GB1491528A - Device for varying the gas discharge area of an exhaust nozzle at the outlet of a jet deflecting device - Google Patents

Device for varying the gas discharge area of an exhaust nozzle at the outlet of a jet deflecting device

Info

Publication number
GB1491528A
GB1491528A GB8425/75A GB842575A GB1491528A GB 1491528 A GB1491528 A GB 1491528A GB 8425/75 A GB8425/75 A GB 8425/75A GB 842575 A GB842575 A GB 842575A GB 1491528 A GB1491528 A GB 1491528A
Authority
GB
United Kingdom
Prior art keywords
pipe section
roller
arm
engages
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
GB8425/75A
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.)
MTU Aero Engines AG
Original Assignee
MTU Motoren und Turbinen Union Muenchen GmbH
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 DE19742410069 external-priority patent/DE2410069C3/de
Application filed by MTU Motoren und Turbinen Union Muenchen GmbH filed Critical MTU Motoren und Turbinen Union Muenchen GmbH
Publication of GB1491528A publication Critical patent/GB1491528A/en
Expired legal-status Critical Current

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
    • F02K1/002—Plants 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
    • F02K1/004—Plants 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 by using one or more swivable nozzles rotating about their own axis
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Nozzles (AREA)
  • Exhaust Silencers (AREA)
GB8425/75A 1974-03-02 1975-02-28 Device for varying the gas discharge area of an exhaust nozzle at the outlet of a jet deflecting device Expired GB1491528A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19742410069 DE2410069C3 (de) 1974-03-02 Vorrichtung zur Verstellung des Gasaustrittsquerschnitts einer Schubdüse, die einer aus verdrehbaren Rohrabschnitten bestehenden Strahlablenkvorrichtung zugeordnet ist

Publications (1)

Publication Number Publication Date
GB1491528A true GB1491528A (en) 1977-11-09

Family

ID=5908923

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8425/75A Expired GB1491528A (en) 1974-03-02 1975-02-28 Device for varying the gas discharge area of an exhaust nozzle at the outlet of a jet deflecting device

Country Status (3)

Country Link
US (1) US3989193A (https=)
FR (1) FR2262736B3 (https=)
GB (1) GB1491528A (https=)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
GB2163105A (en) * 1984-08-16 1986-02-19 Rolls Royce Vectorable exhaust nozzle for gas turbine engine

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2540537C2 (de) * 1975-09-11 1977-11-10 Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinenstrahltriebwerk zum Antrieb und zur Steuerung eines Flugzeugs
FR2437499A1 (fr) * 1978-09-27 1980-04-25 Snecma Perfectionnement aux tuyeres orientables pour propulseurs a reaction
US4280660A (en) * 1979-08-17 1981-07-28 General Electric Company Vectorable nozzle
US4550877A (en) * 1982-08-03 1985-11-05 Rolls-Royce Inc. Streamlined nozzle for turbomachines
FR2565293B1 (fr) * 1984-06-04 1986-10-17 Aerospatiale Ensemble dilueur-deviateur de jet pour turbomoteur d'aerodyne
ES2059238B1 (es) * 1992-07-03 1997-07-01 Sener Ing & Sist Tobera orientable de geometria variable para propulsores de turbina de gas.
US7814753B2 (en) * 2006-07-25 2010-10-19 United Technologies Corporation Low profile attachment hanger system for a cooling liner within a gas turbine engine swivel exhaust duct
FR2928900B1 (fr) * 2008-03-20 2010-03-19 Airbus France Dispositif pour reduire les emissions infrarouge d'un turbopropulseur.
US11136941B2 (en) * 2017-11-09 2021-10-05 Abe Karem Devices and methods for exhaust vectoring in tilt rotor aircraft
CN110641713A (zh) * 2019-10-31 2020-01-03 万勇 一种喷气式无人机的旋转喷嘴

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2260038A (en) * 1940-04-30 1941-10-21 Electric Vacuum Cleaner Co Coupling
US2632660A (en) * 1948-12-31 1953-03-24 Krauthamer Josef Universal swivel coupling or joint
US2836034A (en) * 1951-06-29 1958-05-27 United Aircraft Corp Variable area nozzle
US3319892A (en) * 1965-09-01 1967-05-16 Gen Electric Variable exhaust nozzle assembly
US3776467A (en) * 1971-02-26 1973-12-04 Mtu Muenchen Gmbh Means for actuating a multiple tube jet defector device
GB1381503A (en) * 1971-06-11 1975-01-22 Rolls Royce Variable area nozzle for a gas turbine engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4519543A (en) * 1982-04-07 1985-05-28 Rolls-Royce Inc. Vectorable nozzles for turbomachines
GB2163105A (en) * 1984-08-16 1986-02-19 Rolls Royce Vectorable exhaust nozzle for gas turbine engine
US4679732A (en) * 1984-08-16 1987-07-14 Rolls-Royce Plc Vectorable exhaust nozzle for a gas turbine engine

Also Published As

Publication number Publication date
DE2410069B2 (de) 1977-06-23
US3989193A (en) 1976-11-02
DE2410069A1 (de) 1975-09-11
FR2262736A1 (https=) 1975-09-26
FR2262736B3 (https=) 1977-11-10

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
746 Register noted 'licences of right' (sect. 46/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19930228