US3968834A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Heat exchanger mounting for a turbine engine
Assignee: Caterpillar Inc
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Filing: 1975-02-07
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Granted: 1976-07-13
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Expires: 1995-02-07
Abstract
Abstract A heat exchanger core made up of a loose stack of heat exchange sheets is surrounded by a support frame which holds the sheets against separation. One end of the support frame is mounted on the engine body and restrained against vertical, fore-and-aft and sidewise movement relative to the engine body. The other end of the support frame is mounted on the engine body by a double pivot link assembly which restrains that end against vertical and sidewise movement but allows fore-and-aft movement. A simple expansion bellows joins the high-pressure air inlet of the heat exchanger to the engine body. A simple expansion bellows may be used to join either or both of the high-pressure air outlet and low-pressure hot exhaust gas inlet of the heat exchanger to the engine body.
Inventors
- 👤 Ervin E. Mangus
- 👤 Richard W. Kizer
- 👤 D. Craig Young
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 20:30
CPC Classifications
F; F28; F28F; F28F9/00; F28F9/001; F02; F02C; F02C7/00; F02C7/08; F28D; F28D9/00; F28F9/007; F28F9/0075; F28F2265/00; F28F2265/26; Y; Y10; Y10S; Y10S165/00; Y10S165/051; Y10S165/071
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
267 words
In a heat exchanger mounting system for a turbine engine: a. a heat exchanger unit comprising an elongated core having opposed upper and lower surfaces, opposed end members and opposed side surfaces, an air-in manifold integrally connected to the upper surface of said core and an air-out manifold integrally connected to the lower surface of said core, b. said heat exchanger unit further comprising a support frame surrounding the end members and side surfaces of said core, said support frame having rigid end beams and side members extending between the end beams and secured thereto; c. said heat exchanger unit further comprising means for supporting said core in said frame against upward or downward movement relative thereto; d. said heat exchanger unit further comprising a gas-in manifold connected thereto, e. an engine body having air-in, air-out and gas-in passages therein, f. rigid link means pivoted to said engine body and to one end beam of said support frame for supporting said end beam spaced a substantially fixed distance from said engine body and for restraining said end beam against sidewise movement while allowing endwise movement of said end beam relative to said engine body, g. means for supporting the other end beam of said support frame spaced a substantially fixed distance from said engine body and for restraining said other end beam against endwise and sidewise movement relative to said engine body, h. conduit means, including an expansion bellows therein, connecting and communicating said air-in manifold to and with said air-in passage, i. conduit means connecting and communicating said gas-in manifold to and with said gas-in passage.
Claim 2
Dependent Claim
267 words
In a heat exchanger mounting system for a turbine engine: a. a heat exchanger unit comprising an elongated core having opposed upper and lower surfaces, opposed end members and opposed side surfaces, an air-in manifold integrally connected to the upper surface of said core and an air-out manifold integrally connected to the lower surface of said core, b. said heat exchanger unit further comprising a support frame surrounding the end members and side surfaces of said core, said support frame having rigid end beams and side members extending between the end beams and secured thereto; c. said heat exchanger unit further comprising means for supporting said core in said frame against upward or downward movement relative thereto; d. said heat exchanger unit further comprising a gas-in manifold connected thereto, e. an engine body having air-in, air-out and gas-in passages therein, f. rigid link means pivoted to said engine body and to one end beam of said support frame for supporting said end beam spaced a substantially fixed distance from said engine body and for restraining said end beam against sidewise movement while allowing endwise movement of said end beam relative to said engine body, g. means for supporting the other end beam of said support frame spaced a substantially fixed distance from said engine body and for restraining said other end beam against endwise and sidewise movement relative to said engine body, h. conduit means, including an expansion bellows therein, connecting and communicating said air-in manifold to and with said air-in passage, i. conduit means connecting and communicating said gas-in manifold to and with said gas-in passage.
Claim 3
Dependent Claim
32 words
A combination as set forth in claim 1, wherein said means (c) comprises projecting bosses and boss-receiving sockets on adjacent end beams of said support frame and end members of said core.
Claim 4
Dependent Claim
30 words
A combination as set forth in claim 1 and further including thermal insulation means disposed between the end beams of said support frame and the end members of said core.
Claim 5
Dependent Claim
28 words
A combination as set forth in claim 1 wherein said means (g) comprises a rigid conduit connecting and communicating said air-out conduit to and with said air-out passage.
Claim 6
Dependent Claim
17 words
A combination as set forth in claim 1, wherein said means (i) includes an expansion bellows therein.
Claim 7
Dependent Claim
26 words
A combination as set forth in claim 1, and further including: j. conduit means connecting and communicating said air-out conduit to and with said air-out passage.
Claim 8
Dependent Claim
17 words
A combination as set forth in claim 6, wherein said means (j) includes an expansion bellows therein.
Claim 9
Dependent Claim
21 words
A combination as set forth in claim 6, wherein each of said means (i) and (j) includes an expansion bellows therein.
Claim 10
Dependent Claim
115 words
A combination as set forth in claim 7 wherein said means (g) comprises a first rigid link means pivoted to said engine body and pivoted relative to said other frame end beam for restraining movement of said other frame end beam towards and away from said engine body while allowing endwise movement of said other frame end beam relative to said engine body and a second rigid link means pivoted to said engine body and pivoted to said heat exchanger unit for restraining endwise movement of said other frame end beam relative to said engine body while allowing upward and downward movement of said other frame end beam towards and away from said engine body.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1979-07-13 | 1980-01-12 | 1980-07-13 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-07-13 | 1984-01-12 | 1984-07-13 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-07-13 | 1988-01-12 | 1988-07-13 | $7700.00 | Window Closed / Lapsed |