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)
  • Tires In General (AREA)
  • Engine Equipment That Uses Special Cycles (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 (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6367738B1 (en) * 2000-01-31 2002-04-09 John Wadleigh Aerobatic aircraft
EP1777378A3 (en) * 2003-07-29 2011-03-09 Pratt & Whitney Canada Corp. Turbofan case and method of making
US7370467B2 (en) * 2003-07-29 2008-05-13 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
GB2626521B (en) * 2015-08-28 2026-03-18 Bae Systems Plc Exhaust duct
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
EP0849165B1 (en) 2003-04-16
GB9626231D0 (en) 1997-09-17
DE69720931D1 (de) 2003-05-22
DE69720931T2 (de) 2003-11-06
GB2320525A (en) 1998-06-24
US6068212A (en) 2000-05-30
EP0849165A2 (en) 1998-06-24
EP0849165A3 (en) 2000-09-13

Similar Documents

Publication Publication Date Title
ES2192657T3 (es) Estructura de avion y planta de potencia para usarse en ella.
DE59704567D1 (de) Mehrstufige Gasturbine mit Dampfkühlung und -einleitung in die Brennkammer
CO4650252A1 (es) Una planta turbogeneradora
ES8601440A1 (es) Un metodo de mejora del rendimiento y salida de flujo luminoso de una luminaria
ES2136872T3 (es) Turbina de muy alto rendimiento y combinacion de celula de combustible.
PE20010079A1 (es) Sistema y metodo para convertir hidrocarburos ligeros en hidrocarburos mas pesados con multiples subsistemas de gas de sintesis
GB2375085A (en) Engine arrangement
DE60007775D1 (de) Axiallüfter
ES2105929B1 (es) Tobera axisimetrica orientable de geometria variable para propulsores de turbina de gas.
ES8602209A1 (es) Un compresor rotatorio
DE69902147D1 (de) Luftfedervorrichtung
ES2067884T3 (es) Submarino convertible de casco resistente.
ES2009550A6 (es) Una turbomaquina.,particularmente una turbina de vapor con alabes de entrada axil dotados de reducidas fugas y rozamientos con el aire.
ES2100363T3 (es) Aparato para la energia de un fluido.
ES2172903T3 (es) Instalacion de turbinas de gas y de vapor y procedimiento para la refrigeracion del refrigerante de la turbina de gas de una instalacion de este tipo.
TW360895B (en) Glow-lamp with reflection-layer
ES2140358B1 (es) Instalacion de generador eolico y solar de corriente.
ES2163581T3 (es) Amortiguador del ruido en combinacion con un compresor del tipo de husillo y su uso en una fabrica de gas de hornos de coque.
DE602005000373D1 (de) Flugzeug mit vier Druckpropeller
ES2168281T3 (es) Dispositivo para la regulacion de una tension que cae en un consumidor.
CN205717103U (zh) 一种应用于计算机辅助照明的新型灯具散热结构
GB586552A (en) Improvements in or relating to internal combustion turbine plant
Tomozawa The origins of cosmic rays and quantum effects on gravity
ES2052126T3 (es) Aislamiento en una central electrica de turbina de baja presion.
RU94028910A (ru) Выходное устройство газотурбинного двигателя