V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR EDGE GUARD

V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR EDGE GUARD

An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and...

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Hauptverfasser: HERNANDEZ LANGFORD, CARLA PATRICIA, ROBINSON, JORDAN DANIEL, SZEHIDEWICZ, KAMIL, DURCHHOLZ, ANTHONY JOHN, RAVENHALL, JOHN ANDREW, BLACKBURN, MICHELLE ANN
Format: Patent
Sprache:eng ; fre
Schlagworte:
BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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creator HERNANDEZ LANGFORD, CARLA PATRICIA
ROBINSON, JORDAN DANIEL
SZEHIDEWICZ, KAMIL
DURCHHOLZ, ANTHONY JOHN
RAVENHALL, JOHN ANDREW
BLACKBURN, MICHELLE ANN
description An annular molded composite wear sleeve (40) is bonded with epoxy or other bonding agent in an annular V-groove (34) in a groove ring (64). Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). Annular V-blade (30) is on clamshell cowl (20) rotatable to insert annular V-blade (30) in annular V-groove (34).
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Wear sleeve (40) may include forward and aft sleeve walls (46, 48) extending at forward and aft sleeve obtuse angles (50, 52) away from a sleeve bottom (44) and may include annular forward and aft sleeve fillets (54, 56) between sleeve bottom (44) and forward and aft sleeve walls (46, 48). Aft sleeve wall (48) may include an aft flap (60) compliant with an annular aft taper (62) on groove ring (64). An aircraft gas turbine engine cowl clamping mechanism (22) for clamping a clamshell cowl (20) to a fan casing (26) includes groove ring (64) on a fan casing (26) and molded composite wear sleeve (40) bonded with epoxy or other bonding agent in annular V-groove (34) in groove ring (64). 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subjects BLASTING
COMBUSTION ENGINES
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
JET-PROPULSION PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
title V-BLADE AND V-GROOVE JOINT MOLDED COMPOSITE WEAR EDGE GUARD
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