Engine Exhaust System Design Considerations for Rotorcraft
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Product Code: ARP4056
Date Published: 1989-10-01
Issuing Committee:
S-12 Helicopter Powerplant Committee
Scope
Turbine engines installed in rotorcraft have an exhaust system that is designed and produced by the aircraft manufacturer. The primary function of the exhaust system is to direct hot exhaust gases away from the airframe. The exhaust system may consist of a tailpipe, which is attached to the engine, and an exhaust fairing, which is part of the rotorcraft. The engine manufacturer specifies a baseline "referee" tailpipe design, and guaranteed engine performance is based upon the use of the referee tailpipe and tailpipe exit diameter. The configuration used on the rotorcraft may differ from the referee tailpipe, but it is intended to minimize additional losses attributed to the installation.
This Aerospace Recommended Practice (ARP) describes the physical, functional, and performance interfaces to be considered in the design of the aircraft exhaust system.
Product Status: In Stock
File Size:
377K
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| Current & Historical versions of this standard |
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| Standard |
Date published |
?Status |
| ARP4056 |
1989-10-01 |
Issued |
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