GB578007A - Improvements in combustion chamber linings - Google Patents

Improvements in combustion chamber linings

Info

Publication number
GB578007A
GB578007A GB1440041A GB1440041A GB578007A GB 578007 A GB578007 A GB 578007A GB 1440041 A GB1440041 A GB 1440041A GB 1440041 A GB1440041 A GB 1440041A GB 578007 A GB578007 A GB 578007A
Authority
GB
United Kingdom
Prior art keywords
combustion chamber
segments
rings
expansion nozzle
chamber linings
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
GB1440041A
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.)
Asiatic Petroleum Co Ltd
Original Assignee
Asiatic Petroleum Co Ltd
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 Asiatic Petroleum Co Ltd filed Critical Asiatic Petroleum Co Ltd
Priority to GB1440041A priority Critical patent/GB578007A/en
Publication of GB578007A publication Critical patent/GB578007A/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
    • 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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Portable Nailing Machines And Staplers (AREA)

Abstract

578,007. Combustion chambers. ASIATIC PETROLEUM CO., Ltd., LUBBOCK, I., BECKER, L. S., and GOLLIN, G. J. Nov. 7, 1941, No. 14400. [Class 51 (i)] A combustion chamber having an expansion nozzle 2 which operates at high temperatures and pressures, as in jet propulsion apparatus, is provided with a refractory lining, preferably of graphite, divided transversely into rings 3 of comparatively short lengths, designed so as not to be subjected to excessive tensile stress in operation, either by dividing each ring radially into segments, or by shrinking the metal shell 1 around the rings. Radial gaps may be provided between the segments. An additional interior lining 5 may be provided at the throat of the expansion nozzle, and a retaining-plate 6 fitted at the open end.
GB1440041A 1941-11-07 1941-11-07 Improvements in combustion chamber linings Expired GB578007A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1440041A GB578007A (en) 1941-11-07 1941-11-07 Improvements in combustion chamber linings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1440041A GB578007A (en) 1941-11-07 1941-11-07 Improvements in combustion chamber linings

Publications (1)

Publication Number Publication Date
GB578007A true GB578007A (en) 1946-06-12

Family

ID=10040514

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1440041A Expired GB578007A (en) 1941-11-07 1941-11-07 Improvements in combustion chamber linings

Country Status (1)

Country Link
GB (1) GB578007A (en)

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699036A (en) * 1950-12-09 1955-01-11 Carborundum Co Ceramic lined, lightweight rocket motor structure and like device
US2705399A (en) * 1951-12-06 1955-04-05 Armstrong Siddeley Motors Ltd Combustion chambers
DE959423C (en) * 1951-03-21 1957-03-07 Carborundum Co Device for burning liquid and solid fuels, especially in jet engines or the like.
DE1042971B (en) * 1954-01-02 1958-11-06 Carborundum Co Device for the conduction and directional release of gases, especially for rocket engines
US2987874A (en) * 1954-03-15 1961-06-13 Carborundum Co Ceramic lined, light weight rocket motor nozzles and like devices
US3282421A (en) * 1961-12-21 1966-11-01 Gen Motors Corp Reaction motor exhaust nozzle incorporating a fusible coolant
US3712061A (en) * 1966-11-02 1973-01-23 Us Navy Vortex baffle

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2699036A (en) * 1950-12-09 1955-01-11 Carborundum Co Ceramic lined, lightweight rocket motor structure and like device
DE959423C (en) * 1951-03-21 1957-03-07 Carborundum Co Device for burning liquid and solid fuels, especially in jet engines or the like.
US2705399A (en) * 1951-12-06 1955-04-05 Armstrong Siddeley Motors Ltd Combustion chambers
DE1042971B (en) * 1954-01-02 1958-11-06 Carborundum Co Device for the conduction and directional release of gases, especially for rocket engines
US2987874A (en) * 1954-03-15 1961-06-13 Carborundum Co Ceramic lined, light weight rocket motor nozzles and like devices
US3282421A (en) * 1961-12-21 1966-11-01 Gen Motors Corp Reaction motor exhaust nozzle incorporating a fusible coolant
US3712061A (en) * 1966-11-02 1973-01-23 Us Navy Vortex baffle

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