BRPI0516069A - empenagem vertical para aeronave munida dessa empenagem - Google Patents

empenagem vertical para aeronave munida dessa empenagem

Info

Publication number
BRPI0516069A
BRPI0516069A BRPI0516069-3A BRPI0516069A BRPI0516069A BR PI0516069 A BRPI0516069 A BR PI0516069A BR PI0516069 A BRPI0516069 A BR PI0516069A BR PI0516069 A BRPI0516069 A BR PI0516069A
Authority
BR
Brazil
Prior art keywords
buckling
vertical
aircraft
drift
engine
Prior art date
Application number
BRPI0516069-3A
Other languages
English (en)
Inventor
Bernard Guering
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Publication of BRPI0516069A publication Critical patent/BRPI0516069A/pt

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
    • 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—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
    • B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
    • B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
    • B64D2033/0293—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for turboprop engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Packaging Of Machine Parts And Wound Products (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
  • Tents Or Canopies (AREA)
  • Retarders (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Body Structure For Vehicles (AREA)
  • Tires In General (AREA)
  • Rolling Contact Bearings (AREA)

Abstract

''EMPENAGEM VERTICAL PARA AERONAVE MUNIDA DESSA EMPENAGEM". A invenção se refere a uma empenagem vertical (5) para aeronave (1). A empenagem vertical é munida de um motor (7). O motor se estende sem suporte além de uma deriva (11) da empenagem vertical e é solidarizado a essa deriva por meio de uma armação (12). Essa armação é pelo menos parcialmente fixado na deriva. A armação comporta, por exemplo, uma pluralidade de semi-arcos 10 (17) dispostos de ambos os lados da deriva. A invenção se refere também a uma aeronave (1), munida de uma empenagem vertical (5), que sustenta um motor (7).
BRPI0516069-3A 2004-10-15 2005-09-23 empenagem vertical para aeronave munida dessa empenagem BRPI0516069A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0452348A FR2876658B1 (fr) 2004-10-15 2004-10-15 Empennage vertical pour aeronef et aeronef muni d'un tel empennage
PCT/FR2005/050770 WO2006042982A1 (fr) 2004-10-15 2005-09-23 Empennage vertical pour aéronef et aéronef muni d'un tel empennage

Publications (1)

Publication Number Publication Date
BRPI0516069A true BRPI0516069A (pt) 2008-08-19

Family

ID=34950022

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0516069-3A BRPI0516069A (pt) 2004-10-15 2005-09-23 empenagem vertical para aeronave munida dessa empenagem

Country Status (11)

Country Link
US (1) US7581694B2 (pt)
EP (1) EP1799549B1 (pt)
JP (1) JP4418000B2 (pt)
CN (1) CN100430300C (pt)
AT (1) ATE392361T1 (pt)
BR (1) BRPI0516069A (pt)
CA (1) CA2582684C (pt)
DE (1) DE602005006147T2 (pt)
FR (1) FR2876658B1 (pt)
RU (1) RU2346854C1 (pt)
WO (1) WO2006042982A1 (pt)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2891242B1 (fr) * 2005-09-23 2007-10-26 Airbus France Sas Turboreacteur pour aeronef, aeronef muni d'un tel turboreacteur, et procede de montage d'un tel turboreacteur sur un aeronef
FR2899200B1 (fr) * 2006-03-28 2008-11-07 Airbus France Sas Aeronef a impact environnemental reduit
DE102008011643A1 (de) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Flugzeugantriebseinheit mit Multi-Fan-Ausgestaltung
FR2935353B1 (fr) * 2008-09-03 2010-09-10 Airbus France Mat pour la suspension d'un turbomoteur sous une aile d'aeronef
DE102008062813A1 (de) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einer Heck-Propeller-Triebwerksanordnung
GB201102987D0 (en) * 2011-02-22 2011-04-06 Rolls Royce Plc A propfan engine
US8740139B1 (en) * 2012-04-23 2014-06-03 The Boeing Company Leading edge snag for exposed propeller engine installation
US9644537B2 (en) * 2013-03-14 2017-05-09 United Technologies Corporation Free stream intake with particle separator for reverse core engine
FR3020347B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Procede d'assemblage d'une partie arriere d'aeronef
FR3039133B1 (fr) * 2015-07-22 2020-01-17 Safran Aircraft Engines Aeronef avec un ensemble propulsif comprenant une soufflante a l'arriere du fuselage
FR3043723B1 (fr) * 2015-11-13 2017-11-24 Snecma Ensemble de propulsion d'un aeronef comportant un generateur de gaz, deux soufflantes deportees et une manche d'entree d'air
US10800539B2 (en) * 2016-08-19 2020-10-13 General Electric Company Propulsion engine for an aircraft

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2499350A (en) * 1945-01-17 1950-03-07 Theodore C Bennett Floating wing airplane
US3666211A (en) * 1970-03-12 1972-05-30 Mc Donnell Douglas Corp Trijet aircraft
GB1364313A (en) * 1971-02-05 1974-08-21 Britten Norman Ltd Aircraft
US4456204A (en) * 1981-09-29 1984-06-26 The Boeing Company Deployable inlet for aeroplane center boost engine
US4871130A (en) * 1988-06-21 1989-10-03 Walter Schulze Propulsion apparatus for an aircraft
US6113028A (en) * 1996-02-22 2000-09-05 Lohse; James R. Amphibious aircraft
EP1046577A3 (en) * 1999-04-19 2001-07-11 Conway Holdings, Ltd. Single engined aircraft
US6575406B2 (en) * 2001-01-19 2003-06-10 The Boeing Company Integrated and/or modular high-speed aircraft

Also Published As

Publication number Publication date
ATE392361T1 (de) 2008-05-15
CA2582684C (fr) 2009-08-04
JP4418000B2 (ja) 2010-02-17
EP1799549A1 (fr) 2007-06-27
JP2008516834A (ja) 2008-05-22
DE602005006147T2 (de) 2009-05-07
RU2007117896A (ru) 2008-11-20
FR2876658A1 (fr) 2006-04-21
CN100430300C (zh) 2008-11-05
EP1799549B1 (fr) 2008-04-16
WO2006042982A1 (fr) 2006-04-27
FR2876658B1 (fr) 2007-01-19
DE602005006147D1 (de) 2008-05-29
US20070284477A1 (en) 2007-12-13
RU2346854C1 (ru) 2009-02-20
CA2582684A1 (fr) 2006-04-27
US7581694B2 (en) 2009-09-01
CN101039840A (zh) 2007-09-19

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Legal Events

Date Code Title Description
B25A Requested transfer of rights approved

Owner name: AIRBUS OPERATIONS SAS (FR)

Free format text: TRANSFERIDO POR INCORPORACAO DE: AIRBUS FRANCE

B06F Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B11D Dismissal acc. art. 38, par 2 of ipl - failure to pay fee after grant in time