DE2133901C3 - - Google Patents

Info

Publication number
DE2133901C3
DE2133901C3 DE2133901A DE2133901A DE2133901C3 DE 2133901 C3 DE2133901 C3 DE 2133901C3 DE 2133901 A DE2133901 A DE 2133901A DE 2133901 A DE2133901 A DE 2133901A DE 2133901 C3 DE2133901 C3 DE 2133901C3
Authority
DE
Germany
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
DE2133901A
Other languages
German (de)
Other versions
DE2133901B2 (de
DE2133901A1 (de
Inventor
John Albert Chellaston Derby Mullins (Grossbritannien)
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.)
UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Publication of DE2133901A1 publication Critical patent/DE2133901A1/de
Publication of DE2133901B2 publication Critical patent/DE2133901B2/de
Application granted granted Critical
Publication of DE2133901C3 publication Critical patent/DE2133901C3/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Transmission Devices (AREA)
DE2133901A 1970-07-09 1971-07-07 Flugzeug mit mehreren Triebwerken Granted DE2133901B2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB33316/70A GB1262419A (en) 1970-07-09 1970-07-09 Aircraft engine mountings

Publications (3)

Publication Number Publication Date
DE2133901A1 DE2133901A1 (de) 1972-06-22
DE2133901B2 DE2133901B2 (de) 1974-12-19
DE2133901C3 true DE2133901C3 (OSRAM) 1975-08-21

Family

ID=10351370

Family Applications (1)

Application Number Title Priority Date Filing Date
DE2133901A Granted DE2133901B2 (de) 1970-07-09 1971-07-07 Flugzeug mit mehreren Triebwerken

Country Status (4)

Country Link
US (1) US3735946A (OSRAM)
DE (1) DE2133901B2 (OSRAM)
GB (1) GB1262419A (OSRAM)
IT (1) IT940430B (OSRAM)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3997132A (en) * 1974-12-11 1976-12-14 The Garrett Corporation Method and apparatus for controlling tip vortices
US4043522A (en) * 1975-12-22 1977-08-23 The Boeing Company Common pod for housing a plurality of different turbofan jet propulsion engines
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
CN1143589A (zh) * 1995-08-18 1997-02-26 梁富泉 复合翼飞机
GB0116219D0 (en) * 2001-07-03 2002-03-06 Bae Systems Plc An aircraft
US7122080B2 (en) * 2001-09-14 2006-10-17 Imerys Pigments, Inc. Integrated process for simultaneous beneficiation, leaching, and dewatering of kaolin clay suspension
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
FR2892705B1 (fr) * 2005-11-03 2009-04-24 Airbus France Sas Aeronef a impact environnemental reduit.
GB2434837B (en) * 2006-02-07 2008-04-09 Rolls Royce Plc A containment system for a gas turbine engine
FR2905356B1 (fr) * 2006-09-05 2008-11-07 Airbus France Sas Procede pour la realisation d'un aeronef a impact environnemental reduit et aeronef obtenu
WO2009110943A2 (en) * 2007-12-17 2009-09-11 Massachusetts Institute Of Technology Aircraft drag management structure
FR2968634B1 (fr) * 2010-12-08 2013-08-02 Snecma Pylone de fixation d'un moteur d'aeronef a helices propulsives non carenees
EP2683609B1 (en) * 2011-03-09 2018-04-11 Gunnar Rosenlund Propulsion system
FR3074477B1 (fr) * 2017-12-06 2019-12-20 Airbus Operations Avion a configuration evolutive en vol
GB201809822D0 (en) * 2018-06-15 2018-08-01 Rolls Royce Plc Gas turbine engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2421699A (en) * 1944-05-12 1947-06-03 Lockheed Aircraft Corp Auxiliary fuel tank
US2863620A (en) * 1952-10-04 1958-12-09 Sud Aviation Jet-propelled aircraft
US3098632A (en) * 1953-09-11 1963-07-23 Lockheed Aircraft Corp Combination aircraft fuel tank and powerplant arrangement
BE652447A (OSRAM) * 1963-08-29
GB1093050A (en) * 1965-03-16 1967-11-29 Rolls Royce Aircraft engine mounting
GB1294324A (en) * 1969-05-03 1972-10-25 Dowty Rotol Ltd Engine installations

Also Published As

Publication number Publication date
US3735946A (en) 1973-05-29
DE2133901B2 (de) 1974-12-19
IT940430B (it) 1973-02-10
DE2133901A1 (de) 1972-06-22
GB1262419A (en) 1972-02-02

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Legal Events

Date Code Title Description
C3 Grant after two publication steps (3rd publication)