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GB864668A - Improvements relating to rocket combustion chambers - Google Patents

Improvements relating to rocket combustion chambers

Info

Publication number
GB864668A
GB864668A GB14632/59A GB1463259A GB864668A GB 864668 A GB864668 A GB 864668A GB 14632/59 A GB14632/59 A GB 14632/59A GB 1463259 A GB1463259 A GB 1463259A GB 864668 A GB864668 A GB 864668A
Authority
GB
United Kingdom
Prior art keywords
strips
wall
rings
rocket combustion
combustion chambers
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
GB14632/59A
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.)
Daimler Benz AG
Original Assignee
Daimler Benz AG
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
Application filed by Daimler Benz AG filed Critical Daimler Benz AG
Publication of GB864668A publication Critical patent/GB864668A/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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)

Abstract

864,668. Self-propelled missiles. DAIMLERBENZ A. G. April 29, 1959 [May 8, 1958], No. 14632/59. Class 9(2). [Also in Groups XII and XXVI] A rocket combustion chamber 1 and nozzle is constructed by assembling together T-sectioned strips 4 to form an inner wall 2 and connecting to this a cooling jacket 3. The webs 5 of the strips 4 have castellated edges forming projections 6, which engage in slots 8 of frusto-conical rings 9 placed over the wall 2 to form the jacket 3, the spaces between the webs 5 being used as ducts for a coolant. The strips 4 are welded together to form a closed inner wall and the rings 9 are also welded together. The projections 6 are welded in the slots. Expansion joints may be provided between the rings and/or between the strips 4.
GB14632/59A 1958-05-08 1959-04-29 Improvements relating to rocket combustion chambers Expired GB864668A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE864668X 1958-05-08

Publications (1)

Publication Number Publication Date
GB864668A true GB864668A (en) 1961-04-06

Family

ID=6801702

Family Applications (1)

Application Number Title Priority Date Filing Date
GB14632/59A Expired GB864668A (en) 1958-05-08 1959-04-29 Improvements relating to rocket combustion chambers

Country Status (1)

Country Link
GB (1) GB864668A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113894453A (en) * 2021-09-15 2022-01-07 蓝箭航天空间科技股份有限公司 Method for processing combustion chamber structure of dissimilar metal and combustion chamber

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113894453A (en) * 2021-09-15 2022-01-07 蓝箭航天空间科技股份有限公司 Method for processing combustion chamber structure of dissimilar metal and combustion chamber
CN113894453B (en) * 2021-09-15 2022-06-17 蓝箭航天空间科技股份有限公司 Processing method and combustion chamber of a dissimilar metal combustion chamber structure

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