BAFFLE SEAL FOR GAS TURBINE ENGINE REVERSE THRUST APPARATUS

PROBLEM TO BE SOLVED: To provide a baffle seal for a reverse thrust apparatus of a gas turbine engine. SOLUTION: The baffle seal 50 includes a seal body 56 of an elastic material. The seal body 56 has a comparatively flat center 64 equipped with a front face and a rear face facing each other. A prot...

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Hauptverfasser:	TSOU CHI-LING MICHAEL, HOLDREN CARL FRANCIS, LENAHAN DEAN T, BAILEY WILLIAM ANDREW
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a baffle seal for a reverse thrust apparatus of a gas turbine engine. SOLUTION: The baffle seal 50 includes a seal body 56 of an elastic material. The seal body 56 has a comparatively flat center 64 equipped with a front face and a rear face facing each other. A protuberance seal ring rim 70 is extended at least partially around the center 64. An outer circumference of the seal ring rim 70 is extended over the outer circumference of the center 64 to form an exposed seal surface 74. COPYRIGHT: (C)2010,JPO&INPIT