发明名称 Nozzle seal assembly with removable baseplate
摘要 A thermal shield and support structure assembly for a gas turbine engine is disclosed wherein the thermal shield can be removed while the support structure is still mounted in the engine. The thermal shield in the form of a divergent seal baseplate and the support structure is particularly useful for divergent seals and provides a removable baseplate having at least two hooks disposed on the back side of the baseplate. The hooks have axially facing openings, preferably open in the forward facing direction and are operable to engage transversely extending pins on the frame of the support structure. An axial retaining means to prevent the hooks from disengaging from the pins may also be used which, in one embodiment, provides a lug having a first aperture and extending away from the back side of the baseplate to engage a clevis having two arms having second apertures alignable with the lug's aperture and a bolt or other fastening means disposed through the apertures.
申请公布号 US5584173(A) 申请公布日期 1996.12.17
申请号 US19940334070 申请日期 1994.09.01
申请人 GENERAL ELECTRIC COMPANY 发明人 LYBARGER, MICHAEL A.
分类号 F02C7/20;F02C7/24;F02K1/12;F02K1/80;F02K1/82;(IPC1-7):F02C7/20 主分类号 F02C7/20
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