ES2192657T3 - Estructura de avion y planta de potencia para usarse en ella. - Google Patents

Estructura de avion y planta de potencia para usarse en ella.

Info

Publication number
ES2192657T3
ES2192657T3 ES97310265T ES97310265T ES2192657T3 ES 2192657 T3 ES2192657 T3 ES 2192657T3 ES 97310265 T ES97310265 T ES 97310265T ES 97310265 T ES97310265 T ES 97310265T ES 2192657 T3 ES2192657 T3 ES 2192657T3
Authority
ES
Spain
Prior art keywords
power plant
airplane structure
aircraft
airplane
energy
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 - Lifetime
Application number
ES97310265T
Other languages
English (en)
Inventor
Geoffrey James Ash
Matthew Peter Toolan
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.)
BAE Systems PLC
Original Assignee
BAE Systems PLC
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 BAE Systems PLC filed Critical BAE Systems PLC
Application granted granted Critical
Publication of ES2192657T3 publication Critical patent/ES2192657T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
  • Tires In General (AREA)

Abstract

SE TRATA DE UNA AERONAVE QUE INCORPORA UNA CENTRAL DE ENERGIA CON MOTORES DE TURBINA DE GAS EN LA QUE, AL MENOS, PARTE DE LA PLANTA DE ENERGIA FORMA PARTE DEL ARMAZON DE LA AERONAVE O ESTA INTEGRADA EN EL MISMO.
ES97310265T 1996-12-18 1997-12-18 Estructura de avion y planta de potencia para usarse en ella. Expired - Lifetime ES2192657T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9626231A GB2320525A (en) 1996-12-18 1996-12-18 Mounting of powerplant in aircraft

Publications (1)

Publication Number Publication Date
ES2192657T3 true ES2192657T3 (es) 2003-10-16

Family

ID=10804608

Family Applications (1)

Application Number Title Priority Date Filing Date
ES97310265T Expired - Lifetime ES2192657T3 (es) 1996-12-18 1997-12-18 Estructura de avion y planta de potencia para usarse en ella.

Country Status (5)

Country Link
US (1) US6068212A (es)
EP (1) EP0849165B1 (es)
DE (1) DE69720931T2 (es)
ES (1) ES2192657T3 (es)
GB (1) GB2320525A (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7370467B2 (en) * 2003-07-29 2008-05-13 Pratt & Whitney Canada Corp. Turbofan case and method of making
EP1777378A3 (en) * 2003-07-29 2011-03-09 Pratt & Whitney Canada Corp. Turbofan case and method of making
GB2416009A (en) * 2004-05-12 2006-01-11 Dunlop Aerospace Ltd Hydraulic fluid control apparatus
US20100236244A1 (en) * 2006-06-28 2010-09-23 Longardner Robert L Heat absorbing and reflecting shield for air breathing heat engine
ES2560896T3 (es) * 2011-12-28 2016-02-23 Airbus Operations S.L. Parte trasera del fuselaje con un escudo para una aeronave con motores montados en el fuselaje y método para la determinación del área del escudo
US9498850B2 (en) 2012-03-27 2016-11-22 Pratt & Whitney Canada Corp. Structural case for aircraft gas turbine engine
FR3072947B1 (fr) * 2017-10-30 2021-12-17 Airbus Operations Sas Aeronef comprenant au moins un ensemble moteur relie au fuselage de l'aeronef par deux bielles de poussee positionnees au moins partiellement dans une entree d'air de l'ensemble moteur
US11162416B2 (en) * 2018-12-17 2021-11-02 Raytheon Technologies Corporation Attritable engine integrated with vehicle
US11613372B2 (en) * 2020-11-09 2023-03-28 Rohr, Inc. Ducted fan case attachment structure

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2504422A (en) * 1946-04-25 1950-04-18 Lockheed Aircraft Corp Aircraft engine and fuselage arrangement
GB737322A (en) * 1953-01-13 1955-09-21 Rolls Royce Improvements in or relating to aircraft and aircraft power plant arrangements
GB801832A (en) * 1955-09-24 1958-09-24 Fiat Spa Fuselage structure for jet propelled aircraft
GB1135100A (en) * 1966-07-27 1968-11-27 British Aircraft Corp Ltd Improvements in jet-propelled aeroplanes
US4022018A (en) * 1975-04-29 1977-05-10 General Electric Company Mounting system for a thrust generating engine
US4471609A (en) * 1982-08-23 1984-09-18 The Boeing Company Apparatus and method for minimizing engine backbone bending
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
GB9602130D0 (en) * 1996-02-02 1996-04-03 Rolls Royce Plc Improved method of combining ducted fan gas turbine engine modules and aircraft structure
GB2312251B (en) * 1996-04-18 1999-10-27 Rolls Royce Plc Ducted fan gas turbine engine mounting

Also Published As

Publication number Publication date
EP0849165A2 (en) 1998-06-24
EP0849165A3 (en) 2000-09-13
GB2320525A (en) 1998-06-24
DE69720931T2 (de) 2003-11-06
EP0849165B1 (en) 2003-04-16
GB9626231D0 (en) 1997-09-17
US6068212A (en) 2000-05-30
DE69720931D1 (de) 2003-05-22

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