[go: up one dir, main page]

GB694373A - Ignition equipment for the combustion equipment of a rocket motor - Google Patents

Ignition equipment for the combustion equipment of a rocket motor

Info

Publication number
GB694373A
GB694373A GB22157/50A GB2215750A GB694373A GB 694373 A GB694373 A GB 694373A GB 22157/50 A GB22157/50 A GB 22157/50A GB 2215750 A GB2215750 A GB 2215750A GB 694373 A GB694373 A GB 694373A
Authority
GB
United Kingdom
Prior art keywords
chamber
jacket
fuel
equipment
oxidizer
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
GB22157/50A
Inventor
Edward George David Andrews
Anthony William Thomas Mottram
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.)
Armstrong Siddeley Motors Ltd
Original Assignee
Armstrong Siddeley Motors 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
Priority to BE508933D priority Critical patent/BE508933A/xx
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Priority to GB22157/50A priority patent/GB694373A/en
Priority to US240197A priority patent/US2701445A/en
Priority to DEA15037A priority patent/DE941034C/en
Publication of GB694373A publication Critical patent/GB694373A/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
    • F02K9/95—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by starting or ignition means or 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

694,373. Igniters for liquid fuel combustion equipment. ARMSTRONG SIDDELEY MOTORS, Ltd. July 16,1951 [Sept. 8, 7950], No.. 22157/50.. Class 75(iii) Ignition equipment 8 for the combustion equipment 10 of a rocket motor adapted to burn a mixture of liquid fuel; for instance methyl alcohol admixed with water, and oxidizer, for instance liquid oxygen or nitric acid, comprises a chamber 9 in which a portion of the fuel and oxidizer are combined and which is surrounded by a cooling jacket 19 through which a portion of the liquid fuel is passed to be sprayed from an outlet formed between the wall of the chamber 9 and a surrounding nozzle piece 19b coaxial with the chamber outlet 11 so as to burn in the burning mixture. The chamber 9 is formed as a steel shell which is cylindrical for about half its length and is then connected by a frustoconical part 18 to the cylindrical outlet 11. The jacket comprises a cylindrical part 19a to which the nozzle 19b is connected by a sleeve 19c, the jacket and shell being spaced by helical ridges 27 and by circular ridges 28 ... 30 having oblique grooves. Fuel and oxidizer are sprayed through orifices 22 in the jacket to meet near the entrance end of the chamber adjacent to a sparking plug inserted through a hole 24 in the equipment and fuel is led to the space 26 between chamber and jacket by a duct 25 in the jacket. The ignition charnber 9 communicates with the main chamber 10 of the combustion equipment so that the flame from the outlet 11 meets the main jets of liquid fuel and oxidizer from the main spray device 15. The ignition. equipment 8 is supplied with 3 per cent to 5 per cent of the fuel to the combustion equipment 10 and two parts of this fuel are fed to the jacket and one part to the chamber 9. Specification 694,371 is referred to and Specification 682,732, [Group XXVI], is referred to in the Provisional Specification.
GB22157/50A 1950-09-08 1950-09-08 Ignition equipment for the combustion equipment of a rocket motor Expired GB694373A (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
BE508933D BE508933A (en) 1950-09-08
GB22157/50A GB694373A (en) 1950-09-08 1950-09-08 Ignition equipment for the combustion equipment of a rocket motor
US240197A US2701445A (en) 1950-09-08 1951-08-03 Ignition equipment for the combustion equipment of rocket motors
DEA15037A DE941034C (en) 1950-09-08 1952-01-29 Ignition device for rocket or jet engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22157/50A GB694373A (en) 1950-09-08 1950-09-08 Ignition equipment for the combustion equipment of a rocket motor

Publications (1)

Publication Number Publication Date
GB694373A true GB694373A (en) 1953-07-22

Family

ID=10174856

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22157/50A Expired GB694373A (en) 1950-09-08 1950-09-08 Ignition equipment for the combustion equipment of a rocket motor

Country Status (3)

Country Link
US (1) US2701445A (en)
BE (1) BE508933A (en)
GB (1) GB694373A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5257500A (en) * 1992-07-27 1993-11-02 General Electric Company Aircraft engine ignition system

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB736699A (en) * 1952-09-10 1955-09-14 Ca Nat Research Council Pulsating torch igniter for combustion chambers
US2831322A (en) * 1952-12-29 1958-04-22 Gen Motors Corp Injector igniter plug
US2941364A (en) * 1955-04-05 1960-06-21 Armstrong Siddeley Motors Ltd Igniter chamber for a gas turbine engine
US2967224A (en) * 1956-10-08 1961-01-03 Ford Motor Co Hot wire igniter
US3077073A (en) * 1957-10-29 1963-02-12 United Aircraft Corp Rocket engine having fuel driven propellant pumps
US3143851A (en) * 1960-03-23 1964-08-11 Alwac International Inc Method and apparatus for mixing combustible fluids
US4047880A (en) * 1974-05-15 1977-09-13 Antonio Caldarelli Fluids distributor for energized-fluid systems
FR2421364A2 (en) * 1978-03-28 1979-10-26 Europ Propulsion IGNITION SYSTEM FOR GAS OR COMBUSTIBLE LIQUIDS
CN104481733A (en) * 2014-11-28 2015-04-01 苟仲武 Efficient and environmentally-friendly liquid propellant rocket engine
CN108757223B (en) * 2018-03-29 2019-11-29 北京航天动力研究所 For examining the thrust cell structure and method of the anti-oxidant ablation property of composite material
WO2021242229A1 (en) * 2020-05-27 2021-12-02 Aerojet Rocketdyne, Inc. Two-piece combustor

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE522435C (en) * 1927-08-17 1931-04-09 E H Hans Holzwarth Dr Ing Deflagration chamber, especially for internal combustion turbines
US1879186A (en) * 1930-10-30 1932-09-27 Robert H Goddard Apparatus for igniting liquid fuel
US2395403A (en) * 1939-03-06 1946-02-26 Daniel And Florence Guggenheim Rotatable combustion apparatus for aircraft
US2286909A (en) * 1940-12-16 1942-06-16 Robert H Goddard Combustion chamber
US2408111A (en) * 1943-08-30 1946-09-24 Robert C Truax Two-stage rocket system
US2520751A (en) * 1944-02-19 1950-08-29 Aerojet Engineering Corp Reaction motor with fluid cooling means
US2500334A (en) * 1944-06-19 1950-03-14 Aerojet Engineering Corp Jet motor operable by monopropellant and method of operating it
US2470564A (en) * 1944-11-15 1949-05-17 Reaction Motors Inc Reaction motor control system
US2489716A (en) * 1946-01-12 1949-11-29 Theima Mccollum Internal-combustion heater with pilot burner
FR963784A (en) * 1947-01-13 1950-07-20
US2480147A (en) * 1947-01-29 1949-08-30 Letvin Samuel Firing device for combustion apparatus

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5257500A (en) * 1992-07-27 1993-11-02 General Electric Company Aircraft engine ignition system
US5367871A (en) * 1992-07-27 1994-11-29 General Electric Company Aircraft engine ignition system

Also Published As

Publication number Publication date
BE508933A (en)
US2701445A (en) 1955-02-08

Similar Documents

Publication Publication Date Title
GB694373A (en) Ignition equipment for the combustion equipment of a rocket motor
US2579614A (en) Combustion chamber with rotating fuel and air stream surrounding a flame core
GB660775A (en) An improved combustion and ignition apparatus for a gas turbine engine
US2525207A (en) Ignition torch for internal-combustion prime movers
US2659201A (en) Gas turbine combustion chamber with provision for turbulent mixing of air and fuel
GB1154098A (en) Multi-Fuel Burner Nozzle.
US3169368A (en) Combustion chamber for liquid fuels
GB991428A (en) Improvements in manufacture of carbon black
GB696756A (en) Improvements in or relating to ignition systems for gas turbine engines
GB895015A (en) Improvements in or relating to jet propulsion devices
GB621789A (en) Improved ignition system for gas turbine engines
RU105947U1 (en) MIXING HEAD WITH IGNITION DEVICE
GB565952A (en) Improvements in means for generating a mixture of steam and combustion products under pressure
US2758441A (en) Glow plug igniter structure
GB619354A (en) Combined spark plug and fuel priming means
GB763962A (en) Rocket motors
US3046973A (en) Heating apparatus for liquid fuels
GB747593A (en) Improvements in or relating to igniters for gas turbine engines and combustion heaters
RU2624419C1 (en) Gaseous hydrogen and oxygen thruster with slot nozzle
SU669146A1 (en) Device for explosion-like combustion
US2956403A (en) Igniter
GB715197A (en) Jet propulsion engines
GB805400A (en) Air-breathing jet engines suitable for use at high altitudes
GB699471A (en) Rocket apparatus
SU88823A1 (en) Fuel oil burner in open-hearth furnaces