FR1180334A - Perfectionnements aux tuyères de propulsion - Google Patents

Perfectionnements aux tuyères de propulsion

Info

Publication number
FR1180334A
FR1180334A FR1180334DA FR1180334A FR 1180334 A FR1180334 A FR 1180334A FR 1180334D A FR1180334D A FR 1180334DA FR 1180334 A FR1180334 A FR 1180334A
Authority
FR
France
Prior art keywords
propulsion nozzles
propulsion
nozzles
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
Other languages
English (en)
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.)
Bristol Aero Engines Ltd
Original Assignee
Bristol Aero Engines 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 Bristol Aero Engines Ltd filed Critical Bristol Aero Engines Ltd
Application granted granted Critical
Publication of FR1180334A publication Critical patent/FR1180334A/fr
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D99/00—Subject matter not provided for in other groups of this subclass
    • F27D99/007—Partitions
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/60—Reversing jet main flow by blocking the rearward discharge by means of pivoted eyelids or clamshells, e.g. target-type reversers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F27—FURNACES; KILNS; OVENS; RETORTS
    • F27D—DETAILS OR ACCESSORIES OF FURNACES, KILNS, OVENS, OR RETORTS, IN SO FAR AS THEY ARE OF KINDS OCCURRING IN MORE THAN ONE KIND OF FURNACE
    • F27D1/00—Casings; Linings; Walls; Roofs
    • F27D1/18—Door frames; Doors, lids, removable covers
    • F27D1/1858—Doors
    • F27D2001/1875—Hanging doors and walls

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Testing Of Engines (AREA)
  • Portable Nailing Machines And Staplers (AREA)
  • Basic Packing Technique (AREA)
  • Nozzles (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR1180334D 1956-07-30 1957-07-30 Perfectionnements aux tuyères de propulsion Expired FR1180334A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB23503/56A GB820059A (en) 1956-07-30 1956-07-30 Improvements in or relating to jet propulsion nozzles

Publications (1)

Publication Number Publication Date
FR1180334A true FR1180334A (fr) 1959-06-03

Family

ID=38527326

Family Applications (2)

Application Number Title Priority Date Filing Date
FR1180374D Expired FR1180374A (fr) 1956-07-30 1957-07-30 Mur suspendu réfractaire
FR1180334D Expired FR1180334A (fr) 1956-07-30 1957-07-30 Perfectionnements aux tuyères de propulsion

Family Applications Before (1)

Application Number Title Priority Date Filing Date
FR1180374D Expired FR1180374A (fr) 1956-07-30 1957-07-30 Mur suspendu réfractaire

Country Status (5)

Country Link
US (1) US3028730A (fr)
DE (1) DE1055886B (fr)
ES (1) ES236873A1 (fr)
FR (2) FR1180374A (fr)
GB (1) GB820059A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048973A (en) * 1959-10-29 1962-08-14 Marcus C Benedict Exhaust nozzle

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049873A (en) * 1958-02-04 1962-08-21 Westinghouse Electric Corp Exhaust nozzle having a flow area of variable convergency and divergency
GB985192A (en) * 1960-05-13 1965-03-03 Bristol Siddeley Engines Ltd Improvements in aircraft propulsion power plants
US3157027A (en) * 1962-02-12 1964-11-17 Rolls Royce Propulsion nozzles
DE1221498B (de) * 1962-02-12 1966-07-21 Rolls Royce Strahltriebwerk mit im Querschnitt veraenderbarer Schubduese
US3390837A (en) * 1965-12-08 1968-07-02 Gen Electric Convergent-divergent plug nozzle having a plurality of freely-floating tandem flaps
FR2189642B1 (fr) * 1972-06-19 1976-08-06 Snecma
US3791586A (en) * 1972-12-26 1974-02-12 Boeing Co Combination clamshell thrust reverser & variable nozzle area ramp
US3917198A (en) * 1974-06-21 1975-11-04 Rohr Industries Inc Overwing post exit blocker/deflector door thrust reverser
FR2557278B1 (fr) * 1983-12-23 1986-05-16 Stein Heurtey Ecran pour four de rechauffage siderurgique
CN113833574B (zh) * 2020-06-24 2023-02-03 中国航发商用航空发动机有限责任公司 反推力装置和航空发动机

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2510606A (en) * 1943-05-22 1950-06-06 Lockheed Aircraft Corp Turbine construction
GB636115A (en) * 1944-04-15 1950-04-26 United Aircraft Corp Improvements in or relating to pressure controls for turbines
US2537772A (en) * 1944-11-30 1951-01-09 Wright Aeronautical Corp Turbo-prop exhaust nozzle control system utilizing impact and exhaust pressures as parameters
US2653445A (en) * 1945-05-11 1953-09-29 Dehavilland Aircraft Turbocompressor jet-propulsion apparatus and adjustable nozzle therefor
US2551372A (en) * 1945-11-13 1951-05-01 Cons Vultee Aircraft Corp Orifice control means for jet propulsion motors
US2680948A (en) * 1948-08-30 1954-06-15 Engineering & Res Corp Variable area tail pipe for jet engines
US2693078A (en) * 1949-03-18 1954-11-02 Westinghouse Electric Corp Exhaust orifice control for jet engines
GB681575A (en) * 1949-06-30 1952-10-29 United Aircraft Corp Improvements in or relating to control device for regulating an area of a thrust nozzle
FR1018650A (fr) * 1950-03-14 1953-01-09 Tuyère d'éjection réglable pour propulseurs à réaction, notamment moteurs d'aérodynes
FR1030483A (fr) * 1951-01-04 1953-06-15 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
US2682147A (en) * 1951-06-16 1954-06-29 Rohr Aircraft Corp Adjustable nozzle for exhaust gas
US2671313A (en) * 1952-03-07 1954-03-09 Emile A Laramee Jet engine vacuum expansion nozzle
US2770944A (en) * 1952-04-26 1956-11-20 United Aircraft Corp Variable area reaction nozzle movable from convergent to convergent-di-vergent form
US2806349A (en) * 1952-12-24 1957-09-17 Solar Aircraft Co Sheet metal variable area nozzle
NL87657C (fr) * 1953-04-10
FR65303E (fr) * 1954-02-11 1956-02-08 Snecma Procédé et dispositifs de réglage d'un écoulement et leurs diverses applications
FR1006139A (fr) * 1954-11-25 1952-04-21 Cem Comp Electro Mec Procédé et dispositif de réglage des turbo-réacteurs

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3048973A (en) * 1959-10-29 1962-08-14 Marcus C Benedict Exhaust nozzle

Also Published As

Publication number Publication date
GB820059A (en) 1959-09-16
ES236873A1 (es) 1958-03-01
FR1180374A (fr) 1959-06-03
US3028730A (en) 1962-04-10
DE1055886B (de) 1959-04-23

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