GB1074557A - Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber - Google Patents

Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber

Info

Publication number
GB1074557A
GB1074557A GB3077765A GB3077765A GB1074557A GB 1074557 A GB1074557 A GB 1074557A GB 3077765 A GB3077765 A GB 3077765A GB 3077765 A GB3077765 A GB 3077765A GB 1074557 A GB1074557 A GB 1074557A
Authority
GB
United Kingdom
Prior art keywords
oxidant
fuel
controlling
combustion chamber
flow ratio
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
GB3077765A
Inventor
Reginald Dennis Lowe
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines 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 Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Priority to GB3077765A priority Critical patent/GB1074557A/en
Priority to DE19661476949 priority patent/DE1476949A1/en
Publication of GB1074557A publication Critical patent/GB1074557A/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
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F02K9/58—Propellant feed valves
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D11/00—Control of flow ratio
    • G05D11/003—Control of flow ratio using interconnected flow control elements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Devices For Medical Bathing And Washing (AREA)
  • Testing Of Engines (AREA)

Abstract

1,074,557. Rocket propulsion. BRISTOL SIDDELEY ENGINES Ltd. July 15, 1966 [July 20, 1965], No. 30777/65. Addition to 899, 681. Heading F1J. [Also in Divisions F2 and G3] A modification of the rocket motor oxidant fuel ratio control device described in Specification 899, 681 comprises replacement of the rigid connection between the pistons by a loose abutment rod against which the two pistons are urged by the pressure difference. The piston seals may be omitted and a limited leakage allowed between opposite sides of each piston.
GB3077765A 1965-07-20 1965-07-20 Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber Expired GB1074557A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB3077765A GB1074557A (en) 1965-07-20 1965-07-20 Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber
DE19661476949 DE1476949A1 (en) 1965-07-20 1966-07-19 Device for regulating the quantity ratio of fuel and oxygen carrier for combustion chambers

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3077765A GB1074557A (en) 1965-07-20 1965-07-20 Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber

Publications (1)

Publication Number Publication Date
GB1074557A true GB1074557A (en) 1967-07-05

Family

ID=10312985

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3077765A Expired GB1074557A (en) 1965-07-20 1965-07-20 Apparatus for controlling the flow ratio of oxidant and fuel to a combustion chamber

Country Status (2)

Country Link
DE (1) DE1476949A1 (en)
GB (1) GB1074557A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117703600A (en) * 2024-02-18 2024-03-15 中国人民解放军战略支援部队航天工程大学 Pintle type continuous rotation knocking space attitude control engine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117703600A (en) * 2024-02-18 2024-03-15 中国人民解放军战略支援部队航天工程大学 Pintle type continuous rotation knocking space attitude control engine
CN117703600B (en) * 2024-02-18 2024-04-30 中国人民解放军战略支援部队航天工程大学 Pintle type continuous rotation knocking space attitude control engine

Also Published As

Publication number Publication date
DE1476949A1 (en) 1970-02-26

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