Search NASAโŒ• Search

NASA NTRS ยท 19790005926

Variable area exhaust nozzle

Abstract

An exhaust nozzle for a gas turbine engine comprises a number of arcuate flaps pivotally connected to the trailing edge of a cylindrical casing which houses the engine. Seals disposed within the flaps are spring biased and extensible beyond the side edges of the flaps. The seals of adjacent flaps are maintained in sealing engagement with each other when the flaps are adjusted between positions defining minimum nozzle flow area and the cruise position. Extensible, spring biased seals are also disposed within the flaps adjacent to a supporting pylon to thereby engage the pylon in a sealing arrangement. The flaps are hinged to the casing at the central portion of the flaps' leading edges and are connected to actuators at opposed outer portions of the leading edges to thereby maximize the mechanical advantage in the actuation of the flaps.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Johnston, E. A.. 1979-01-02. Variable area exhaust nozzle. https://ntrs.nasa.gov/citations/19790005926

Cite the original work for its findings. Save a collection to share your selection of sources.