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Variable area exhaust nozzleAn 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.
Document ID
19790005926
Acquisition Source
Legacy CDMS
Document Type
Other - Patent
Authors
Johnston, E. A.
(GE Cincinnati, United States)
Date Acquired
September 3, 2013
Publication Date
January 2, 1979
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
Patent Number: NASA-CASE-LEW-12378-1
Patent Application Number: US-PATENT-APPL-SN-573029
Patent Number: US-PATENT-4,132,068
Accession Number
79N14097
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Patent
NASA-CASE-LEW-12378-1|US-PATENT-4,132,068
Patent Application
US-PATENT-APPL-SN-573029
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