BRPI0513760A - aeronave com asas cuja força de ascensão máxima pode ser alterada por componentes de asa controláveis - Google Patents
aeronave com asas cuja força de ascensão máxima pode ser alterada por componentes de asa controláveisInfo
- Publication number
- BRPI0513760A BRPI0513760A BRPI0513760-8A BRPI0513760A BRPI0513760A BR PI0513760 A BRPI0513760 A BR PI0513760A BR PI0513760 A BRPI0513760 A BR PI0513760A BR PI0513760 A BRPI0513760 A BR PI0513760A
- Authority
- BR
- Brazil
- Prior art keywords
- lift force
- wing components
- altered
- whose maximum
- aircraft whose
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
- G05D1/0055—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements
- G05D1/0066—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot with safety arrangements for limitation of acceleration or stress
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/16—Initiating means actuated automatically, e.g. responsive to gust detectors
-
- 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
- Y02T50/40—Weight reduction
Abstract
AERONAVE COM ASAS CUJA FORçA DE ASCENSãO MáXIMA PODE SER ALTERADA POR COMPONENTES DE ASA CONTROLáVEIS A presente invenção refere-se a uma aeronave com asas cuja força de ascensão máxima pode ser alterada por componentes de asa controláveis. Por meio de um dispositivo regulador (20), que depende de parâmetros de estado de vóo e da carga realmente medida sobre as asas (10), componentes de asa (11, 12) são atuados de modo que a força de ascensão aerodinâmica possível máxima não ultrapasse um valor de limite superior desejado.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE102004045732A DE102004045732A1 (de) | 2004-09-21 | 2004-09-21 | Flugzeug mit Flügeln, deren maximaler Auftrieb durch steuerbare Flügelkomponenten veränderbar ist |
US63130204P | 2004-11-29 | 2004-11-29 | |
PCT/EP2005/010228 WO2006032486A1 (en) | 2004-09-21 | 2005-09-21 | Aircraft with wings whose maximum lift can be altered by controllable wing components |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0513760A true BRPI0513760A (pt) | 2008-05-20 |
Family
ID=36011539
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0513760-8A BRPI0513760A (pt) | 2004-09-21 | 2005-09-21 | aeronave com asas cuja força de ascensão máxima pode ser alterada por componentes de asa controláveis |
Country Status (9)
Country | Link |
---|---|
US (2) | US20080116320A1 (pt) |
EP (1) | EP1791755A1 (pt) |
JP (1) | JP2008513275A (pt) |
CN (1) | CN1989041A (pt) |
BR (1) | BRPI0513760A (pt) |
CA (1) | CA2573606A1 (pt) |
DE (1) | DE102004045732A1 (pt) |
RU (1) | RU2391253C2 (pt) |
WO (1) | WO2006032486A1 (pt) |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ATE530966T1 (de) | 2007-02-16 | 2011-11-15 | Rolls Royce Plc | Auftriebsmessung |
GB0703128D0 (en) | 2007-02-16 | 2007-03-28 | Rolls Royce Plc | Stall detection |
US7992825B2 (en) * | 2008-07-23 | 2011-08-09 | Airbus Espana, S.L. | Control surface of aircraft |
DE102010026162A1 (de) | 2010-07-06 | 2012-01-12 | Airbus Operations Gmbh | Flugzeug mit Tragflügeln und einem System zur Minimierung des Einflusses von instationären Anströmzuständen |
ES2543633T3 (es) * | 2011-07-28 | 2015-08-20 | Airbus Defence and Space GmbH | Método y aparato para minimizar las cargas estructurales dinámicas de un avión |
EP2874873B1 (en) * | 2012-07-20 | 2016-12-14 | Icon Aircraft, Inc. | Spin resistant aircraft configuration |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1862421A (en) * | 1931-07-18 | 1932-06-07 | John F O'malley | Stabilizing device for aircraft |
US2263992A (en) * | 1939-03-16 | 1941-11-25 | Zap Dev Corp | Control system for airplanes |
US4117995A (en) * | 1977-02-28 | 1978-10-03 | Runge Thomas M | Aircraft wing lift augmentation device |
US5082207A (en) * | 1985-02-04 | 1992-01-21 | Rockwell International Corporation | Active flexible wing aircraft control system |
US4796192A (en) * | 1985-11-04 | 1989-01-03 | The Boeing Company | Maneuver load alleviation system |
FR2604001B1 (fr) * | 1986-09-15 | 1988-12-09 | Aerospatiale | Systeme de commande de vol electrique avec protection en incidence pour aeronef |
US5056741A (en) * | 1989-09-29 | 1991-10-15 | The Boeing Company | Apparatus and method for aircraft wing stall control |
FR2656585B1 (fr) * | 1989-12-28 | 1995-01-13 | Aerospatiale | Systeme pour diminuer les efforts appliques a la voilure et notamment a l'emplanture des ailes d'un aeronef en vol. |
US5875998A (en) * | 1996-02-05 | 1999-03-02 | Daimler-Benz Aerospace Airbus Gmbh | Method and apparatus for optimizing the aerodynamic effect of an airfoil |
DE10045732C2 (de) | 2000-09-15 | 2003-08-21 | Norbert Hagen | Vorrichtung zur maschinellen kontinuierlichen Ernte von Früchten, vorzugsweise von Tafel-Kernobst |
GB0115130D0 (en) * | 2001-06-21 | 2001-08-15 | Bae Systems Plc | A winglet |
US6766981B2 (en) * | 2002-10-25 | 2004-07-27 | Northrop Grumman Corporation | Control system for alleviating a gust load on an aircraft wing |
-
2004
- 2004-09-21 DE DE102004045732A patent/DE102004045732A1/de not_active Withdrawn
-
2005
- 2005-09-21 EP EP05796376A patent/EP1791755A1/en not_active Withdrawn
- 2005-09-21 CN CNA200580024391XA patent/CN1989041A/zh active Pending
- 2005-09-21 BR BRPI0513760-8A patent/BRPI0513760A/pt not_active IP Right Cessation
- 2005-09-21 US US11/663,055 patent/US20080116320A1/en not_active Abandoned
- 2005-09-21 JP JP2007531715A patent/JP2008513275A/ja active Pending
- 2005-09-21 RU RU2007111373/11A patent/RU2391253C2/ru not_active IP Right Cessation
- 2005-09-21 WO PCT/EP2005/010228 patent/WO2006032486A1/en active Application Filing
- 2005-09-21 CA CA002573606A patent/CA2573606A1/en not_active Abandoned
-
2009
- 2009-12-17 US US12/640,559 patent/US20100090068A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
CN1989041A (zh) | 2007-06-27 |
WO2006032486A1 (en) | 2006-03-30 |
CA2573606A1 (en) | 2006-03-30 |
WO2006032486B1 (en) | 2006-06-01 |
EP1791755A1 (en) | 2007-06-06 |
RU2391253C2 (ru) | 2010-06-10 |
RU2007111373A (ru) | 2008-11-10 |
US20100090068A1 (en) | 2010-04-15 |
JP2008513275A (ja) | 2008-05-01 |
US20080116320A1 (en) | 2008-05-22 |
DE102004045732A1 (de) | 2006-03-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25D | Requested change of name of applicant approved |
Owner name: AIRBUS OPERATIONS GMBH (DE) Free format text: NOME ALTERADO DE: AIRBUS DEUTSCHLAND GMBH |
|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 10A ANUIDADE. |
|
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 2324 DE 21-07-2015 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. |