Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B

Supersonic Transport Aircraft Engine. Phase Ii-b. Development Program Fuel Control System Study. Appendix B PDF Author: PRATT AND WHITNEY AIRCRAFT GROUP EAST HARTFORD CT.
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Languages : en
Pages : 164

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Book Description
Hamilton Standard, under contract to Pratt and Whitney Aircraft, has conducted a design and development study to conceive and optimize, within contract and time limitations, a fuel control system for the P and WA SST engine. This effort consisted of design and analytical studies, material investigations, and development efforts necessary to adapt current state-of-the-art concepts and new concepts into a fuel control system compatible with the SST environments, envelope requirements, and accuracy tolerances specified for this application. The system decided upon and studied is a hydromechanical unitized concept featuring high reliability, ease of maintenance, durability, and low overall system weight. This report covers all studies conducted under Phase 2 B of the contract for the fuel control system as well as Hamilton Standard funded elastomeric seal development work.