BRPI0813043A2 - "nacela de motor a jato de turboventoinha" - Google Patents

"nacela de motor a jato de turboventoinha"

Info

Publication number: BRPI0813043A2
Authority: BR; Brazil
Prior art keywords: turboventine; nacela; jet engine; jet; engine
Prior art date: 2007-08-20

Application number

BRPI0813043-4A2A

Other languages

English (en)

Inventor

Florent Bouillon

Pat Dunleavy

Original Assignee

Aircelle Sa

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.)

2007-08-20

Filing date

2008-06-20

Publication date

2014-12-16

2008-06-20 Application filed by Aircelle Sa filed Critical Aircelle Sa

2014-12-16 Publication of BRPI0813043A2 publication Critical patent/BRPI0813043A2/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
- B64D29/00—Power-plant nacelles, fairings, or cowlings
- B64D29/08—Inspection panels for power plants

Landscapes

Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)

BRPI0813043-4A2A 2007-08-20 2008-06-20 "nacela de motor a jato de turboventoinha" BRPI0813043A2 (pt)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0705890A FR2920136B1 (fr)	2007-08-20	2007-08-20	Systeme de liaison entre une structure interne et un structure externe d'une nacelle
PCT/FR2008/000864 WO2009024662A2 (fr)	2007-08-20	2008-06-20	Systeme de liaison entre une structure interne et une structure externe d'une nacelle de turboreacteur

Publications (1)

Publication Number	Publication Date
BRPI0813043A2 true BRPI0813043A2 (pt)	2014-12-16

Family

ID=39259543

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0813043-4A2A BRPI0813043A2 (pt)	2007-08-20	2008-06-20	"nacela de motor a jato de turboventoinha"

Country Status (9)

Country	Link
US (1)	US20110094204A1 (pt)
EP (1)	EP2178755B1 (pt)
CN (1)	CN101778765B (pt)
BR (1)	BRPI0813043A2 (pt)
CA (1)	CA2696359C (pt)
ES (1)	ES2400729T3 (pt)
FR (1)	FR2920136B1 (pt)
RU (1)	RU2483984C2 (pt)
WO (1)	WO2009024662A2 (pt)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US9161820B2 (en)	2004-10-28	2015-10-20	Nico Corporation	Surgical access assembly and method of using same
US9579121B2 (en)	2004-10-28	2017-02-28	Nico Corporation	Holding arrangement for a surgical access system
US20110101158A1 (en) *	2005-03-29	2011-05-05	The Boeing Company	Thrust Reversers Including Monolithic Components
US9708073B2 (en) *	2014-08-22	2017-07-18	Rohr, Inc.	Automatic deflection limiting latches for a thrust reverser
FR3057618A1 (fr) *	2016-10-17	2018-04-20	Airbus	Nacelle d'un turboreacteur comportant un volet inverseur
CN109956044B (zh) *	2017-12-22	2022-03-11	空中客车运营简化股份公司	喷气发动机的短舱
GB201806563D0 (en)	2018-04-23	2018-06-06	Rolls Royce Plc	Gas turbine engine keel beam
GB201806564D0 (en)	2018-04-23	2018-06-06	Rolls Royce Plc	Gas turbine engine inner barrel
CN110065639A (zh) *	2019-05-09	2019-07-30	西北工业大学	一种用于无人机快卸对开式动力舱罩

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3541794A (en) *	1969-04-23	1970-11-24	Gen Electric	Bifurcated fan duct thrust reverser
US4044973A (en) *	1975-12-29	1977-08-30	The Boeing Company	Nacelle assembly and mounting structures for a turbofan jet propulsion engine
US4365775A (en) *	1980-12-08	1982-12-28	The Boeing Company	Cowl structure alignment and shear device
US4679750A (en) *	1984-06-20	1987-07-14	The Boeing Company	Latch system
US4585189A (en) *	1984-10-22	1986-04-29	Lockheed Corporation	Counterbalanced cowling assembly for a pylon-mounted engine and nacelle therefor
FR2613773B1 (fr) *	1987-04-08	1990-11-30	Snecma	Panneau acoustique pour garniture insonorisante et turboreacteur comportant une telle garniture
GB8822798D0 (en) *	1988-09-28	1988-11-02	Short Brothers Ltd	Ducted fan turbine engine
FR2756323B1 (fr) *	1996-11-28	1998-12-31	Hispano Suiza Sa	Dispositif de liaison d'un inverseur de poussee a un turbomoteur
DE19649518A1 (de) *	1996-11-29	1998-06-04	Daimler Benz Ag	Linearer Synchronmotor mit passivem Stator
FR2856379B1 (fr) *	2003-06-18	2006-11-24	Airbus France	Moteur d'avion dont les capots de soufflante et d'inverseurs de poussee sont separes par un jeu reduit
US7083144B2 (en) *	2004-08-18	2006-08-01	The Boeing Company	Apparatus and methods for support of propulsion systems interconnect members
FR2896481B1 (fr) *	2006-01-23	2009-12-04	Aircelle Sa	Systeme de fixation pour element constitutif d'une nacelle de turboreacteur

2007
- 2007-08-20 FR FR0705890A patent/FR2920136B1/fr not_active Expired - Fee Related
2008
- 2008-06-20 BR BRPI0813043-4A2A patent/BRPI0813043A2/pt not_active IP Right Cessation
- 2008-06-20 WO PCT/FR2008/000864 patent/WO2009024662A2/fr active Application Filing
- 2008-06-20 CN CN200880103135.3A patent/CN101778765B/zh not_active Expired - Fee Related
- 2008-06-20 ES ES08827805T patent/ES2400729T3/es active Active
- 2008-06-20 RU RU2010109816/11A patent/RU2483984C2/ru not_active IP Right Cessation
- 2008-06-20 EP EP08827805A patent/EP2178755B1/fr active Active
- 2008-06-20 US US12/673,259 patent/US20110094204A1/en not_active Abandoned
- 2008-06-20 CA CA2696359A patent/CA2696359C/fr not_active Expired - Fee Related

Also Published As

Publication number	Publication date
EP2178755A2 (fr)	2010-04-28
RU2010109816A (ru)	2011-09-27
WO2009024662A3 (fr)	2009-04-16
EP2178755B1 (fr)	2012-12-05
CN101778765B (zh)	2015-01-21
CA2696359A1 (fr)	2009-02-26
CA2696359C (fr)	2015-03-31
FR2920136B1 (fr)	2009-10-30
RU2483984C2 (ru)	2013-06-10
FR2920136A1 (fr)	2009-02-27
US20110094204A1 (en)	2011-04-28
ES2400729T3 (es)	2013-04-11
WO2009024662A2 (fr)	2009-02-26
CN101778765A (zh)	2010-07-14

Legal Events

Date	Code	Title	Description
2017-04-18	B08F	Application fees: application dismissed [chapter 8.6 patent gazette]
2017-08-01	B08K	Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Publication	Publication Date	Title
BRPI0720329A2 (pt)	2013-12-24	" nacela de motor a jato de aeronave "
BRPI0813042A2 (pt)	2014-12-16	"nacela para um motor a jato"
BRPI0813043A2 (pt)	2014-12-16	"nacela de motor a jato de turboventoinha"
BRPI0817123A2 (pt)	2015-03-31	Motor a diesel
GB2442337B (en)	2011-02-09	Turbofan jet engine
GB2450778B (en)	2009-09-09	Turbine engine driving auxiliary component
EP2084061A4 (en)	2013-07-24	SUPERSONIC AIRCRAFT REACTOR
DE602007009347D1 (de)	2010-11-04	Hilfstriebwerkanordnung
BRPI0818465A2 (pt)	2015-04-14	Arranjo em um motor de combustão superalimentado
BRPI0813049A2 (pt)	2014-12-16	"inversor de empuxo para nacela de motor a jato"
EP2032829A4 (en)	2012-10-10	ENGINE EXHAUST SYSTEM WITH DIRECTIONAL NOZZLE
EP1992804A4 (en)	2011-08-03	TWO-STROKE ENGINE
IL176194A0 (en)	2006-10-05	Turbine engine nozzle
GB2443946B (en)	2011-07-20	Turbofan engine nozzle assembly
DE602008005797D1 (de)	2011-05-12	Motor
EP1908918A4 (en)	2009-01-21	JET STEAM ENGINE
BRPI0814484A8 (pt)	2018-12-11	motor a jato de fluxo duplo para aeronave
BRPI0908325A2 (pt)	2018-07-17	motor a jato de fluxo duplo para aernonave
AU315982S (en)	2007-09-05	Engine shroud
BRPI0813610A2 (pt)	2014-12-30	"nacela para um motor turbojato"
BRPI0819562A2 (pt)	2015-05-05	"equipamento de aquecimento de combustível de um motor a diesel"
ZA200903385B (en)	2010-01-27	Vehicle engine
EP1890003A4 (en)	2011-08-24	JET STEAM ENGINE
PL2022950T3 (pl)	2016-09-30	Maszyna przepływowa i wyporowa
DE602007002517D1 (de)	2009-11-05	Motor