AIRCRAFT GAS TURBINE ENGINE Russian patent published in 2010 - IPC F02C7/04 B64D33/02 F02K3/06 

Abstract RU 2382218 C1

FIELD: engines and pumps.

SUBSTANCE: proposed engine comprises air intake (2) with cylindrical inner wall and fan (3) with cylindrical casing and air fed from said air intake. Air intake inner cylindrical wall and fan casing form an integral cylindrical component (30) made from composite material consisting of resin and fibrous filler. Said composite material can be based on carbon fiber. Aforesaid cylindrical component is jointed, via flange (32) and bolts, to outer hood (22) of fan duct (23). Rear end (30R) of cylindrical component (30) represents a homogeneous member. Flange (32) is attached to said rear end (30R) and fixed thereon.

EFFECT: ruling out lamination of composite material.

2 cl, 5 dwg

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RU 2 382 218 C1

Authors

Port Alen

Gant'E Fabris

Shelen Frederik

Oberle Patrik

Dates

2010-02-20Published

2007-07-04Filed