ES2422587T3 - Fuselaje de aeronave resistente a impactos - Google Patents
Fuselaje de aeronave resistente a impactosInfo
- Publication number
- ES2422587T3 ES2422587T3 ES08853247T ES08853247T ES2422587T3 ES 2422587 T3 ES2422587 T3 ES 2422587T3 ES 08853247 T ES08853247 T ES 08853247T ES 08853247 T ES08853247 T ES 08853247T ES 2422587 T3 ES2422587 T3 ES 2422587T3
- Authority
- ES
- Spain
- Prior art keywords
- fuselage
- aircraft
- risk
- impact
- lining
- 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.)
- Active
Links
- 241001674048 Phthiraptera Species 0.000 abstract 1
- 238000005253 cladding Methods 0.000 abstract 1
- 230000007704 transition Effects 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/12—Construction or attachment of skin panels
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
- B64C1/068—Fuselage sections
- B64C1/0685—Tail cones
-
- 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
- B64D27/04—Aircraft characterised by the type or position of power plants of piston type
- B64D27/08—Aircraft characterised by the type or position of power plants of piston type within, or attached to, fuselages
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
- B64C2001/0054—Fuselage structures substantially made from particular materials
- B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
-
- 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)
- Mechanical Engineering (AREA)
- Tires In General (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Abstract
Fuselaje (20) de una aeronave con motores de hélice (1) que comprenden hélices (23) formadas a su vez porpalas (3), estando los citados motores de hélice (1) ubicados en la parte trasera del fuselaje y estando a su vez elempenaje (5) de la aeronave situado detrás del plano de las hélices (23), caracterizado porque el fuselaje trasero (4)comprende un revestimiento exterior (6), la estructura del fuselaje trasero (4) comprendiendo un revestimiento exterior(6) y un revestimiento interior (7) en el área de riesgo de impacto de la pala (3), estando ambos revestimientos (6, 7)unidos por medio de unos elementos radiales (13) que configuran de este modo unas celdillas (14) cerradasindependientes en el área de riesgo de impacto, de tal forma que las celdillas (14) mejoran la resistencia a torsión delfuselaje trasero (4) de la aeronave en el área de riesgo de impacto de la pala (3) en caso de daño del fuselaje trasero (4)por desprendimiento de una de las palas (3) de los motores de hélice (1), comprendiendo además la configuración unazona de transición (8) del revestimiento interior (7), en la que se une el revestimiento exterior (6) con el revestimientoúnico de otras zonas del fuselaje de la aeronave, longitudinalmente a lo largo del fuselaje de la citada aeronave, encuanto se abandona la zona de riesgo de impacto de la pala (3) del motor de hélice (1).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
ES200703181A ES2342866B1 (es) | 2007-11-30 | 2007-11-30 | Fuselaje de aeronave resistente a impactos. |
PCT/EP2008/066400 WO2009068638A1 (en) | 2007-11-30 | 2008-11-28 | Impact resistant aircraft fuselage |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2422587T3 true ES2422587T3 (es) | 2013-09-12 |
Family
ID=40548870
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES200703181A Expired - Fee Related ES2342866B1 (es) | 2007-11-30 | 2007-11-30 | Fuselaje de aeronave resistente a impactos. |
ES08853247T Active ES2422587T3 (es) | 2007-11-30 | 2008-11-28 | Fuselaje de aeronave resistente a impactos |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES200703181A Expired - Fee Related ES2342866B1 (es) | 2007-11-30 | 2007-11-30 | Fuselaje de aeronave resistente a impactos. |
Country Status (6)
Country | Link |
---|---|
US (1) | US8573538B2 (es) |
EP (1) | EP2279115B1 (es) |
BR (1) | BRPI0821079B1 (es) |
CA (1) | CA2707092C (es) |
ES (2) | ES2342866B1 (es) |
WO (1) | WO2009068638A1 (es) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ES2398287B1 (es) * | 2010-03-29 | 2014-01-29 | Airbus Operations S.L. | Fuselaje de aeronave resistente al impacto y tolerante al daño. |
RU2482015C2 (ru) * | 2011-06-28 | 2013-05-20 | Александр Макарович Матвеенко | Самолет с двойным фюзеляжем |
US20130001356A1 (en) * | 2011-07-01 | 2013-01-03 | Airbus Operations, S.L. | Reinforced aircraft fuselage |
ES2404946B1 (es) * | 2011-10-21 | 2014-09-02 | Airbus Operations S.L. | Fuselaje de aeronave resistente al impacto y tolerante al daño mejorado |
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 |
FR3020347B1 (fr) * | 2014-04-28 | 2016-05-20 | Airbus Operations Sas | Procede d'assemblage d'une partie arriere d'aeronef |
CN104443349B (zh) * | 2014-12-15 | 2017-05-17 | 中国飞机强度研究所 | 一种用于涡桨飞机舱内噪声控制的声学防冰板结构 |
FR3032942B1 (fr) * | 2015-02-19 | 2018-11-23 | Safran Aircraft Engines | Ensemble propulsif pour aeronef comprenant un turboreacteur a soufflante non carenee et un pylone d'accrochage |
EP3106381B1 (en) * | 2015-06-15 | 2018-10-24 | Airbus Operations, S.L. | Aircraft with a protective shield against an engine blade release |
US9630702B2 (en) * | 2015-06-30 | 2017-04-25 | Rohr, Inc. | Noise attenuation for an open rotor aircraft propulsion system |
ES2919960T3 (es) * | 2017-03-15 | 2022-07-29 | Airbus Operations Sl | Fuselaje resistente a impactos |
WO2019045689A1 (en) * | 2017-08-29 | 2019-03-07 | On-Power, Inc. | MOBILE ENERGY GENERATION SYSTEM COMPRISING A CLOSED WALLED BASE STRUCTURE |
US10458334B2 (en) | 2017-08-29 | 2019-10-29 | On-Power, Inc. | Mobile power generation system including closed cell base structure |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2420292A (en) * | 1942-10-23 | 1947-05-13 | Guardite Corp | Airplane body |
US2382817A (en) * | 1943-08-24 | 1945-08-14 | Ernest H Reiss | Protective means for aircraft |
US3020986A (en) * | 1958-08-18 | 1962-02-13 | Gen Dynamics Corp | Composite structural panel |
US3740905A (en) * | 1971-12-22 | 1973-06-26 | Boegin Co | Insulation and condensation control system |
US3867244A (en) * | 1971-12-22 | 1975-02-18 | Boeing Co | Insulation and condensation control blanket |
US4235398A (en) * | 1978-12-18 | 1980-11-25 | The Boeing Company | Thermal insulation for aircraft fuselage |
US4291851A (en) * | 1978-12-18 | 1981-09-29 | The Boeing Company | Thermal insulation for aircraft fuselage |
US4976396A (en) * | 1987-11-13 | 1990-12-11 | The Boeing Company | Aircraft configuration with aft mounted engines |
US5577688A (en) * | 1994-06-15 | 1996-11-26 | Sloan; Frank P. | Containment systems for insulation, and insulation elements employing such systems |
DE19529476C2 (de) * | 1995-08-11 | 2000-08-10 | Deutsch Zentr Luft & Raumfahrt | Flügel mit schubsteifen Flügelschalen aus Faserverbundwerkstoffen für Luftfahrzeuge |
US6231710B1 (en) * | 1999-06-04 | 2001-05-15 | The United States Of America As Represented By The Secretary Of The Air Force | Method of making composite chambercore sandwich-type structure with inherent acoustic attenuation |
SE519185C2 (sv) | 2001-06-07 | 2003-01-28 | Saab Ab | Flygplanspanel |
US7040575B2 (en) * | 2004-03-29 | 2006-05-09 | The Boeing Company | Foam composite insulation for aircraft |
-
2007
- 2007-11-30 ES ES200703181A patent/ES2342866B1/es not_active Expired - Fee Related
-
2008
- 2008-01-30 US US12/012,009 patent/US8573538B2/en active Active
- 2008-11-28 BR BRPI0821079A patent/BRPI0821079B1/pt active IP Right Grant
- 2008-11-28 EP EP08853247.8A patent/EP2279115B1/en active Active
- 2008-11-28 WO PCT/EP2008/066400 patent/WO2009068638A1/en active Application Filing
- 2008-11-28 CA CA2707092A patent/CA2707092C/en not_active Expired - Fee Related
- 2008-11-28 ES ES08853247T patent/ES2422587T3/es active Active
Also Published As
Publication number | Publication date |
---|---|
CA2707092A1 (en) | 2009-06-04 |
ES2342866A1 (es) | 2010-07-15 |
EP2279115A1 (en) | 2011-02-02 |
EP2279115B1 (en) | 2013-04-24 |
US20090140096A1 (en) | 2009-06-04 |
WO2009068638A1 (en) | 2009-06-04 |
BRPI0821079A2 (pt) | 2015-06-16 |
ES2342866B1 (es) | 2011-05-18 |
US8573538B2 (en) | 2013-11-05 |
BRPI0821079B1 (pt) | 2020-04-28 |
CA2707092C (en) | 2016-01-26 |
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