Convergent flap bearing with integral hold-down device

An exhaust nozzle of the type utilized with high performance supersonic aircraft is disclosed. The exhaust nozzle is variable between convergent and convergent/divergent geometries, as well as in aperture size. A bearing guiding segments of the nozzle is held within a roller track by an integral hol...

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Bibliographic Details
Main Author HONEYCUTT, JR.; FRED L
Format Patent
LanguageEnglish
Published 15.11.1988
Edition4
Subjects
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
INDEXING SCHEME FOR ASPECTS RELATING TONON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES ORJET-PROPULSION PLANTS
INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUSSUBCLASSES OF CLASSES F01-F04
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:An exhaust nozzle of the type utilized with high performance supersonic aircraft is disclosed. The exhaust nozzle is variable between convergent and convergent/divergent geometries, as well as in aperture size. A bearing guiding segments of the nozzle is held within a roller track by an integral hold-down bracket.
Bibliography:Application Number: US19870077262