GB618886A - Rocket - Google Patents

Rocket

Info

Publication number
GB618886A
GB618886A GB2145646A GB2145646A GB618886A GB 618886 A GB618886 A GB 618886A GB 2145646 A GB2145646 A GB 2145646A GB 2145646 A GB2145646 A GB 2145646A GB 618886 A GB618886 A GB 618886A
Authority
GB
United Kingdom
Prior art keywords
chambers
chamber
deflector
inlet
combustion chamber
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
GB2145646A
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
Application filed by Individual filed Critical Individual
Priority to GB2145646A priority Critical patent/GB618886A/en
Publication of GB618886A publication Critical patent/GB618886A/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
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
    • 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

Abstract

618,886. Jet-propulsion plant. BEYNON, G. July 17, 1946, No. 21456. [Class 110 (iii)] [Also in Group XII] A rocket comprises an inlet for induced air into which fuel is injected which inlet is flanked by an annular or cylindrical combustion chamber or chambers of circular cross section and a deflector is provided to guide the fuel and air into the combustion chamber or chambers in which it is ignited and after circulation therein is guided by a further deflector to the exhaust jet. Fuel from a pipe 2 mixed with air from the inlet 1 impinges on a deflector A which causes part to enter the annular combustion chamber 3 and part to enter the chamber 4. The part entering the combustion chamber 3 is ignited and then rotates around the chamber from which it is deflected by deflector B into the chamber 4. The cycle is repeated in the chambers 3<1>, 4<1> before entering the propulsion jet. In one modification the chambers 3 are cylindrical in form in another the inlet and the chamber 3 and 4 are annular in form. In a further modification, the chambers 3 are provided with additional baffles to retain some of the burning gases circulating around the chambers.
GB2145646A 1946-07-17 1946-07-17 Rocket Expired GB618886A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2145646A GB618886A (en) 1946-07-17 1946-07-17 Rocket

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2145646A GB618886A (en) 1946-07-17 1946-07-17 Rocket

Publications (1)

Publication Number Publication Date
GB618886A true GB618886A (en) 1949-03-01

Family

ID=10163246

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2145646A Expired GB618886A (en) 1946-07-17 1946-07-17 Rocket

Country Status (1)

Country Link
GB (1) GB618886A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3216191A (en) * 1960-05-09 1965-11-09 North American Aviation Inc Thrust chamber and turbopump assembly
EP0244972A2 (en) * 1986-05-03 1987-11-11 LUCAS INDUSTRIES public limited company Liquid fuel combustor
FR2957635A1 (en) * 2010-03-18 2011-09-23 Gheorghe Parciulea Multichamber static pressure propellant motor for e.g. military missile, has dynamic units including combustion chamber divided into initial chamber and auxiliary chamber, and central body including pumps integrated with turbine
RU2810847C1 (en) * 2023-08-16 2023-12-28 Владислав Юрьевич Климов Liquid rocket engine chamber

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3216191A (en) * 1960-05-09 1965-11-09 North American Aviation Inc Thrust chamber and turbopump assembly
EP0244972A2 (en) * 1986-05-03 1987-11-11 LUCAS INDUSTRIES public limited company Liquid fuel combustor
EP0244972A3 (en) * 1986-05-03 1989-01-25 Lucas Industries Public Limited Company Liquid fuel combustor
FR2957635A1 (en) * 2010-03-18 2011-09-23 Gheorghe Parciulea Multichamber static pressure propellant motor for e.g. military missile, has dynamic units including combustion chamber divided into initial chamber and auxiliary chamber, and central body including pumps integrated with turbine
RU2810847C1 (en) * 2023-08-16 2023-12-28 Владислав Юрьевич Климов Liquid rocket engine chamber

Similar Documents

Publication Publication Date Title
GB627832A (en) Improvement in propulsion plant comprising a gas turbine driven airscrew
JPS5256224A (en) Supersonic fuel injection supply system
GB680371A (en) Reheater for jet propulsion engines
GB650462A (en) Improvements in or relating to combustion apparatus
GB723015A (en) Improvements in or relating to gas turbine plant
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB1094540A (en) Improvements in or relating to annular combustion chambers for gas turbine engines
GB970189A (en) Combustion equipment for a gas turbine engine
GB618886A (en) Rocket
GB627634A (en) Improvements in or relating to gas turbine aircraft propulsion power plants
GB587083A (en) Improvements in combustion chambers for internal combustion turbines
GB627644A (en) Improvements relating to gas-turbine-engines and combustion-equipment therefor
GB1524217A (en) Combustion chamber for a gas turbine engine
GB922069A (en) Combustion chamber for a gas turbine engine
GB899213A (en) Combustion chambers
GB1033851A (en) Improved arrangement of fuel jets in toroid combustion spaces in internal combustion engines
GB1017900A (en) Combustion chambers
GB578764A (en) Improvements relating to combustion chambers for internal combustion turbines
GB1516177A (en) Fuel combustion apparatus
GB757871A (en) Improvements in and relating to combustion chambers
GB821286A (en) Improvements in or relating to reheat combustion equipment of jet-propulsion engines
JPS56113029A (en) Injector of ram rocket
GB1112131A (en) Gas turbine engine combustion apparatus
GB702752A (en) Improvements relating to combustion equipment of gas turbine engines
GB904460A (en) Gas turbine engine combustion chamber