BRPI0914134A2 - conjunto de componentes e estrutura de entrada de ar - Google Patents

conjunto de componentes e estrutura de entrada de ar

Info

Publication number: BRPI0914134A2
Authority: BR; Brazil
Prior art keywords: air inlet; inlet structure; component set; component; air
Prior art date: 2008-07-30

Application number

BRPI0914134A

Other languages

English (en)

Inventor

Guillaume Ruckert

Guy Bernard Vauchel

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.)

2008-07-30

Filing date

2009-07-28

Publication date

2015-10-20

2008-07-30 Priority claimed from FR0804348A external-priority patent/FR2934641B1/fr

2008-11-06 Priority claimed from FR0806196A external-priority patent/FR2938014B1/fr

2008-12-22 Priority claimed from FR0807350A external-priority patent/FR2940377B1/fr

2009-07-28 Application filed by Aircelle Sa filed Critical Aircelle Sa

2015-10-20 Publication of BRPI0914134A2 publication Critical patent/BRPI0914134A2/pt

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
- 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
- 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
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/02—De-icing or preventing icing on exterior surfaces of aircraft by ducted hot gas or liquid
- B64D15/04—Hot gas application
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/045—Air intakes for gas-turbine plants or jet-propulsion plants having provisions for noise suppression
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
- F02C7/047—Heating to prevent icing
- 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
- B64D2033/0206—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising noise reduction means, e.g. acoustic liners
- 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
- B64D2033/0233—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes comprising de-icing means
- 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
- B64D2033/0266—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/0286—Arrangement 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 turbofan engines
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/96—Preventing, counteracting or reducing vibration or noise
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/0536—Highspeed fluid intake means [e.g., jet engine intake]
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12479—Porous [e.g., foamed, spongy, cracked, etc.]
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24149—Honeycomb-like
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/24—Structurally defined web or sheet [e.g., overall dimension, etc.]
- Y10T428/24273—Structurally defined web or sheet [e.g., overall dimension, etc.] including aperture
- Y10T428/24322—Composite web or sheet
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249967—Inorganic matrix in void-containing component
- Y10T428/24997—Of metal-containing material
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249976—Voids specified as closed
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249953—Composite having voids in a component [e.g., porous, cellular, etc.]
- Y10T428/249982—With component specified as adhesive or bonding agent
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/50—FELT FABRIC
- Y10T442/59—At least three layers

Landscapes

Engineering & Computer Science (AREA)
Chemical & Material Sciences (AREA)
Combustion & Propulsion (AREA)
Aviation & Aerospace Engineering (AREA)
Mechanical Engineering (AREA)
General Engineering & Computer Science (AREA)
Laminated Bodies (AREA)
Structures Of Non-Positive Displacement Pumps (AREA)
Soundproofing, Sound Blocking, And Sound Damping (AREA)
External Artificial Organs (AREA)
Separation Using Semi-Permeable Membranes (AREA)

BRPI0914134A 2008-07-30 2009-07-28 conjunto de componentes e estrutura de entrada de ar BRPI0914134A2 (pt)

Applications Claiming Priority (4)

Application Number	Priority Date	Filing Date	Title
FR0804348A FR2934641B1 (fr)	2008-07-30	2008-07-30	Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
FR0806196A FR2938014B1 (fr)	2008-11-06	2008-11-06	Panneau d'attenuation acoustique pour nacelle de moteur d'aeronef
FR0807350A FR2940377B1 (fr)	2008-12-22	2008-12-22	Ensemble de pieces reliees entre elles par un dispositif permettant de conserver l'integrite de la surface de l'une des pieces
PCT/FR2009/000934 WO2010012899A2 (fr)	2008-07-30	2009-07-28	Ensemble de pièces reliées entre elles par un dispositif permettant de conserver l'intégrité de la surface de l'une des pièces

Publications (1)

Publication Number	Publication Date
BRPI0914134A2 true BRPI0914134A2 (pt)	2015-10-20

Family

ID=41402585

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BRPI0914134A BRPI0914134A2 (pt)	2008-07-30	2009-07-28	conjunto de componentes e estrutura de entrada de ar

Country Status (7)

Country	Link
US (1)	US8840059B2 (pt)
EP (1)	EP2321510B1 (pt)
CN (1)	CN102099556B (pt)
BR (1)	BRPI0914134A2 (pt)
CA (1)	CA2732351A1 (pt)
ES (1)	ES2425078T3 (pt)
WO (1)	WO2010012899A2 (pt)

Families Citing this family (28)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
FR2952032B1 (fr) *	2009-11-05	2012-04-06	Airbus Operations Sas	Nacelle d'aeronef comprenant un systeme de traitement acoustique optimise
GB201116337D0 (en) *	2011-09-21	2011-11-02	Airbus Operations Ltd	Bleed air duct joint insulation means
FR2980775B1 (fr) *	2011-10-03	2014-07-11	Airbus Operations Sas	Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins une chambre de stabilisation
FR2980776B1 (fr)	2011-10-03	2014-08-22	Airbus Operations Sas	Nacelle d'aeronef comportant un panneau pour le traitement acoustique integrant des canaux d'air chaud et au moins un canal annulaire
FR2996525B1 (fr) *	2012-10-09	2014-11-28	Aircelle Sa	Element constitutif d’une nacelle a protection contre le givre amelioree
FR3004485B1 (fr) *	2013-04-11	2015-05-08	Snecma	Dispositif de degivrage d'un bec de separation de turbomachine aeronautique
DE102014114575A1 (de) *	2014-06-23	2015-12-24	Von Ardenne Gmbh	Transportvorrichtung, Prozessieranordnung und Beschichtungsverfahren
US20160084108A1 (en) *	2014-09-24	2016-03-24	Honeywell International Inc.	Nacelle inlet and engine fan housing assembly and method for making same
US10156243B2 (en) *	2015-05-04	2018-12-18	Safran Aero Boosters Sa	Composite splitter lip for axial turbomachine compressor
US9771868B2 (en)	2015-07-21	2017-09-26	The Boeing Company	Sound attenuation apparatus and method
US9587563B2 (en)	2015-07-21	2017-03-07	The Boeing Company	Sound attenuation apparatus and method
US10393020B2 (en) *	2015-08-26	2019-08-27	Rohr, Inc.	Injector nozzle configuration for swirl anti-icing system
US10794398B2 (en) *	2015-12-18	2020-10-06	Raytheon Technologies Corporation	Gas turbine engine with one piece acoustic treatment
US9741331B1 (en)	2016-06-01	2017-08-22	The Boeing Company	Sound-attenuating composite structure
US10823061B2 (en) *	2016-07-15	2020-11-03	General Electric Company	Engine air inlet having a double-panel heated wall
RU180269U1 (ru) *	2017-08-29	2018-06-07	Акционерное общество "Объединенная двигателестроительная корпорация" (АО "ОДК")	Воздухозаборный канал газотурбинного двигателя
US11125157B2 (en) *	2017-09-22	2021-09-21	The Boeing Company	Advanced inlet design
FR3075761A1 (fr) *	2017-12-21	2019-06-28	Airbus Operations	Partie anterieure de nacelle d'un ensemble propulsif comportant un cadre de rigidification incline
FR3087420B1 (fr) *	2018-10-19	2021-03-12	Airbus Operations Sas	Nacelle de moteur d’aeronef comprenant un systeme de protection contre le givre.
DE102019111135A1 (de)	2019-04-30	2020-11-05	Airbus Operations Gmbh	Vorderkantenvorrichtung für ein Flugzeug
FR3099913A1 (fr) *	2019-08-13	2021-02-19	Airbus Operations	Partie antérieure de nacelle d’un ensemble propulsif d’aéronef dont le cadre avant est lié à une paroi extérieure sans la traverser
FR3099912B1 (fr)	2019-08-18	2021-08-13	Safran Nacelles	Entrée d’air d’une nacelle d’une turbomachine d’aéronef
CN110979693A (zh) *	2019-11-18	2020-04-10	西安京东天鸿科技有限公司	防除冰系统、无人机及控制方法
US11560843B2 (en)	2020-02-25	2023-01-24	General Electric Company	Frame for a heat engine
US11255264B2 (en)	2020-02-25	2022-02-22	General Electric Company	Frame for a heat engine
US11326519B2 (en)	2020-02-25	2022-05-10	General Electric Company	Frame for a heat engine
BR102022003769A2 (pt)	2021-05-04	2022-11-16	The Boeing Company	Estrutura de entrada de nacele de um conjunto de motor
US11970978B2 (en) *	2021-06-25	2024-04-30	Rohr, Inc.	Acoustic panel and method of forming same

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US4924228A (en) *	1963-07-17	1990-05-08	Boeing Company	Aircraft construction
US3481427A (en) *	1968-11-29	1969-12-02	Mc Donnell Douglas Corp	Acoustical panel structure
US4240250A (en) *	1977-12-27	1980-12-23	The Boeing Company	Noise reducing air inlet for gas turbine engines
US4235303A (en) *	1978-11-20	1980-11-25	The Boeing Company	Combination bulk absorber-honeycomb acoustic panels
GB2112339B (en) *	1981-11-13	1985-07-03	T K S	Porous panel
US4759513A (en) *	1986-09-26	1988-07-26	Quiet Nacelle Corporation	Noise reduction nacelle
USH648H (en) *	1988-08-12	1989-07-04	The United States Of America As Represented By The Secretary Of The Air Force	Air passage device
GB2314887B (en) *	1996-07-02	2000-02-09	Rolls Royce Plc	Ice protection for porous structure
US7318499B2 (en) *	2004-02-20	2008-01-15	Honeywell International, Inc.	Noise suppression structure and method of making the same
FR2868124B1 (fr) *	2004-03-29	2006-06-23	Airbus France Sas	Structure d'entree d'air pour moteur d'aeronef
FR2869360B1 (fr)	2004-04-27	2006-07-14	Airbus France Sas	Ensemble reducteur de bruit pour turboreacteur d'aeronef
FR2887294B1 (fr) *	2005-06-21	2007-08-10	Airbus France Sas	Systeme pour le degivrage du bord d'attaque d'un capot d'entree d'air pour turbomoteur
FR2906568B1 (fr) *	2006-10-02	2012-01-06	Aircelle Sa	Structure d'entree d'air deposable pour nacelle de turboreacteur.

2009
- 2009-07-28 EP EP20090784308 patent/EP2321510B1/fr not_active Not-in-force
- 2009-07-28 CA CA 2732351 patent/CA2732351A1/fr not_active Abandoned
- 2009-07-28 US US13/056,727 patent/US8840059B2/en not_active Expired - Fee Related
- 2009-07-28 BR BRPI0914134A patent/BRPI0914134A2/pt not_active IP Right Cessation
- 2009-07-28 CN CN200980127934.9A patent/CN102099556B/zh not_active Expired - Fee Related
- 2009-07-28 ES ES09784308T patent/ES2425078T3/es active Active
- 2009-07-28 WO PCT/FR2009/000934 patent/WO2010012899A2/fr not_active Ceased

Also Published As

Publication number	Publication date
CA2732351A1 (fr)	2010-02-04
CN102099556A (zh)	2011-06-15
WO2010012899A3 (fr)	2010-04-15
EP2321510A2 (fr)	2011-05-18
CN102099556B (zh)	2014-03-12
US20110131945A1 (en)	2011-06-09
WO2010012899A2 (fr)	2010-02-04
ES2425078T3 (es)	2013-10-11
US8840059B2 (en)	2014-09-23
EP2321510B1 (fr)	2013-07-03

Publication	Publication Date	Title
BRPI0914134A2 (pt)	2015-10-20	conjunto de componentes e estrutura de entrada de ar
EP2180160A4 (en)	2012-05-23	TURBOCHARGER
EP2351920A4 (en)	2012-03-14	TURBOCHARGER
EP2226484A4 (en)	2011-08-03	TURBOCHARGER
EP2261482A4 (en)	2013-04-03	TURBOCHARGER
EP2314940A4 (en)	2015-12-02	AIR CONDITIONER
HRP20170698T1 (hr)	2017-09-22	Lizosomski usmjereni peptidi i njihove uporabe
EP2341296A4 (en)	2014-10-08	Air conditioner
EP2330359A4 (en)	2012-10-03	AIR CONDITIONING DEVICE
BRPI0907231A2 (pt)	2019-09-24	pirrolpirimidinas e pirrolpiridinas
BRPI0907841A2 (pt)	2015-07-21	Fabricação e montagem de ventoinha
BRPI0922878A2 (pt)	2018-05-29	ventilador
EP2320151A4 (en)	2011-09-07	AIR CONDITIONING DEVICE
EP2244354A4 (en)	2016-07-27	Compressor
EP2282144A4 (en)	2014-07-02	AIR CONDITIONING
EP2264379A4 (en)	2014-11-05	AIR CONDITIONING
EP2306101A4 (en)	2016-05-25	Air conditioner
EP2284456A4 (en)	2015-03-04	AIR CONDITIONING
DK2333440T3 (da)	2017-11-20	Klimaanlæg
EP2233847A4 (en)	2014-01-15	AIR CONDITIONING
BRPI0919255A2 (pt)	2015-12-15	aparelho de limpeza de ar
EP2279337A4 (en)	2011-04-20	COMPRESSOR
BRPI0914718A2 (pt)	2015-10-20	compressor axial-centrífugo
EP2312228A4 (en)	2016-12-14	Air conditioner
DK2325662T3 (da)	2019-08-19	Multi-indlæsnings- og multi-udlæsningsanalysator

Legal Events

Date	Code	Title	Description
2016-09-20	B08F	Application fees: dismissal - article 86 of industrial property law	Free format text: REFERENTE A 7A ANUIDADE.
2017-01-10	B08K	Lapse as no evidence of payment of the annual fee has been furnished to inpi (acc. art. 87)	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.