GB632663A - An improved gas turbine jet propulsion engine - Google Patents

An improved gas turbine jet propulsion engine

Info

Publication number
GB632663A
GB632663A GB3090346A GB3090346A GB632663A GB 632663 A GB632663 A GB 632663A GB 3090346 A GB3090346 A GB 3090346A GB 3090346 A GB3090346 A GB 3090346A GB 632663 A GB632663 A GB 632663A
Authority
GB
United Kingdom
Prior art keywords
jet propulsion
gas turbine
propulsion engine
improved gas
turbine jet
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
GB3090346A
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.)
ALEXANDER VIVIAN WYVIN STENSON
Original Assignee
ALEXANDER VIVIAN WYVIN STENSON
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 ALEXANDER VIVIAN WYVIN STENSON filed Critical ALEXANDER VIVIAN WYVIN STENSON
Priority to GB3090346A priority Critical patent/GB632663A/en
Publication of GB632663A publication Critical patent/GB632663A/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
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/04Mounting of an exhaust cone in the jet pipe
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/38Introducing air inside the jet

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)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Treating Waste Gases (AREA)

Abstract

632,663. Jet propulsion plant. STENSON, A. V. W. Oct. 28, 1946, No. 30903. [Class 110(iii)] A gas turbine jet propulsion plant has a hollow truncated bullet 2 through which a mass of air passes which air is led into the bullet through the ducts 3 by which the bullet is supported from the outer casing. This air is heated by the turbine exhaust gases and mixes with the hot exhausf gases at 8. Specification 588,918 is referred to.
GB3090346A 1946-10-28 1946-10-28 An improved gas turbine jet propulsion engine Expired GB632663A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3090346A GB632663A (en) 1946-10-28 1946-10-28 An improved gas turbine jet propulsion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3090346A GB632663A (en) 1946-10-28 1946-10-28 An improved gas turbine jet propulsion engine

Publications (1)

Publication Number Publication Date
GB632663A true GB632663A (en) 1949-11-28

Family

ID=10314898

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3090346A Expired GB632663A (en) 1946-10-28 1946-10-28 An improved gas turbine jet propulsion engine

Country Status (1)

Country Link
GB (1) GB632663A (en)

Similar Documents

Publication Publication Date Title
GB584820A (en) Improvements relating to internal combustion prime movers
FR951218A (en) Improvements to fuel systems for jet engines, gas turbines and similar power sources
GB650462A (en) Improvements in or relating to combustion apparatus
GB588086A (en) Improvements relating to combustion apparatus
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB922069A (en) Combustion chamber for a gas turbine engine
GB632663A (en) An improved gas turbine jet propulsion engine
GB699251A (en) Sheet metal combustion chambers, flame tubes and other like tubular bodies
GB866969A (en) Gas turbine engines
GB701320A (en) Improvements in or relating to combustion equipment of gas-turbine engines
GB534926A (en) Improvements in means for silencing the exhaust of internal combustion engines
GB588097A (en) Improvements in or relating to internal combustion turbine power plants
GB585398A (en) Combustion chamber unit
GB587571A (en) Improvements in or relating to internal combustion turbine power plants
GB710589A (en) Combustion chambers for jet engines or gas turbines
GB618644A (en) Improvements in or relating to combustion units
GB637223A (en) Improvements in and relating to combustion units particularly for use in gas turbinesystems
GB576545A (en) Improvements relating to combustion chambers for prime movers
GB729163A (en) Improvements in or relating to cyclone furnaces
FR1002468A (en) Gas turbine engines capable of operating with or without atmospheric air, in particular for the propulsion of warships
GB657346A (en) Improvements in gas turbine plants
GB627962A (en) A combustion chamber for an internal-combustion turbine plant
GB738811A (en) Improvements relating to continuous combustion apparatus
GB588601A (en) Improvements in or relating to gas turbine plant
GB888109A (en) Improvements relating to gas turbine power plant