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US4083180A Expired / Lapsed US ⏱️ 0.0 years remaining

Gas turbine engine internal insulation

Assignee: Caterpillar Inc
•
Filing: 1976-10-01
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Granted: 1978-04-11
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Expires: 1996-10-01
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Abstract

Abstract The invention is concerned with an improvement in a modular gas turbine engine assembly comprising a tubular case, a gasifier module detachably attachable with a first end thereof adjacent a first end of said case and a power output module detachably attachable with a first end thereof adjacent a second end of said case, said case and said modules defining a partially walled off combustion-ducting section within said engine. The improvement comprises a plurality of individually replaceable insulation packs which provide heat insulation between the combustion-ducting section walls and each of said case, said gasifier module and said power output module. In another sense the invention comprises an improved individually replaceable insulating pack comprising a high temperature resistant metallic sheet having a porous insulation blanket and including a fine mesh of wire covering the surface of the blanket which is not adjacent to the sheet and holding the blanket against the sheet.

Inventors

  • 👤 Leroy R. Thompson
  • 👤 Edward G. Meints

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-04 22:15
CPC Classifications
F; F02; F02C; F02C7/00; F02C7/24

Claims Analysis

Total Claims: 6
Claim 1
Independent Claim 190 words
In a modular gas turbine engine assembly comprising a tubular case, a gasifier module detachably attachable with a first end thereof adjacent a first end of said case and a power output module detachably attachable at a first end thereof adjacent a second end of said case, said case and said modules defining a partially walled off combustion-ducting section within said engine, an improvement comprising a plurality of individually replaceable insulation packs providing heat insulation between said combustion-ducting section and each of said case, said gasifier module and said power output module, each of said packs comprising a high temperature resistant metallic sheet having held against a first side thereof a porous insulation blanket with a fine mesh of metal attached to said sheet and covering the surface of said blanket not abutted to said sheet and wherein said blanket is abutted against a wall portion of said combustion-ducting section with said sheet being spaced therefrom by the thickness of said blanket, said blanket not being bonded to said sheet by a bonding agent and a binder not being used in said blanket to bind said fibers to one another.
Claim 2
Dependent Claim 190 words
In a modular gas turbine engine assembly comprising a tubular case, a gasifier module detachably attachable with a first end thereof adjacent a first end of said case and a power output module detachably attachable at a first end thereof adjacent a second end of said case, said case and said modules defining a partially walled off combustion-ducting section within said engine, an improvement comprising a plurality of individually replaceable insulation packs providing heat insulation between said combustion-ducting section and each of said case, said gasifier module and said power output module, each of said packs comprising a high temperature resistant metallic sheet having held against a first side thereof a porous insulation blanket with a fine mesh of metal attached to said sheet and covering the surface of said blanket not abutted to said sheet and wherein said blanket is abutted against a wall portion of said combustion-ducting section with said sheet being spaced therefrom by the thickness of said blanket, said blanket not being bonded to said sheet by a bonding agent and a binder not being used in said blanket to bind said fibers to one another.
Claim 3
Dependent Claim 15 words
An improvement as in claim 1, wherein each of said blankets comprise interlaced ceramic fibers.
Claim 4
Dependent Claim 14 words
An improvement as in claim 2, wherein said fibers comprise an aluminosilicate fire clay.
Claim 5
Dependent Claim 12 words
An improvement as in claim 3, wherein said case comprises carbon steel.
Claim 6
Dependent Claim 12 words
An improvement as in claim 1, wherein said sheet comprises spring metal.

References Cited (Backward Citations)

US2625013A Cited
US3167914A Cited
US3196611A Cited
US3321179A Cited
US3647606A Cited
US3823553A Cited
US3842595A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1981-04-10 1981-10-10 1982-04-11 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1985-04-10 1985-10-10 1986-04-11 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1989-04-10 1989-10-10 1990-04-11 $7700.00 Window Closed / Lapsed

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