Claims
- 1. In a gas turbine engine of a type having an axis and including an augmentor aft of an engine core, said augmentor including at least one substantially radially-extending fuel pipe and a substantially cylindrical diffuser wall, and a generally cylindrical bypass duct for conveying cooling air to said augmentor, said duct including an outer duct wall through which said fuel pipe extends radially inwardly towards said axis, a heat shield comprising:
- a hollow, elongate housing enclosing said fuel pipe substantially entirely along its length; and
- means for removably mounting said housing on said outer duct wall, said mounting means permitting removal of said housing by access from within said augmentor without requiring access from outside said outer duct wall.
- 2. The heat shield of claim 1 wherein said mounting means includes bolt means threaded substantially radially outwardly into said outer duct wall.
- 3. The shield of claim 2 wherein said mounting means includes a nose projecting outwardly from said housing; and said outer duct wall includes slot means for receiving said nose.
- 4. The heat shield of claim 3 wherein said housing is retained by engagement of said nose and said slot at a forward end of said housing and by said bolt means at an aft end of said housing.
- 5. The heat shield of claim 2 wherein said bolt means includes lug means shaped to engage said housing and clamp said housing against said outer duct wall when said bolt means is tightened, and wherein said housing includes a rearwardly-projecting flange shaped to be engaged by said lug means.
- 6. The heat shield of claim 5 wherein said outer duct wall includes a radially inwardly projecting lip; and said flange includes a recess shaped to receive said lip.
- 7. The heat shield of claim 1 wherein said housing includes a frustoconical portion at a radially outer end thereof; and said outer duct wall includes a complementary wedge-shaped recess; and said mounting means includes bolt means including a wedge-shaped cam at an end thereof, said cam being shaped to engage and lock said frustoconical portion against said wedge-shaped recess.
- 8. The heat shield of claim 7 wherein said bolt means includes a threaded boss, attached to said outer duct wall and including a guideway for said cam.
- 9. The heat shield of claim 1 wherein said housing includes diffuser flowpath segment means aligned substantially with said diffuser wall in said augmentor.
- 10. The heat shield of claim 9 wherein said diffuser flowpath segment means includes stiffener means for changing vibration characteristics of said diffuser flowpath segment means such that a natural frequency thereof is greater than tin engine operating speed.
- 11. The heat shield of claim 9 wherein said diffuser flowpath segment means includes opposing, axially-extending lateral edges, said lateral edges defining longitudinal slots, and said heat shield further comprises a plurality of said housings arranged in a spoke pattern such that said lateral edges of said diffuser flowpath segment means of adjacent housings abut each other; and said flowpath segment means includes spline seal segment means, mounted in said longitudinal slots, for effecting a seal between said diffuser flowpath segments.
- 12. The heat shield of claim 11 wherein said diffuser flowpath segment means includes a transverse edge, and a contiguous portion of said diffuser wall includes means for effecting a seal between said portion and said transverse edge.
- 13. The heat shield of claim 1 wherein said housing includes an opening, positioned between said outer duct wall and said diffuser wall, for receiving cooling air from said bypass duct and conveying said cooling air radially inwardly along said housing.
- 14. In a gas turbine engine of a type having an axis and including an augmentor aft of an engine core, said augmentor including at least one substantially radially-extending fuel pipe and a substantially cylindrical diffuser wall, and a generally cylindrical bypass duct for conveying cooling air to said augmentor, said duct including an outer duct wall through which said fuel pipe extends radially inwardly towards said axis, a heat shield comprising:
- a hollow, elongate housing enclosing said fuel pipe substantially entirely along its length, with a first section substantially enclosing said fuel pipe from said outer duct wall radially inwardly to about said diffuser wall, and a second section enclosing said fuel pipe substantially entirely along its length from said first section radially inwardly; and
- means for removably mounting said housing second section on one of said outer duct wall and said housing first section, said mounting means permitting removal of said housing second section by access from within said augmentor and without requiring access from outside said outer duct wall.
- 15. The heat shield of claim 14 wherein said housing first section comprises a substantially cylindrical strut; and said mounting means mounts said housing second section to said strut.
- 16. The heat shield of claim 15 wherein said mounting means includes a nose projecting outwardly from said housing second section; a slot is formed in an end of said strut for receiving said nose; bolt means threaded substantially radially outwardly into said strut; and said housing second section includes a flange for receiving said bolt means therethrough.
- 17. The heat shield of claim 14 further comprising a collar coupled to said housing and wherein said mounting means comprises a fastener attaching said housing second section to said outer duct wall through said collar.
- 18. The heat shield of claim 17 further comprising said housing first section integral with said housing second section.
- 19. The heat shield of claim 18 further comprising said housing first section including a mounting flange adapted to engage said outer duct wall and said fastener comprising an extended shank shoulder bolt including a shoulder for engaging said flange and clamping said flange to said outer duct wall.
- 20. The heat shield of claim 17 wherein said collar includes a recess for receiving said fastener out of a core gas flowpath defined by said cylindrical diffuser wall.
Parent Case Info
This application is a continuation-in-part application of U.S. patent application Ser. No. 07/816,000 for a Thrust Augmentor Heat Shield, filed on Jan. 2, 1992, now abandoned.
Government Interests
The government has rights in this invention pursuant to contract No. F33657-83C-0281 awarded by the Department of the Air Force and contract No. N00019-91C-0114 awarded by the Department of the Navy.
US Referenced Citations (23)
Foreign Referenced Citations (1)
Number |
Date |
Country |
2636378 |
Mar 1990 |
FRX |
Continuation in Parts (1)
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Number |
Date |
Country |
Parent |
816000 |
Jan 1992 |
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