FR2072009A7 - - Google Patents

Info

Publication number
FR2072009A7
FR2072009A7 FR7045809A FR7045809A FR2072009A7 FR 2072009 A7 FR2072009 A7 FR 2072009A7 FR 7045809 A FR7045809 A FR 7045809A FR 7045809 A FR7045809 A FR 7045809A FR 2072009 A7 FR2072009 A7 FR 2072009A7
Authority
FR
France
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
FR7045809A
Other versions
FR2072009B3 (fr
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 claimed from DE19691964716 external-priority patent/DE1964716C3/de
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Application granted granted Critical
Publication of FR2072009A7 publication Critical patent/FR2072009A7/fr
Publication of FR2072009B3 publication Critical patent/FR2072009B3/fr
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
    • F02K1/06Varying effective area of jet pipe or nozzle
    • F02K1/12Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261Varying 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • B64C9/38Jet flaps
    • 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
    • F02K1/002Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/006Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector within one plane only

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
  • Jet Pumps And Other Pumps (AREA)
FR707045809A 1969-12-23 1970-12-18 Expired FR2072009B3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691964716 DE1964716C3 (de) 1969-12-23 Flugzeug-Strahltriebwerk mit einer bezug ich des Austrittsquerschnitts verstellbaren Schubdüse

Publications (2)

Publication Number Publication Date
FR2072009A7 true FR2072009A7 (fr) 1971-09-24
FR2072009B3 FR2072009B3 (fr) 1973-08-10

Family

ID=5754879

Family Applications (1)

Application Number Title Priority Date Filing Date
FR707045809A Expired FR2072009B3 (fr) 1969-12-23 1970-12-18

Country Status (2)

Country Link
FR (1) FR2072009B3 (fr)
GB (1) GB1306588A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439304A1 (fr) * 1978-10-17 1980-05-16 Mtu Muenchen Gmbh Piece d'extremite d'un reacteur prevu notamment sur un avion

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2537657A1 (fr) * 1982-12-08 1984-06-15 Snecma Tuyere a section variable pour un turboreacteur et avion comportant un tel equipement
FR2790791B1 (fr) * 1999-03-10 2001-04-13 Snecma Tuyere d'ejection de turboreacteur axisymetrique et a orientation globale
FR2792366B1 (fr) 1999-04-15 2005-08-19 Snecma Tuyere d'ejection axisymetrique, convergente divergente et orientable
GB2365463B (en) 2000-08-01 2005-02-16 Renovus Ltd Drilling method
US6546716B2 (en) * 2001-04-26 2003-04-15 Jean-Pierre Lair Jet engine nozzle with variable thrust vectoring and exhaust area
US7230879B2 (en) 2005-02-12 2007-06-12 Chevron U.S.A. Inc. Method and apparatus for true relative amplitude correction of seismic data for normal moveout stretch effects
CN116877503A (zh) * 2023-07-07 2023-10-13 芜湖泰瑞汽车有限公司 一种喷嘴截面可变的引射器

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2439304A1 (fr) * 1978-10-17 1980-05-16 Mtu Muenchen Gmbh Piece d'extremite d'un reacteur prevu notamment sur un avion

Also Published As

Publication number Publication date
DE1964716A1 (de) 1971-07-01
FR2072009B3 (fr) 1973-08-10
DE1964716B2 (de) 1976-04-29
GB1306588A (en) 1973-02-14

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