US4508680A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method of manufacturing a rocket combustion chamber
Assignee: DIRECTOR OF NATIONAL AEROSPACE LABORATORY OF SCIENCE AND TECHNOLOGY AGENCY
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Filing: 1983-06-01
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Granted: 1985-04-02
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Expires: 2003-06-01
Abstract
Abstract The present invention is directed particularly to an improved method usingowder metallurgy for the manufacture of the grooved cooling wall of a liquid-propellant rocket combustion chamber. The surface of an inner cylinder constituting the cooling wall is formed with cooling grooves, and these grooves are densely filled up with a filler such as paraffin wax. Thereafter, metal powder which will provide an outer cylinder is compression-molded to a predetermined thickness around the inner cylinder. This metal powder is the same material as the material of the inner cylinder. After the paraffin wax which is the filler is evaporated and removed, the compression-molded metal powder body is sintered in a furnace. During this sintering heat treatment, the inner and outer cylinders are rigidly joined together by the sintering reaction between the atoms of the inner cylinder and the atoms of the metal powder.
Inventors
- 👤 Masayuki Niino
- 👤 Nobuyuki Yatsuyanagi
- 👤 Akinaga Kumakawa
- 👤 Akio Suzuki
- 👤 Hiromi Gomi
- 👤 Hiroshi Sakamoto
- 👤 Masaki Sasaki
- 👤 Yoshimichi Masuda
- 👤 Ryuzo Watanabe
- 👤 Junjiro Takekawa
- 👤 Etsuo Ohtsuki
- 👤 Terashi Isago
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-24 19:22
CPC Classifications
B; B22; B22F; B22F7/00; B22F7/06; B22F7/08; B22F5/00; B22F5/10; F; F02; F02K; F02K9/00; F02K9/42; F02K9/60; F02K9/62; F02K9/64
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
125 words
A method for manufacturing the cooling wall of a rocket combustion chamber, comprising the steps of: making an inner cylinder of a metallic material formed with grooves in the exterior surface thereof; filling up the grooves of said inner cylinder with a filler; compression-molding an outer cylinder on the inner cylinder by uniformly compressing metallic material powder of a predetermined thickness against the entire outermost surface of the inner cylinder having its grooves filled up with the filler; removing the filler from the grooves of said inner cylinder, whereby the grooves remain as empty cooling channels; and sintering the compression-molded powder to join the sintered outer cylinder material to the inner cylinder material and to form integral inner and outer cylinders with cooling channels therebetween.
Claim 2
Independent Claim
125 words
A method for manufacturing the cooling wall of a rocket combustion chamber, comprising the steps of: making an inner cylinder of a metallic material formed with grooves in the exterior surface thereof; filling up the grooves of said inner cylinder with a filler; compression-molding an outer cylinder on the inner cylinder by uniformly compressing metallic material powder of a predetermined thickness against the entire outermost surface of the inner cylinder having its grooves filled up with the filler; removing the filler from the grooves of said inner cylinder, whereby the grooves remain as empty cooling channels; and sintering the compression-molded powder to join the sintered outer cylinder material to the inner cylinder material and to form integral inner and outer cylinders with cooling channels therebetween.
Claim 3
Dependent Claim
20 words
A method according to claim 1, wherein said metallurgy powder is the same as the material of said inner cylinder.
Claim 4
Dependent Claim
16 words
A method according to claim 1, wherein said powder is electrolytic copper powder of 150-400 mesh.
Claim 5
Dependent Claim
12 words
A method according to claim 1, wherein said filler is paraffin wax.
Claim 6
Dependent Claim
21 words
A method according to claim 1, wherein said filler is mixed wax consisting of paraffin wax and ceramic powder added thereto.
Claim 7
Dependent Claim
56 words
A method according to claim 1, wherein the step of filling up said grooves with said filler comprises applying a compression pressure to said filler filling up said grooves to thereby make the fi11er dense, and making the surface of said filler densely filling up said grooves flush with the surface of the groove partition walls.
Claim 8
Dependent Claim
29 words
A method according to claim 6, wherein the step of sintering said metal powder is carried out in an atmosphere of hydrogen gas or rare gas or in vacuum.
Claim 9
Dependent Claim
45 words
A method according to claim 4, wherein the step of removing the filler comprises evaporating and removing said paraffin wax filled up in the groove by heating it at an evaporating temperature of wax prior to the sintering of said powder at a sintering temperature.
Claim 10
Dependent Claim
46 words
A method according to claim 5, wherein the step of removing the filler comprises evaporating and removing said mixed wax by heating it at an evaporating temperature of wax and washing the added ceramic powder, prior to the sintering of said powder at a sintering temperature.
References Cited (Backward Citations)
GB491416A
Cited
SU149226A1
Cited
FR1602258A
Cited
US3531848A
Cited
US3549357A
Cited
US4431449A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-04-01 | 1988-10-01 | 1989-04-02 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-04-01 | 1992-10-01 | 1993-04-02 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-04-01 | 1996-10-01 | 1997-04-02 | $7700.00 | Window Closed / Lapsed |