable-Delivery Vane Pump With Flexible Laminated Cam Ring Design
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
670547	Axial-Gear Differential Constant-Speed Drives for Driving Constant-Frequency A-C Generators on Aircraft
670530	Comparative Evaluation of Flight Control Power Distribution Systems for Hypersonic Aircraft
670584	Computer Technique to Evaluate Routing of Tubing on Turbine Engine Fuel, Oil, and Hydraulic Systems
670535	Corrosion Inhibition, Sea-Water Compatibility, and Fire Resistance of Hydraulic Fluids for Deep Submergence Vehicles
670582	Design of Integrated Flight Control/Hydraulic System for Boeing 2707 Supersonic Transport Aircraft
670528	Flight Control System for the Boeing 2707 Supersonic Transport Airplane
670529	Hydraulic Power Units for Supersonic Aircraft
670825	Methods of Maintaining Cleanliness of Parts for Liquid Propellant and Hydraulic Systems and Spacecraft Interiors
670564	Sheaves - a Growth Contaminant in Hydrocarbon Systems
670531	Special Problems Encountered in the Design of the Hydraulic System for the Concorde Supersonic Transport
670585	Use of Induction Brazing Method to Form Permanent Joints in Hydraulic Tubing for the A-74 Corsair Ii Aircraft
660664	Evaluation of Proposed Hydraulic Fluids for the Supersonic Transport
660661	Hydraulic Fluids for High-Altitude High-Temperature, High Performance Vehicles
650345	Control of Contamination in Rocket Booster Hydraulic Systems
650306	Design of Hydraulic Gimbal System for Moon Mission Booster Stage
650347	Development of Failure Analysis Program for a High Reliability Missile Hydraulic Power Supply
650307	Development of Fluid Power Techniques for Lunar Environments
650358	Developments in High-Strength Tubing
650352	Effect of Contamination on Fluids and Effect of Ingredients of the Fluids on Contamination
650333	Establishing Hydraulic System Operational Contamination Limits
650327	Fire-Resistant High-Temperature Hydraulic Fluids for Supersonic Transport
650337	Grade a Hermetically Sealed Hydraulic Servo System
650315	High-Performance Single-Stage Servovalve
650317	Hybrid Digital Hydraulic Servo
650336	Modular Hydraulic Servos
650329	New Considerations in Hydraulic Fluid Testing
650323	New Design Concepts in the Dc-9 Hydraulic System
650318	New Servovalve Concept--The Ball Valve
650343	Operation and Maintenance Requirements for Supersonic Transport Hydraulic Systems
650326	Operation and Maintenance of Caravelle Jet Transport Hydraulic System
650339	Pneumatic-Hydraulic Power Converter
650335	Pulsating Flow Hydraulic Concepts
650361	Redundant Damper Servoactuators for the F-111 Airplane
650305	Saturn S-Ii Stage Engine Actuation System
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	Servovalve Internal Leakage as Affected By Contamination
650328	Supersonic Transport Fluid Evaluation Program
650341	Technical Considerations in Designing a Hydraulic System for Supersonic Transport
650798	Technological Advancements Resulting From Xb-70 Performance Requirements
650331	Value Engineering of Contamination Control