UA88436C2 - Самолет - Google Patents
СамолетInfo
- Publication number
- UA88436C2 UA88436C2 UA20041109234A UA20041109234A UA88436C2 UA 88436 C2 UA88436 C2 UA 88436C2 UA 20041109234 A UA20041109234 A UA 20041109234A UA 20041109234 A UA20041109234 A UA 20041109234A UA 88436 C2 UA88436 C2 UA 88436C2
- Authority
- UA
- Ukraine
- Prior art keywords
- aircraft
- fuselage
- housing
- turbojet engine
- front housing
- Prior art date
Links
- 238000009434 installation Methods 0.000 abstract 1
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
- B64D27/40—Arrangements for mounting power plants in aircraft
-
- 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
- B64D27/20—Aircraft characterised by the type or position of power plants of jet 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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Arrangement Or Mounting Of Propulsion Units For Vehicles (AREA)
Abstract
Самолет имеет турбореактивный двигатель для установки на верхнюю часть хвостовой секции фюзеляжа (1) самолета, в котором используется, по крайней мере, одна "вешалка для одежды" ((28, 128), (28', 128')), при этом турбореактивный двигатель (10) содержит воздушный винт (11), передний корпус (12), задний корпус (18), вспомогательное оборудование (22, 23, 24, 25), которое расположено вблизи периферии переднего корпуса (12), а передний корпус (12) содержит точки ((31, 32, 33), (31', 32', 33')) для крепления "вешалки для одежды" (28, 28'). Точки крепления расположены так, чтобы турбореактивный двигатель (10) мог быть установленным на любой стороне фюзеляжа (1) самолета, причем вспомогательное оборудование (22, 23, 24, 25) размещается на корпусе таким образом, что к нему имеется доступ снаружи фюзеляжа (1), независимо от того, с какой стороны установлен двигатель.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0313245A FR2862045B1 (fr) | 2003-11-12 | 2003-11-12 | Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere |
Publications (1)
Publication Number | Publication Date |
---|---|
UA88436C2 true UA88436C2 (ru) | 2009-10-26 |
Family
ID=34508411
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UA20041109234A UA88436C2 (ru) | 2003-11-12 | 2004-11-11 | Самолет |
Country Status (9)
Country | Link |
---|---|
US (1) | US7007890B2 (ru) |
EP (1) | EP1553019B1 (ru) |
JP (1) | JP4057007B2 (ru) |
CN (1) | CN100537354C (ru) |
CA (1) | CA2485242C (ru) |
DE (1) | DE602004008205T2 (ru) |
FR (1) | FR2862045B1 (ru) |
RU (1) | RU2354587C2 (ru) |
UA (1) | UA88436C2 (ru) |
Families Citing this family (33)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP5156184B2 (ja) * | 2005-09-12 | 2013-03-06 | ザ・ボーイング・カンパニー | 航空機システム、航空機上の逆推力装置を製造するための方法、および逆推力装置上のラッチ機構を動作するための方法 |
FR2891243B1 (fr) * | 2005-09-26 | 2009-04-03 | Airbus France Sas | Mat d'accrochage de moteur pour aeronef |
FR2892705B1 (fr) * | 2005-11-03 | 2009-04-24 | Airbus France Sas | Aeronef a impact environnemental reduit. |
FR2899200B1 (fr) * | 2006-03-28 | 2008-11-07 | Airbus France Sas | Aeronef a impact environnemental reduit |
FR2900906B1 (fr) * | 2006-05-09 | 2009-01-09 | Airbus France Sas | Systeme de fixation tolerant aux dommages pour moteur d'aeronef |
FR2911916B1 (fr) * | 2007-01-30 | 2009-03-27 | Hispano Suiza Sa | Moteur a turbine a gaz incorporant un demarreur monte sur la boite a engrenages |
FR2914907B1 (fr) * | 2007-04-16 | 2009-10-30 | Snecma Sa | Suspension souple avec peigne pour turbomoteur |
US9719428B2 (en) * | 2007-11-30 | 2017-08-01 | United Technologies Corporation | Gas turbine engine with pylon mounted accessory drive |
FR2925877B1 (fr) * | 2007-12-26 | 2009-12-04 | Aircelle Sa | Installation de systeme de guidage sur une nacelle d'aeronef. |
FR2926789B1 (fr) * | 2008-01-29 | 2010-05-28 | Aircelle Sa | Nacelle pour turboreacteur |
US20090205341A1 (en) * | 2008-02-20 | 2009-08-20 | Muldoon Marc J | Gas turbine engine with twin towershaft accessory gearbox |
FR2928181B1 (fr) * | 2008-02-28 | 2010-04-02 | Airbus France | Ensemble moteur pour aeronef comprenant un turboreacteur avec des structures de renfort reliant le carter de soufflante au carter central. |
FR2933071B1 (fr) * | 2008-06-25 | 2010-06-11 | Snecma | Dispositif de capotage de nacelle d'unite de puissance propulsive d'aeronef |
FR2935954B1 (fr) * | 2008-09-18 | 2011-06-03 | Airbus France | Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle. |
FR2935955B1 (fr) * | 2008-09-18 | 2010-10-15 | Airbus France | Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression. |
FR2935953B1 (fr) * | 2008-09-18 | 2010-10-29 | Airbus France | Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef. |
FR2939101B1 (fr) * | 2008-12-01 | 2010-12-31 | Airbus France | Structure rigide de mat d'aeronef plaquee contre une extension laterale de fuselage pour sa fixation |
US9816441B2 (en) * | 2009-03-30 | 2017-11-14 | United Technologies Corporation | Gas turbine engine with stacked accessory components |
FR2970463B1 (fr) | 2011-01-17 | 2013-02-15 | Airbus Operations Sas | Dispositif d'eclissage a tenue mecanique amelioree. |
FR2994942B1 (fr) * | 2012-09-06 | 2015-08-07 | Airbus Operations Sas | Ensemble propulsif lateral pour aeronef comprenant un arceau de support d'un turbomoteur. |
US10266273B2 (en) | 2013-07-26 | 2019-04-23 | Mra Systems, Llc | Aircraft engine pylon |
FR3010699A1 (fr) * | 2013-09-19 | 2015-03-20 | Airbus Operations Sas | Dispositif de carenage pour ensemble propulsif d'aeronef comprenant un compartiment interieur equipe d'un ventilateur |
FR3014840B1 (fr) | 2013-12-17 | 2017-10-13 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur equipe d'au moins une ferrure de support de manille penetrant dans le caisson du mat d'accrochage |
FR3014841B1 (fr) | 2013-12-17 | 2017-12-08 | Airbus Operations Sas | Ensemble pour aeronef comprenant un corps d'attache moteur en partie realise d'une seule piece avec une nervure interieure de rigidification d'un caisson de mat d'accrochage |
FR3015431B1 (fr) | 2013-12-19 | 2017-12-15 | Airbus Operations Sas | Structure primaire de mat d'accrochage renforcee. |
FR3015433B1 (fr) * | 2013-12-23 | 2016-02-12 | Airbus Operations Sas | Ensemble pour aeronef comprenant un mat d'accrochage integre a la nacelle et agence en partie arriere du fuselage |
FR3024435B1 (fr) * | 2014-07-31 | 2016-08-26 | Airbus Operations Sas | Capot de soufflante pliable guide, pour ensemble moteur d'aeronef |
US10072582B2 (en) | 2016-04-28 | 2018-09-11 | General Electric Company | Integral offset oil tank for inline accessory gearbox |
US10723472B2 (en) * | 2017-06-19 | 2020-07-28 | Bell Helicopter Textron Inc. | Two position cowling assembly for single person operation |
US10814995B2 (en) * | 2017-08-29 | 2020-10-27 | Spirit Aerosystems, Inc. | High-mounted aircraft nacelle |
US10836504B2 (en) | 2018-04-26 | 2020-11-17 | Textron Innovations Inc. | Passive particle separation system |
EP3597542A1 (en) * | 2018-07-18 | 2020-01-22 | Rolls-Royce plc | Gas turbine engine mount arrangement |
FR3113485B1 (fr) * | 2020-08-21 | 2022-10-28 | Safran Nacelles | Nacelle pour moteur d’aéronef comportant des capots de soufflante asymétriques |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2863620A (en) * | 1952-10-04 | 1958-12-09 | Sud Aviation | Jet-propelled aircraft |
US3543588A (en) * | 1968-11-12 | 1970-12-01 | Gen Motors Corp | Accessory installation |
GB1262419A (en) * | 1970-07-09 | 1972-02-02 | Rolls Royce | Aircraft engine mountings |
US3714779A (en) * | 1970-09-28 | 1973-02-06 | Avco Corp | Gas turbine engine having a horizontal accessory gear box |
US3809340A (en) * | 1972-12-26 | 1974-05-07 | A Dolgy | Devices for mounting an engine on an aircraft pylon |
US4044973A (en) * | 1975-12-29 | 1977-08-30 | The Boeing Company | Nacelle assembly and mounting structures for a turbofan jet propulsion engine |
US4585189A (en) * | 1984-10-22 | 1986-04-29 | Lockheed Corporation | Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor |
US5443229A (en) * | 1993-12-13 | 1995-08-22 | General Electric Company | Aircraft gas turbine engine sideways mount |
US6357220B1 (en) * | 1998-12-22 | 2002-03-19 | United Technologies Corporation | Gearbox accessory mount |
US6401448B1 (en) * | 2000-08-31 | 2002-06-11 | General Electric Company | System for mounting aircraft engines |
GB0124446D0 (en) * | 2001-10-11 | 2001-12-05 | Short Brothers Ltd | Aircraft propulsive power unit |
-
2003
- 2003-11-12 FR FR0313245A patent/FR2862045B1/fr not_active Expired - Fee Related
-
2004
- 2004-11-10 JP JP2004326238A patent/JP4057007B2/ja active Active
- 2004-11-10 DE DE602004008205T patent/DE602004008205T2/de active Active
- 2004-11-10 EP EP04300782A patent/EP1553019B1/fr active Active
- 2004-11-11 RU RU2004132978/11A patent/RU2354587C2/ru active
- 2004-11-11 UA UA20041109234A patent/UA88436C2/ru unknown
- 2004-11-12 CN CNB2004101047016A patent/CN100537354C/zh active Active
- 2004-11-12 US US10/986,004 patent/US7007890B2/en active Active
- 2004-11-12 CA CA2485242A patent/CA2485242C/fr active Active
Also Published As
Publication number | Publication date |
---|---|
JP4057007B2 (ja) | 2008-03-05 |
FR2862045B1 (fr) | 2006-05-05 |
US20050178887A1 (en) | 2005-08-18 |
US7007890B2 (en) | 2006-03-07 |
EP1553019B1 (fr) | 2007-08-15 |
DE602004008205T2 (de) | 2008-05-08 |
DE602004008205D1 (de) | 2007-09-27 |
RU2354587C2 (ru) | 2009-05-10 |
CA2485242A1 (fr) | 2005-05-12 |
CN1648000A (zh) | 2005-08-03 |
CA2485242C (fr) | 2011-08-30 |
JP2005147146A (ja) | 2005-06-09 |
EP1553019A1 (fr) | 2005-07-13 |
RU2004132978A (ru) | 2006-04-27 |
CN100537354C (zh) | 2009-09-09 |
FR2862045A1 (fr) | 2005-05-13 |
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