GB937695A - Process for the manufacture of liquid cooled combustion chambers for rockets - Google Patents
Process for the manufacture of liquid cooled combustion chambers for rocketsInfo
- Publication number
- GB937695A GB937695A GB4604961A GB4604961A GB937695A GB 937695 A GB937695 A GB 937695A GB 4604961 A GB4604961 A GB 4604961A GB 4604961 A GB4604961 A GB 4604961A GB 937695 A GB937695 A GB 937695A
- Authority
- GB
- United Kingdom
- Prior art keywords
- liquid cooled
- bolkow
- cooled combustion
- rockets
- manufacture
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B21—MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D—WORKING OR PROCESSING OF SHEET METAL OR METAL TUBES, RODS OR PROFILES WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
- B21D53/00—Making other particular articles
- B21D53/02—Making other particular articles heat exchangers or parts thereof, e.g. radiators, condensers fins, headers
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Testing Of Engines (AREA)
Abstract
937,695. Generating combustion products under pressure. L. BOLKOW, [trading as BOLKOW ENTWICKLUNGEN KOMM.- GES.]. Dec. 22, 1961, No. 46049/61. Class 51(1). [Also in Groups XXII and XXVI] A liquid cooled combustion chamber such as for a liquid fuel rocket motor comprises an inner and an outer tube longitudinally welded together at spaced intervals, the composite tube being formed into a thrust nozzle and the internal passages between the welds expanded so as to form cooling chambers. The chamber is subsequently wound with high tensile tape 19 or armour wire. A third tube 26 may be welded to the assembly to form additional cooling passages 29.
Priority Applications (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB55024A DE1135405B (en) | 1959-10-02 | 1959-10-02 | Process for producing liquid-cooled rocket combustion chambers |
GB4604961A GB937695A (en) | 1961-12-22 | 1961-12-22 | Process for the manufacture of liquid cooled combustion chambers for rockets |
US169815A US3235947A (en) | 1961-12-22 | 1962-01-30 | Method for making a combustion chamber |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4604961A GB937695A (en) | 1961-12-22 | 1961-12-22 | Process for the manufacture of liquid cooled combustion chambers for rockets |
Publications (1)
Publication Number | Publication Date |
---|---|
GB937695A true GB937695A (en) | 1963-09-25 |
Family
ID=10439650
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4604961A Expired GB937695A (en) | 1959-10-02 | 1961-12-22 | Process for the manufacture of liquid cooled combustion chambers for rockets |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB937695A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3208132A (en) * | 1962-04-13 | 1965-09-28 | William J D Escher | Method of making a multi-walled chamber |
US5233755A (en) * | 1990-11-30 | 1993-08-10 | Societe Europeenne De Propulsion | Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber obtained by the method |
CN109967871A (en) * | 2019-03-29 | 2019-07-05 | 北京航空航天大学 | The processing tool of miniature gas turbine combustion chamber |
CN111375690A (en) * | 2018-12-27 | 2020-07-07 | 航天海鹰(哈尔滨)钛业有限公司 | Hot press forming method for titanium alloy variable-curvature bidirectional stress structure sheet metal part |
CN116038171A (en) * | 2023-03-30 | 2023-05-02 | 北京星河动力装备科技有限公司 | Regenerative cooling thrust chamber and manufacturing method thereof |
-
1961
- 1961-12-22 GB GB4604961A patent/GB937695A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3208132A (en) * | 1962-04-13 | 1965-09-28 | William J D Escher | Method of making a multi-walled chamber |
US5233755A (en) * | 1990-11-30 | 1993-08-10 | Societe Europeenne De Propulsion | Method of manufacturing the wall of a combustion chamber, in particular for a rocket engine, and a combustion chamber obtained by the method |
CN111375690A (en) * | 2018-12-27 | 2020-07-07 | 航天海鹰(哈尔滨)钛业有限公司 | Hot press forming method for titanium alloy variable-curvature bidirectional stress structure sheet metal part |
CN111375690B (en) * | 2018-12-27 | 2022-04-12 | 航天海鹰(哈尔滨)钛业有限公司 | Hot press forming method for titanium alloy variable-curvature bidirectional stress structure sheet metal part |
CN109967871A (en) * | 2019-03-29 | 2019-07-05 | 北京航空航天大学 | The processing tool of miniature gas turbine combustion chamber |
CN116038171A (en) * | 2023-03-30 | 2023-05-02 | 北京星河动力装备科技有限公司 | Regenerative cooling thrust chamber and manufacturing method thereof |
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