GB937695A - Process for the manufacture of liquid cooled combustion chambers for rockets - Google Patents

Process for the manufacture of liquid cooled combustion chambers for rockets

Info

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
Application number
GB4604961A
Inventor
Just Sohlemann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Priority to DEB55024A priority Critical patent/DE1135405B/en
Application filed by Individual filed Critical Individual
Priority to GB4604961A priority patent/GB937695A/en
Priority to US169815A priority patent/US3235947A/en
Publication of GB937695A publication Critical patent/GB937695A/en
Expired legal-status Critical Current

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.
GB4604961A 1959-10-02 1961-12-22 Process for the manufacture of liquid cooled combustion chambers for rockets Expired GB937695A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (6)

* Cited by examiner, † Cited by third party
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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