ATE268714T1 - Lufteinlass mit verbesserter tragbarkeit für eine triebwerksgondel mit grossen abmessungen - Google Patents

Lufteinlass mit verbesserter tragbarkeit für eine triebwerksgondel mit grossen abmessungen

Info

Publication number
ATE268714T1
ATE268714T1 AT01402147T AT01402147T ATE268714T1 AT E268714 T1 ATE268714 T1 AT E268714T1 AT 01402147 T AT01402147 T AT 01402147T AT 01402147 T AT01402147 T AT 01402147T AT E268714 T1 ATE268714 T1 AT E268714T1
Authority
AT
Austria
Prior art keywords
air intake
engine
nachel
improved portability
large dimensioned
Prior art date
Application number
AT01402147T
Other languages
English (en)
Inventor
Patrick Gonidec
Francois Grigis
Original Assignee
Hurel Hispano
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 Hurel Hispano filed Critical Hurel Hispano
Application granted granted Critical
Publication of ATE268714T1 publication Critical patent/ATE268714T1/de

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
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/08—Inspection panels for power plants
    • 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
    • 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
    • B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
AT01402147T 2000-08-11 2001-08-09 Lufteinlass mit verbesserter tragbarkeit für eine triebwerksgondel mit grossen abmessungen ATE268714T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0010567A FR2812911B1 (fr) 2000-08-11 2000-08-11 Entree d'air pour nacelle de grandes dimensions a transportabilite amelioree

Publications (1)

Publication Number Publication Date
ATE268714T1 true ATE268714T1 (de) 2004-06-15

Family

ID=8853493

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01402147T ATE268714T1 (de) 2000-08-11 2001-08-09 Lufteinlass mit verbesserter tragbarkeit für eine triebwerksgondel mit grossen abmessungen

Country Status (11)

Country Link
US (1) US6837459B2 (de)
EP (1) EP1179473B1 (de)
AT (1) ATE268714T1 (de)
CA (1) CA2394296C (de)
DE (1) DE60103707T2 (de)
ES (1) ES2222968T3 (de)
FR (1) FR2812911B1 (de)
IL (1) IL150658A0 (de)
RU (1) RU2002119705A (de)
UA (1) UA57183C2 (de)
WO (1) WO2002014149A1 (de)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4418168B2 (ja) * 2003-05-14 2010-02-17 本田技研工業株式会社 楕円形環体の製造方法
US7923668B2 (en) * 2006-02-24 2011-04-12 Rohr, Inc. Acoustic nacelle inlet lip having composite construction and an integral electric ice protection heater disposed therein
GB0614640D0 (en) * 2006-07-22 2006-08-30 Rolls Royce Plc An annulus filler seal
FR2906568B1 (fr) * 2006-10-02 2012-01-06 Aircelle Sa Structure d'entree d'air deposable pour nacelle de turboreacteur.
US7837150B2 (en) * 2007-12-21 2010-11-23 Rohr, Inc. Ice protection system for a multi-segment aircraft component
FR2926791B1 (fr) * 2008-01-29 2010-05-28 Aircelle Sa Entree d'air pour nacelle d'aeronef, et ensemble propulsif comprenant une telle entree d'air
FR2931205B1 (fr) * 2008-05-16 2010-05-14 Aircelle Sa Ensemble propulsif pour aeronef, et structure d'entree d'air pour un tel ensemble
US8757540B2 (en) * 2008-06-30 2014-06-24 Pratt & Whitney Canada Corp. Nacelle inlet lip
WO2010102635A2 (en) * 2009-03-13 2010-09-16 Vestas Wind Systems A/S Wind turbine nacelle
RU2389653C1 (ru) * 2009-04-10 2010-05-20 Эдуард Дмитриевич Житников Гондола с внутренним крылом
FR2961789B1 (fr) * 2010-06-24 2012-07-20 Eurocopter France Procede pour eviter le colmatage d'une grille, grille et entree d'air mettant en oeuvre un tel procede
US9663238B2 (en) * 2013-11-11 2017-05-30 The Boeing Company Nacelle inlet lip skin with pad-up defining a developable surface having parallel ruling lines
FR3033545B1 (fr) * 2015-03-12 2018-08-10 Airbus Operations Nacelle pour ensemble moteur d'aeronef comprenant au moins un capot de nacelle articule a son extremite avant
FR3060650B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Structure d'entree d'air pour une nacelle d'aeronef
FR3081837B1 (fr) * 2018-06-05 2020-11-27 Airbus Operations Sas Ensemble turbomachine d'aeronef comportant un capot articule
FR3083777B1 (fr) * 2018-07-10 2021-03-05 Airbus Operations Sas Entree d'air, nacelle et ensemble propulsif d'aeronef a secteurs monoblocs
FR3085353A1 (fr) * 2018-09-04 2020-03-06 Airbus Operations Ensemble turbomachine d'aeronef comportant un capot articule
FR3092871B1 (fr) * 2019-02-15 2022-02-25 Airbus Operations Sas Procede d’assemblage d’une entree d’air d’un turboreacteur d’aeronef
CN110816885A (zh) * 2019-11-07 2020-02-21 中国科学院光电研究院 一种浮空器结冰特性数值仿真与试验验证系统

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3271806D1 (en) * 1982-12-27 1986-07-24 Boeing Co Inlet cowl attachment for jet engine
FR2731049B1 (fr) * 1995-02-28 1997-05-09 Aerospatiale Dispositif de fixation d'une bouche d'entree d'air sur un reacteur et reacteur comportant un tel dispositif
FR2757823B1 (fr) * 1996-12-26 1999-03-12 Aerospatiale Nacelle de turboreacteur a ecoulement laminaire
FR2771776B1 (fr) * 1997-12-02 2000-01-28 Aerospatiale Dispositif d'evacuation d'air chaud pour capot d'entree d'air de moteur a reaction, a circuit de degivrage
FR2787509B1 (fr) * 1998-12-21 2001-03-30 Aerospatiale Structure d'entree d'air pour moteur d'aeronef

Also Published As

Publication number Publication date
RU2002119705A (ru) 2004-01-27
US20040000615A1 (en) 2004-01-01
WO2002014149A1 (fr) 2002-02-21
ES2222968T3 (es) 2005-02-16
FR2812911B1 (fr) 2002-09-20
EP1179473B1 (de) 2004-06-09
CA2394296A1 (fr) 2002-02-21
DE60103707D1 (de) 2004-07-15
FR2812911A1 (fr) 2002-02-15
IL150658A0 (en) 2003-02-12
UA57183C2 (uk) 2003-06-16
DE60103707T2 (de) 2005-06-30
CA2394296C (fr) 2007-10-09
US6837459B2 (en) 2005-01-04
EP1179473A1 (de) 2002-02-13

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Legal Events

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