ES195638A1 - Un turbo motor de chorro - Google Patents

Un turbo motor de chorro

Info

Publication number
ES195638A1
ES195638A1 ES0195638A ES195638A ES195638A1 ES 195638 A1 ES195638 A1 ES 195638A1 ES 0195638 A ES0195638 A ES 0195638A ES 195638 A ES195638 A ES 195638A ES 195638 A1 ES195638 A1 ES 195638A1
Authority
ES
Spain
Prior art keywords
jet
nozzle
fuel
annular passage
tube
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
ES0195638A
Other languages
English (en)
Spanish (es)
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
Application filed by Armstrong Siddeley Motors Ltd filed Critical Armstrong Siddeley Motors Ltd
Publication of ES195638A1 publication Critical patent/ES195638A1/es
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26Controlling the air flow
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K3/00Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Jet Pumps And Other Pumps (AREA)
ES0195638A 1949-12-31 1950-12-01 Un turbo motor de chorro Expired ES195638A1 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33494/49A GB669915A (en) 1949-12-31 1949-12-31 Turbo jet engines

Publications (1)

Publication Number Publication Date
ES195638A1 true ES195638A1 (es) 1952-05-16

Family

ID=10353701

Family Applications (1)

Application Number Title Priority Date Filing Date
ES0195638A Expired ES195638A1 (es) 1949-12-31 1950-12-01 Un turbo motor de chorro

Country Status (7)

Country Link
US (1) US2708340A (en, 2012)
BE (1) BE500180A (en, 2012)
CH (1) CH294839A (en, 2012)
DE (1) DE849628C (en, 2012)
ES (1) ES195638A1 (en, 2012)
FR (1) FR1027801A (en, 2012)
GB (1) GB669915A (en, 2012)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE955558C (de) * 1952-04-20 1957-01-03 Max Adolf Mueller Dipl Ing Strahltriebwerk
US2933886A (en) * 1953-04-15 1960-04-26 Sharma Devendra Nath Turbojet engine convertible to ramjet engine
GB910178A (en) * 1960-08-02 1962-11-14 Rolls Royce Gas turbine by-pass jet engine
DE1276969B (de) * 1962-10-30 1968-09-05 Bristol Siddeley Engines Ltd Gasturbinenstrahltriebwerk
US3279193A (en) * 1964-07-01 1966-10-18 James E Webb Method and construction for protecting heat sensitive bodies from thermal radiation ad convective heat
US4072008A (en) * 1976-05-04 1978-02-07 General Electric Company Variable area bypass injector system
US4074523A (en) * 1976-12-08 1978-02-21 The United States Of America As Represented By The Secretary Of The Air Force Pressure actuated collapsible curtain liners for a gas turbine engine nozzle
EP0160491B1 (en) * 1984-04-26 1990-04-18 Matsushita Electric Industrial Co., Ltd. Enclosed lead storage battery and process for producing the same
US9969500B2 (en) * 2014-02-06 2018-05-15 Honeywell International Inc. Bifurcated ducts including plenums for stabilizing flow therethrough and exhaust systems including the same

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB412970A (en) * 1933-01-06 1934-07-06 British Thomson Houston Co Ltd Improvements in and relating to gas turbine cycles with interstage reheating
US2408099A (en) * 1943-04-07 1946-09-24 Sherman Albert Variable-area nozzle for jetpropelled aircraft
US2585270A (en) * 1945-03-12 1952-02-12 Boeing Co Adjustable jet nozzle for aircraft propulsion
US2653445A (en) * 1945-05-11 1953-09-29 Dehavilland Aircraft Turbocompressor jet-propulsion apparatus and adjustable nozzle therefor
US2635420A (en) * 1947-05-14 1953-04-21 Shell Dev Jet propulsion engine with auxiliary pulse jet engine
US2509238A (en) * 1947-07-31 1950-05-30 Arnold W Martin Thrust reversing and speed control for jet propulsion engines
US2557883A (en) * 1947-09-17 1951-06-19 Ernest F Miller Jet propulsion exhaust nozzle apparatus
CA486078A (en) * 1950-04-27 1952-08-26 W. Kellal George Exit area control for jet engines
US2516910A (en) * 1948-06-02 1950-08-01 Westinghouse Electric Corp Gas turbine apparatus with selective regenerator control

Also Published As

Publication number Publication date
FR1027801A (fr) 1953-05-15
GB669915A (en) 1952-04-09
BE500180A (en, 2012)
DE849628C (de) 1952-09-18
CH294839A (fr) 1953-11-30
US2708340A (en) 1955-05-17

Similar Documents

Publication Publication Date Title
US2475911A (en) Combustion apparatus
US2520388A (en) Apparatus for supporting combustion in fast-moving air streams
GB627832A (en) Improvement in propulsion plant comprising a gas turbine driven airscrew
ES195638A1 (es) Un turbo motor de chorro
GB691068A (en) Fuel burning means for a gaseous-fluid propulsion jet
GB680371A (en) Reheater for jet propulsion engines
US2771743A (en) Gas-turbine engine with reheat combustion equipment
GB1116930A (en) Improvements in cooled flameholder assembly
US2872785A (en) Jet engine burner apparatus having means for spreading the pilot flame
GB588847A (en) Improvements in combustion chambers for internal combustion turbines
GB871842A (en) Improvements in or relating to gas turbine engines
US2651178A (en) Combination injector and stabilizer for gas turbine afterburners
GB744196A (en) Improvements in or relating to silencing means
US2685168A (en) Combustion chamber
US2709337A (en) Boundary layer control for the diffuser of a gas turbine
GB627634A (en) Improvements in or relating to gas turbine aircraft propulsion power plants
GB659794A (en) Improvements in or relating to means for securing stabilised burning of fuel in fast-moving air or gas streams
US2639581A (en) Apparatus for burning fuel in a high velocity gas stream
GB1126163A (en) Gas turbine by-pass engine
GB879484A (en) Improvements relating to flameholder units
US2835109A (en) Igniter for ram-jet
US3504491A (en) Combustion devices
GB674641A (en) Fuel-burning means for a gaseous-fluid propulsion jet
GB719301A (en) Improvements relating to gas turbine engines
US2972231A (en) Rod-igniters for ramjet burners