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Pneumatics for Supersonic Transport
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English
Abstract
With the advent of the supersonic transport accessory power system, designers will be faced with a quantum jump in power requirements and environmental conditions. All types of systems must be studied before a selection is made.
The advantages and disadvantages of a pneumatic system for secondary power transmission on aerospace vehicles are given along with the results of four years operation of the pneumatic utility system on the Fairchild F-27. The requirements and operating conditions for secondary power on the supersonic transport are discussed and subsystem designs are presented.
Citation
Schmidlin, A., "Pneumatics for Supersonic Transport," SAE Technical Paper 630223, 1963, https://doi.org/10.4271/630223.Also In
References
- Cannon C. H. “Research on a 1000 F Pneumatic System.” Lockheed Aircraft Corp., Ga. Contract No. AF33(616) - 3761; Unconfirmed Minutes of Meetings No. 43, Oct. 1957 and No. 44, May 1958; SAE Committee A-6, Aircraft and Missile Hydraulic and Pneumatic Systems and Equipment.
- Casebolt R. W. “Development of a High Temperature Nuclear Radiation Resistant Pneumatic Power System for Flight Vehicles.” General Dynamics/Convair; Contract No. AF33 (616)-7582; Unconfirmed Minutes of Meetings No. 52, May 1962 and No. 53, Oct. 1962; SAE Committee A-6, Aerospace Fluid Power Systems and Equipment.
- Kibby B. G. Toplin L. B. Feucht R. E. “Progress of the Aeronautical System Division Hot Gas Flight Stabilization System Program.” Paper presented at the SAE Aerospace Fluid Power Systems and Equipment Meeting, Subcommittee A-6B, Montreal May 1962
- “The Supersonic Transport Propulsion System Component Research and Study Program.” Wright Aeronautical Div., Curtiss Wright Corp., Contract No. AF33(657)-9058.
- Schmidlin A. E. “Hot Gas Control Systems - I, Basics of Hot Gas Systems Design,” Control Engineering Jan. 1961
- “SAE Aerospace Fluid Power Meeting.” Hydraulics and Pneumatics August 1962 96