Claims
- 1. A cooling arrangement for the trailing edge of a nozzle flap comprising a structural honeycomb planular support plate;
- a nozzle liner spaced from said support plate and forming a coolant plenum therebetween;
- a nozzle trailing edge liner secured to said nozzle liner, extending outwardly therefrom and covering the edges of said coolant plenum and said support plate;
- a baffle supported from one of said liners and sealing biased against said support plate, said baffle forming a coolant volume between the baffle and said edge liner; and
- means for passing coolant from said coolant plenum through said coolant volume in contact with said edge liner for cooling said edge liner.
- 2. The cooling arrangement that is in claim 1:
- said means for passing coolant comprising a plurality of impingement holes in said baffle for directing coolant through said baffle against said edge liner.
- 3. A cooling arrangment as in claim 2:
- said means for passing coolant also including a plurality of holes through said edge liner.
- 4. A cooling arrangment as in claim 2:
- said means for passing coolant also including an opening between said edge liner and said support plate.
- 5. A cooling arrangement as in claim 1:
- said nozzle liner fixedly secured to said support plate at a location remote from said edge liner;
- an abutting seal between said edge liner and said support plate;
- said seal abutting in a direction parallel to the expansion of said nozzle liner from the fixed support, whereby expansion of the liner relative to the support structure opens said abutting seal permitting cooling air to flow therethrough.
Government Interests
The Government has rights in this invention pursuant to Contract No. F33615-84-C-3015 awarded by the Department of the Air Force.
US Referenced Citations (7)