Patent US4037998A successfully refreshed from Google Patents.
US4037998A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Rotary engine cooling
Assignee: Caterpillar Inc
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Filing: 1975-11-03
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Granted: 1977-07-26
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Expires: 1995-11-03
Abstract
Abstract An improved rotary engine including a housing having interior walls defining an operating chamber with a rotor mounted for movement therein. Within the chamber is a thin layer of wear resistant metal which is located to be sealingly engaged by the rotor as the rotor moves within the chamber and a backing is secured to the thin layer in good heat transfer relation and interposed between the same and the housing for transmitting pressure applied to the thin layer to the housing. The backing is formed of a metal having high thermal conductivity and is provided with a plurality of relatively closely spaced coolant passages to provide an improved cooling structure for the engine to thereby extend its life.
Inventors
- 👤 Alexander Goloff
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-28 11:24
CPC Classifications
F; F02; F02B; F02B55/00; F02B55/08; F02B55/10; F01; F01C; F01C21/00; F01C21/06; Y; Y02; Y02T; Y02T10/00; Y02T10/10; Y02T10/12
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
137 words
A rotary engine comprising: a. a housing having interior walls defining an operating chamber; b. a rotor mounted for movement in said chamber; c. a thin layer of wear resistant metal within said chamber and located to be sealingly engaged by said rotor as said rotor moves within said chamber; and d. a backing for said thin layer interposed in sandwiched relation between said thin layer and said housing for transmitting pressure applied to said thin layer to said housing, said backing being formed of a metal having high thermal conductivity and being provided with a plurality of relatively closely spaced, elongated, coolant passages, said backing including a plurality of protrusions extending into said passages to introduce turbulence in a coolant passing through said passages, said passages having a substantially uniform cross sectional area along their length.
Claim 2
Dependent Claim
137 words
A rotary engine comprising: a. a housing having interior walls defining an operating chamber; b. a rotor mounted for movement in said chamber; c. a thin layer of wear resistant metal within said chamber and located to be sealingly engaged by said rotor as said rotor moves within said chamber; and d. a backing for said thin layer interposed in sandwiched relation between said thin layer and said housing for transmitting pressure applied to said thin layer to said housing, said backing being formed of a metal having high thermal conductivity and being provided with a plurality of relatively closely spaced, elongated, coolant passages, said backing including a plurality of protrusions extending into said passages to introduce turbulence in a coolant passing through said passages, said passages having a substantially uniform cross sectional area along their length.
Claim 3
Dependent Claim
40 words
The rotary engine of claim 1 wherein said passages are open along their length to one side of said backing, one of said thin layer and said housing abutting said backing to substantially close said one side of said passages.
Claim 4
Dependent Claim
27 words
A rotary engine according to claim 1 wherein said metal having a high thermal conductivity is selected from the group consisting of copper, brass, aluminum and magnesium.
Claim 5
Dependent Claim
20 words
The rotary engine of claim 1 wherein said thin layer is bonded to said backing in good heat transfer relation.
Claim 6
Dependent Claim
34 words
The rotary engine of claim 4 wherein said housing has opposed side walls and a radially outer peripheral wall; and said thin layer and said backing extend at least partially about said peripheral wall.
Claim 7
Dependent Claim
28 words
The rotary engine of claim 5 wherein said thin layer and said backing extend entirely about said peripheral wall; and said passages are elongated about said peripheral wall.
Claim 8
Dependent Claim
32 words
The rotary engine of claim 4 wherein said housing has opposed side walls and a radially outer peripheral wall; and said thin layer and said backing are located on said side walls.
Claim 9
Dependent Claim
34 words
The rotary engine of claim 7 wherein said side walls are separate from said peripheral wall and said thin layer and said backing are formed to define a removable liner for said operating chamber.
Claim 10
Dependent Claim
47 words
The rotary engine of claim 8 wherein said rotor has generally planar side surfaces facing said side walls and said removable liner defined by said thin layer and said backing is pre-bowed such that said thin layer opposite from said backing is slightly concave prior to assembly.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1980-07-25 | 1981-01-24 | 1981-07-26 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1984-07-25 | 1985-01-24 | 1985-07-26 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1988-07-25 | 1989-01-24 | 1989-07-26 | $7700.00 | Window Closed / Lapsed |