This specification defines the objectives, criteria, and configuration, and establishes the requirements for performance, design, test, and qualification for the Aircraft Engine Installation Subsystem (AEIS) for the prototype model supersonic transport airplane. The subsystem provides the total propulsive power required by the airplane for accomplishing its intended functions. The subsystem also provides mechanical and pneumatic power for supporting airframe accessory, environmental and air inlet subsystems. The subsystem contains the engine, exhaust and thrust reverser assembly engine accessories, engine mounting provisions, engine controls, cowling, bleed air ducting, instrumentation plumbing and wiring.
Supersonic Transport Development Program. Phase III Proposal. Boeing Model 2707. Aircraft Engine Installation Subsystem Specification
1966
64 pages
Report
Keine Angabe
Englisch
Jet & Gas Turbine Engines , Aircraft , Jet transport planes , Turbofan engines , Supersonic aircraft , Specifications , Configuration , Pneumatic devices , Airframes , Environment , Jet engine inlets , Exhaust systems , Thrust reversal , Engine mounts , Control systems , Control panels , Engine starters , Drives , Power