BE526525A - - Google Patents

Info

Publication number
BE526525A
BE526525A BE526525DA BE526525A BE 526525 A BE526525 A BE 526525A BE 526525D A BE526525D A BE 526525DA BE 526525 A BE526525 A BE 526525A
Authority
BE
Belgium
Application number
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.)
Publication of BE526525A publication Critical patent/BE526525A/xx

Links

Classifications

    • 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
    • F02K1/1207—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 fixed 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
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/123—Varying effective area of jet pipe or nozzle by means of pivoted flaps of two series of flaps, both having their flaps hinged at their upstream ends on a fixed structure

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Supercharger (AREA)
BE526525D 1953-02-16 BE526525A (no)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB324501X 1953-02-16
GB110254X 1954-02-11

Publications (1)

Publication Number Publication Date
BE526525A true BE526525A (no)

Family

ID=26247958

Family Applications (1)

Application Number Title Priority Date Filing Date
BE526525D BE526525A (no) 1953-02-16

Country Status (4)

Country Link
BE (1) BE526525A (no)
CH (1) CH324501A (no)
FR (1) FR1097287A (no)
GB (1) GB750307A (no)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930186A (en) * 1954-11-26 1960-03-29 Ashwood Peter Frederick Discharge nozzles for propulsive jets
US2982089A (en) * 1955-06-24 1961-05-02 Gen Motors Corp Afterburner nozzle

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3049875A (en) * 1952-08-15 1962-08-21 United Aircraft Corp Variable flap plug type nozzle
DE1164754B (de) * 1952-08-15 1964-03-05 United Aircraft Corp Schubduese fuer ein Flugzeugstrahltriebwerk
US3032974A (en) * 1956-08-24 1962-05-08 United Aircraft Corp Exhaust nozzle
US3004385A (en) * 1958-06-25 1961-10-17 Gen Motors Corp Variable convergent-divergent jet nozzle
US3038304A (en) * 1959-04-17 1962-06-12 Gen Electric Variable exhaust nozzle configuration
GB951130A (en) * 1961-07-28 1964-03-04 Rolls Royce Improvements relating to jet engines
GB1127826A (en) * 1966-06-17 1968-09-18 Rolls Royce Gas turbine engine
FR2732408A1 (fr) * 1983-03-16 1996-10-04 Snecma Tuyere, en particulier pour turboreacteur
US6318070B1 (en) 2000-03-03 2001-11-20 United Technologies Corporation Variable area nozzle for gas turbine engines driven by shape memory alloy actuators
US6543224B1 (en) * 2002-01-29 2003-04-08 United Technologies Corporation System and method for controlling shape memory alloy actuators
US7216831B2 (en) 2004-11-12 2007-05-15 The Boeing Company Shape changing structure
US7546727B2 (en) 2004-11-12 2009-06-16 The Boeing Company Reduced noise jet engine
US7340883B2 (en) 2004-11-12 2008-03-11 The Boeing Company Morphing structure
EP2074312B1 (en) * 2006-10-12 2017-12-13 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle with sliding actuation system
EP3008322B1 (en) * 2013-06-14 2022-03-09 Saab Ab Variable-geometry exhaust nozzle for a jet engine and a method for varying the nozzle
FR3051228B1 (fr) * 2016-05-12 2020-02-14 Herakles Rigidification de la liaison entre volets dans une tuyere a section variable
CN110159454B (zh) * 2019-06-17 2023-11-24 西安航空学院 固冲发动机可调喷管

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2930186A (en) * 1954-11-26 1960-03-29 Ashwood Peter Frederick Discharge nozzles for propulsive jets
US2982089A (en) * 1955-06-24 1961-05-02 Gen Motors Corp Afterburner nozzle

Also Published As

Publication number Publication date
GB750307A (en) 1956-06-13
FR1097287A (fr) 1955-07-04
CH324501A (de) 1957-09-30

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