BRPI0815492A2 - Cone de ejeção de gases para turborreator de aeronave e turborreator e conjunto motor para aeronave - Google Patents

Cone de ejeção de gases para turborreator de aeronave e turborreator e conjunto motor para aeronave

Info

Publication number: BRPI0815492A2
Authority: BR; Brazil
Prior art keywords: aircraft; turborreactor; gas ejection; engine assembly; ejection cone
Prior art date: 2007-08-23

Application number

BRPI0815492-9A2A

Other languages

English (en)

Inventor

Frederic Journade

Jerome Journade

Jerome Hubert

Original Assignee

Airbus Operations Sas

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.)

2007-08-23

Filing date

2008-08-21

Publication date

2015-02-10

2008-08-21 Application filed by Airbus Operations Sas filed Critical Airbus Operations Sas

2015-02-10 Publication of BRPI0815492A2 publication Critical patent/BRPI0815492A2/pt

Classifications

- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/04—Mounting of an exhaust cone in the jet pipe
- 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
- B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D33/06—Silencing exhaust or propulsion jets
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/06—Varying effective area of jet pipe or nozzle
- F02K1/08—Varying effective area of jet pipe or nozzle by axially moving or transversely deforming an internal member, e.g. the exhaust cone
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
- F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
- F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
- F02K3/06—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type with front fan

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Aviation & Aerospace Engineering (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
Acyclic And Carbocyclic Compounds In Medicinal Compositions (AREA)

BRPI0815492-9A2A 2007-08-23 2008-08-21 Cone de ejeção de gases para turborreator de aeronave e turborreator e conjunto motor para aeronave BRPI0815492A2 (pt)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
FR0757137A FR2920194B1 (fr)	2007-08-23	2007-08-23	Cone d'ejection des gaz pour turboreacteur d'aeronef equipe d'un dispositif de generation de turbulences de flux primaire limitant le bruit de jet
PCT/EP2008/060932 WO2009024594A1 (fr)	2007-08-23	2008-08-21	Cone d'ejection des gaz pour turboreacteur d'aeronef equipe d'un dispositif de generation de turbulences de flux primaire limitant le bruit de jet, et turboreacteur et ensemble moteur associes

Publications (1)

Publication Number	Publication Date
BRPI0815492A2 true BRPI0815492A2 (pt)	2015-02-10

Family

ID=39186407

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0815492-9A2A BRPI0815492A2 (pt)	2007-08-23	2008-08-21	Cone de ejeção de gases para turborreator de aeronave e turborreator e conjunto motor para aeronave

Country Status (9)

Country	Link
US (1)	US8516824B2 (pt)
EP (1)	EP2191124B1 (pt)
JP (1)	JP5215395B2 (pt)
CN (1)	CN101772635B (pt)
BR (1)	BRPI0815492A2 (pt)
CA (1)	CA2696178C (pt)
FR (1)	FR2920194B1 (pt)
RU (1)	RU2482310C2 (pt)
WO (1)	WO2009024594A1 (pt)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2988434B1 (fr) *	2012-03-20	2016-02-05	Aircelle Sa	Cone d'ejection des gaz pour turboreacteurs d'aeronefs
FR2994460B1 (fr) *	2012-08-09	2018-04-27	Safran Aircraft Engines	Cone d'ejection pour turbomachine comportant des moyens d'aspiration de couche limite d'un flux d'air
FR2997997B1 (fr) *	2012-11-12	2014-12-26	Snecma	Support de tube d'evacuation d'air dans une turbomachine
CN106968831A (zh) *	2016-01-14	2017-07-21	王佐良	一种舵式矢量发动机
US11248561B2 (en) *	2019-12-18	2022-02-15	Rolls-Royce Deutschland Ltd & Co Kg	Exhaust nozzle of a gas turbine engine
CN113503364B (zh) *	2021-09-09	2021-11-26	中国空气动力研究与发展中心高速空气动力研究所	一种节流锥流量调节装置
CN115030837B (zh) *	2022-08-10	2022-11-08	中国空气动力研究与发展中心低速空气动力研究所	一种喷口降噪装置

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US2585270A (en)	1945-03-12	1952-02-12	Boeing Co	Adjustable jet nozzle for aircraft propulsion
US2583570A (en) *	1945-06-28	1952-01-29	Clarence N Hickman	Nozzle for rocket motors
US2557883A (en) *	1947-09-17	1951-06-19	Ernest F Miller	Jet propulsion exhaust nozzle apparatus
SU75548A1 (ru) *	1948-07-13	1948-11-30	А.Н. Новидарский	Механизм дл перемещени подвижного конуса реактивного сопла турбореактивного двигател
US2771740A (en) *	1950-11-16	1956-11-27	Lockheed Aircraft Corp	Afterburning means for turbo-jet engines
BE530004A (pt) *	1953-06-30
US2825603A (en)	1953-11-10	1958-03-04	Mary E Altergott	Spraying device
GB792831A (en)	1955-03-11	1958-04-02	Power Jets Res & Dev Ltd	An improved gas-flow control device for a jet-propulsion plant
US3174282A (en) *	1963-04-19	1965-03-23	Ryan Aeronautical Co	Asymmetrical jet nozzle noise suppressor
FR1478475A (fr)	1966-03-03	1967-04-28		Régulateur de l'ouverture de la tuyère d'un réacteur
US3572464A (en) *	1969-10-06	1971-03-30	Rohr Corp	Method and apparatus for suppressing the noise of a fan-jet engine
BE756228R (pt) *	1970-03-02	1971-03-01	Gen Electric
US5038559A (en) *	1981-12-22	1991-08-13	Allied-Signal Inc.	Method and apparatus for selectively varying an effective fluid flow area of a jet engine exhaust nozzle
FR2868131B1 (fr)	2004-03-25	2006-06-09	Airbus France Sas	Tuyere primaire a chevrons pour turboreacteur a double flux d'aeronef et aeronef comportant une telle tuyere

2007
- 2007-08-23 FR FR0757137A patent/FR2920194B1/fr not_active Expired - Fee Related
2008
- 2008-08-21 CA CA2696178A patent/CA2696178C/en not_active Expired - Fee Related
- 2008-08-21 JP JP2010521425A patent/JP5215395B2/ja not_active Expired - Fee Related
- 2008-08-21 RU RU2010110826/06A patent/RU2482310C2/ru not_active IP Right Cessation
- 2008-08-21 BR BRPI0815492-9A2A patent/BRPI0815492A2/pt not_active IP Right Cessation
- 2008-08-21 CN CN2008801014339A patent/CN101772635B/zh not_active Expired - Fee Related
- 2008-08-21 US US12/673,125 patent/US8516824B2/en not_active Expired - Fee Related
- 2008-08-21 EP EP08787376.6A patent/EP2191124B1/fr not_active Not-in-force
- 2008-08-21 WO PCT/EP2008/060932 patent/WO2009024594A1/fr not_active Ceased

Also Published As

Publication number	Publication date
FR2920194A1 (fr)	2009-02-27
RU2482310C2 (ru)	2013-05-20
US20110203254A1 (en)	2011-08-25
JP2011511195A (ja)	2011-04-07
CN101772635B (zh)	2013-05-08
CA2696178A1 (en)	2009-02-26
RU2010110826A (ru)	2011-09-27
US8516824B2 (en)	2013-08-27
WO2009024594A1 (fr)	2009-02-26
JP5215395B2 (ja)	2013-06-19
CA2696178C (en)	2016-01-05
EP2191124B1 (fr)	2015-10-07
FR2920194B1 (fr)	2014-02-21
CN101772635A (zh)	2010-07-07
EP2191124A1 (fr)	2010-06-02

Publication	Publication Date	Title
BRPI0717730A2 (pt)	2013-10-22	Nacela para motor turbojato de contorno, conjunto de propulsão e avião
BRPI0908079A2 (pt)	2015-08-25	Conjunto motor para aeronave, e, aeronave
GB2422875B (en)	2007-11-14	Systems and methods for starting aircraft engines
BRPI0907771A2 (pt)	2015-07-14	Conjunto motor para aeronave, e, aeronave
BRPI0821504A2 (pt)	2016-01-19	nacela para motor de avião
EP2084061A4 (en)	2013-07-24	SUPERSONIC AIRCRAFT REACTOR
BRPI0812844A2 (pt)	2014-12-09	Estribo de afixação para motor de aeronave, conjunto motor para aeronave, e, aeronave
PL1902953T3 (pl)	2018-12-31	Silnik śmigłowca z turbiną gazową
GB2473578B (en)	2011-08-03	Gas turbine engine system
GB2436708B (en)	2011-07-27	Auxiliary gas turbine engine assembly, aircraft component and controller
BRPI0821929A2 (pt)	2015-06-16	Nacela para motor turbojato
BRPI1007029A2 (pt)	2016-02-10	conjunto de suspensão para motor turbojato de aeronaves
BR112014001679A2 (pt)	2017-03-07	cone de escape para motor turbojato de aeronave
IL182789A0 (en)	2007-08-19	Propulsion gas exhaust assembly in an aircraft forming an elbow
BR112013005595A2 (pt)	2016-05-03	aparelho de propulsão e motor de turbina a gás de aeronave
BRPI0922745A2 (pt)	2016-01-05	ventoinha para turbomáquina de aeronave e turbomáquina para aeronave.
BRPI0921975A2 (pt)	2016-01-05	reversor de empuxo para nacela de motor turbofan, nacela de motor turbofan e aeronave.
BRPI0815492A2 (pt)	2015-02-10	Cone de ejeção de gases para turborreator de aeronave e turborreator e conjunto motor para aeronave
GB2473651B (en)	2011-08-31	Gas turbine aircraft engines and operation thereof
GB2455181B (en)	2012-12-26	Methods and systems for reducing the emissions from combustion gases
GB0616740D0 (en)	2006-10-04	Aircraft engine thrust reverser
BR112014001529A2 (pt)	2017-02-14	nacela de motor turbojato compreendendo uma parte fixa e um meio reversor de empuxo
BRPI0911572A2 (pt)	2018-04-03	unidade de propulsão para uma aeronave e estrutura de entrada de ar para a referida unidade de propulsão
BRPI0810535A2 (pt)	2014-10-21	Nacela para turbojato e avião.
BRPI0822127A2 (pt)	2015-06-23	Nacela para motor turbojato e aeronave

Legal Events

Date	Code	Title	Description
2016-09-20	B08F	Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]	Free format text: REFERENTE A 8A ANUIDADE.
2017-01-17	B08K	Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]	Free format text: EM VIRTUDE DO ARQUIVAMENTO PUBLICADO NA RPI 2385 DE 20-09-2016 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDO O ARQUIVAMENTO DO PEDIDO DE PATENTE, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.