GB870270A - Jet propulsion unit - Google Patents

Jet propulsion unit

Info

Publication number
GB870270A
GB870270A GB2572257A GB2572257A GB870270A GB 870270 A GB870270 A GB 870270A GB 2572257 A GB2572257 A GB 2572257A GB 2572257 A GB2572257 A GB 2572257A GB 870270 A GB870270 A GB 870270A
Authority
GB
United Kingdom
Prior art keywords
struts
platinum
propulsion unit
jet propulsion
similar
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
GB2572257A
Inventor
Randolph Samuel Rae
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.)
Garrett Corp
Original Assignee
Garrett Corp
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 US417828A priority Critical patent/US3040518A/en
Application filed by Garrett Corp filed Critical Garrett Corp
Priority to GB2572257A priority patent/GB870270A/en
Publication of GB870270A publication Critical patent/GB870270A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/74Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/78Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with an air-breathing jet-propulsion plant
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/06Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor the compressor comprising only axial stages
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Gas After Treatment (AREA)

Abstract

870,270. Generating combustion products under pressure. GARRETT CORPORATION. Aug. 14, 1957, No. 25722/57. Class 51 (1). [Also in Group XXVI] The combustion chamber 27, Fig. 11, of a jetpropulsion engine contains four struts 52 which support conical section 53 having a screen base portion 54 upon which is deposited finelydivided platinum; oxidant is directed through a passage 29 and a nozzle against the platinum which acts as a catalyst to maintain the flame. The afterburner may be of similar construction and comprise four similar conical sections located at the intersections of four radial V-shaped struts with a V-shaped ring supported by the struts, Figs. 4 and 9 (not shown).
GB2572257A 1954-03-22 1957-08-14 Jet propulsion unit Expired GB870270A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US417828A US3040518A (en) 1954-03-22 1954-03-22 Propulsion unit
GB2572257A GB870270A (en) 1957-08-14 1957-08-14 Jet propulsion unit

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2572257A GB870270A (en) 1957-08-14 1957-08-14 Jet propulsion unit

Publications (1)

Publication Number Publication Date
GB870270A true GB870270A (en) 1961-06-14

Family

ID=10232228

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2572257A Expired GB870270A (en) 1954-03-22 1957-08-14 Jet propulsion unit

Country Status (1)

Country Link
GB (1) GB870270A (en)

Similar Documents

Publication Publication Date Title
FR1222266A (en) Gas turbine reactor with downstream burner and thrust nozzle, especially for vertical takeoff and fast takeoff airplanes
GB680371A (en) Reheater for jet propulsion engines
GB1070788A (en) Cutting torch nozzle
GB870268A (en) Compound gas turbine engine
GB870270A (en) Jet propulsion unit
GB922876A (en) Jet-propelled aircraft with vertical take-off means
GB840914A (en) Rocket engines
GB1127653A (en) Improvements in and relating to a continuous fuel splash plate arrangement for a gas turbine jet propulsion engine afterburner
FR1209212A (en) Improvements made to pressurized liquid injectors, particularly fuel injectors
GB878785A (en) Improvements in and relating to oil burners
JPS5279111A (en) Combustor
GB885908A (en) Improvements in intakes for compressible fluids
GB599257A (en) Improvements relating to burners for liquid or gaseous fuels
FR1248821A (en) Annular combustion chamber for gas turbines, in particular for airplanes and turbine equipped with said chamber or with a similar chamber
GB775455A (en) Improvements in or relating to turbines and nozzle mechanism therefor
CA546179A (en) Fuel injection arrangement in vortex air stream in an annular combustion chamber surrounding a gas turbine
GB855469A (en) Gas turbine engine afterburner
GB923320A (en) Injector head for rockets
GB808975A (en) Improvements relating to jet propulsion systems
CA601999A (en) Combined steam and gas turbine powerplant with pressurized steam generator
GB892988A (en) Gas turbine control system
CA523686A (en) Means for conducting the flow of liquid fuel for feeding burners of gas turbine engines
FR76840E (en) Gas turbine reactor with downstream burner and thrust nozzle, especially for vertical takeoff and fast takeoff airplanes
CA523055A (en) Gas turbine jet engine
GB1108330A (en) Burner, e.g. for a gas turbine engine compressor chamber