V-blade and V-groove joint molded composite wear resistant edge protection

The invention relates to V-blade and V-groove joint molded composite wear resistant edge protection. An annular molded composite wear sleeve (40) is incorporated in an annular V-shaped groove (34) in a groove ring (64) using an epoxide or other adhesive. The wear sleeve (40) may include front and re...

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Bibliographische Detailangaben
Hauptverfasser:	RAVENHALL JOHN ANDREW, BLACKBURN MICHELLE ANN, DURCHHOLZ ANTHONY JOHN, SEHIDWICH, KHURSHED, HERNANDEZ LANGFORD CARLA PATRICIA, ROBINSON JOHN DAVID
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	The invention relates to V-blade and V-groove joint molded composite wear resistant edge protection. An annular molded composite wear sleeve (40) is incorporated in an annular V-shaped groove (34) in a groove ring (64) using an epoxide or other adhesive. The wear sleeve (40) may include front and rear sleeve walls (46, 48) extending away from the sleeve bottom (44) with front and rear sleeve obtuse angles (50, 52) and may include annular front and rear sleeve fillets (54, 56) between the sleeve bottom (44) and the front and rear sleeve walls (46, 48). The aft sleeve wall (48) may include aft flaps (60) conforming to an annular aft cone (62) on the groove ring (64). An aircraft gas turbine engine hood clamp mechanism (22) for clamping a clam shell hood (20) to a fan housing (26) includes a grooved ring (64) located on the fan housing (26) and a molded composite wear sleeve (40) incorporated in an annular V-shaped groove (34) in the grooved ring (64) with an epoxide or other adhesive. The annular V-shaped blade