发明名称 SYSTEME DE POST-COMBUSTION
摘要 A new and improved gas turbine engine augmentor including a liner having a film-coolable first portion joined to a convection-coolable second portion is disclosed. A cooling gas, such as fan bypass air, is channeled to the liner for film cooling the first portion and providing a residual cooling film to the second portion. The second portion is also convection coolable by air passing over an outer surface thereof. In a particular embodiment of the invention, the augmentor liner also includes a screech portion disposed at an upstream end of the first portion and downstream of a flameholder. The screech portion includes a substantially imperforate outer wall and an inner wall spaced therefrom which define a manifold therebetween. The inner wall includes a plurality of apertures in flow communication with the combustion zone. The manifold and apertures are effective for suppressing screech while substantially preventing the leakage of cooling air therethrough.
申请公布号 FR2574859(B1) 申请公布日期 1992.11.06
申请号 FR19850018684 申请日期 1985.12.17
申请人 GENERAL ELECTRIC CY 发明人 JOHN WILLIAM VDOVIAK ET CHESTER JOSEPH LAMANDO, JR.
分类号 F02K3/08;F23R3/00;F23R3/06;F23R3/20 主分类号 F02K3/08
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