BR112012020284A2 - dispositivo de avaliação de coeficiente aerodinâmico e dispositivo de deteção de falha/danificação de superfície de controle - Google Patents
dispositivo de avaliação de coeficiente aerodinâmico e dispositivo de deteção de falha/danificação de superfície de controleInfo
- Publication number
- BR112012020284A2 BR112012020284A2 BR112012020284A BR112012020284A BR112012020284A2 BR 112012020284 A2 BR112012020284 A2 BR 112012020284A2 BR 112012020284 A BR112012020284 A BR 112012020284A BR 112012020284 A BR112012020284 A BR 112012020284A BR 112012020284 A2 BR112012020284 A2 BR 112012020284A2
- Authority
- BR
- Brazil
- Prior art keywords
- control surface
- aerodynamic coefficient
- evaluation
- aerodynamic
- coefficient
- Prior art date
Links
- 238000001514 detection method Methods 0.000 title abstract 2
- 238000011156 evaluation Methods 0.000 abstract 5
Classifications
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/06—Measuring arrangements specially adapted for aerodynamic testing
-
- 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M9/00—Aerodynamic testing; Arrangements in or on wind tunnels
- G01M9/08—Aerodynamic models
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D2045/0085—Devices for aircraft health monitoring, e.g. monitoring flutter or vibration
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
- G01C23/005—Flight directors
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
- G05D1/0077—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements using redundant signals or controls
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0004—Transmission of traffic-related information to or from an aircraft
- G08G5/0013—Transmission of traffic-related information to or from an aircraft with a ground station
-
- G—PHYSICS
- G08—SIGNALLING
- G08G—TRAFFIC CONTROL SYSTEMS
- G08G5/00—Traffic control systems for aircraft, e.g. air-traffic control [ATC]
- G08G5/0017—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information
- G08G5/0021—Arrangements for implementing traffic-related aircraft activities, e.g. arrangements for generating, displaying, acquiring or managing traffic information located in the aircraft
Landscapes
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- Fluid Mechanics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
- Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Traffic Control Systems (AREA)
Abstract
dispositivo de avaliação de coeficiente aerodinâmico e dispositivo de deteção de falha/danificação de superfície de controle. pode-se realizar a computação de uma avaliação de coeficiente aerodinâmico altamente confiável, sendo a computação desta avaliação de coeficiente aerodinâmico capaz de detectar com precisão a falha/danificação da superfície de controle, enquanto que reduzindo o desconforto para os passageiros. o mecanismo de geração de sinal de comando de ângulo de deflexão (5) gera um sinal de comando de ângulo de deflexão voltado para a avaliação de um coeficiente aerodinâmico indicando as características aerodinâmicas de uma estrutura de aparelho. mecanismo de avaliação de condição cinética (6) obtendo uma quantidade de condição cinética da estrutura do aparelho obtida a partir da movimentação resultante de uma superfície de controle provida em uma estrutura de aparelho com base no sinal de comando de ãngulo de deflexão. mecanismo de cálculo de valor candidato (7) calculando os valores candidatos destinados a avaliação do coeficiente aerodinâmico para a quantidade de condição cinética fazendo uso de duas ou mais avaliações. mecanismo de determinação da avaliação de coeficiente aerodinâmico (8) determinado uma avaliação de coeficiente aerodinâmico com base nos valores candidatos.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP2010062708A JP5550398B2 (ja) | 2010-03-18 | 2010-03-18 | 舵面故障・損傷検出装置 |
PCT/JP2011/056191 WO2011115164A1 (ja) | 2010-03-18 | 2011-03-16 | 空力係数推定装置及びこれを用いた舵面故障・損傷検出装置 |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112012020284A2 true BR112012020284A2 (pt) | 2016-05-03 |
Family
ID=44649247
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112012020284A BR112012020284A2 (pt) | 2010-03-18 | 2011-03-16 | dispositivo de avaliação de coeficiente aerodinâmico e dispositivo de deteção de falha/danificação de superfície de controle |
Country Status (8)
Country | Link |
---|---|
US (1) | US8954208B2 (pt) |
EP (1) | EP2548799B1 (pt) |
JP (1) | JP5550398B2 (pt) |
CN (1) | CN102753435B (pt) |
BR (1) | BR112012020284A2 (pt) |
CA (1) | CA2788536C (pt) |
RU (1) | RU2515947C1 (pt) |
WO (1) | WO2011115164A1 (pt) |
Families Citing this family (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2966951A1 (fr) * | 2010-11-03 | 2012-05-04 | Airbus Operations Sas | Procede de simulation pour determiner des coefficients aerodynamiques d'un aeronef |
FR2978858B1 (fr) * | 2011-08-01 | 2013-08-30 | Airbus Operations Sas | Procede et systeme pour la determination de parametres de vol d'un aeronef |
JP5811711B2 (ja) | 2011-09-07 | 2015-11-11 | 株式会社リコー | 機器連携システム、機能提供方法 |
PL2700814T3 (pl) * | 2012-08-23 | 2015-07-31 | Ampyx Power B V | Szybowiec do wytwarzania energii wiatrowej generowanej przez elektrownie latające |
FR3010448B1 (fr) * | 2013-09-06 | 2015-08-21 | Snecma | Procede de surveillance d’une degradation d’un dispositif embarque d’un aeronef avec determination automatique d’un seuil de decision |
US9359065B2 (en) | 2013-09-24 | 2016-06-07 | The Boeing Company | System and method for optimizing performance of an aircraft |
US9327827B2 (en) | 2013-09-24 | 2016-05-03 | The Boeing Company | Leading and trailing edge device deflections during descent of an aircraft |
US9180962B2 (en) | 2013-09-24 | 2015-11-10 | The Boeing Company | Leading edge variable camber system and method |
US9254909B2 (en) | 2013-09-24 | 2016-02-09 | The Boeing Company | Optimized flap positioning for go-around operations |
US9656741B2 (en) * | 2013-09-24 | 2017-05-23 | The Boeing Company | Control interface for leading and trailing edge devices |
US9284043B2 (en) * | 2013-11-21 | 2016-03-15 | Aai Corporation | Evaluating aileron deflection while an unmanned aerial vehicle is in flight |
US10401875B2 (en) * | 2014-07-31 | 2019-09-03 | The Boeing Company | Electronic stopper in actuator control |
US9418561B2 (en) * | 2014-12-02 | 2016-08-16 | Honeywell International Inc. | System and method for displaying predictive conformal configuration cues for executing a landing |
US10043402B1 (en) * | 2015-09-04 | 2018-08-07 | Rockwell Collins, Inc. | Flight path cross check |
US9701418B2 (en) | 2015-10-06 | 2017-07-11 | Honeywell International Inc. | Pilot fatigue detection system and method from aircraft control device movement |
CN109562843B (zh) | 2016-09-26 | 2021-01-01 | 株式会社斯巴鲁 | 损伤检测***和损伤检测方法 |
FR3057954B1 (fr) * | 2016-10-24 | 2021-04-02 | Safran Landing Systems | Procede d'estimation de l'endommagement subi par des parties de trains d'atterrissage d'aeronef |
CN107483230B (zh) * | 2017-07-26 | 2020-11-03 | 中国航空工业集团公司西安飞机设计研究所 | 一种飞机轮载信号地面检测方法 |
CA3002186A1 (en) * | 2018-04-19 | 2019-10-19 | Curran Crawford | Aerodynamic drag monitoring system and method |
CN109387350B (zh) * | 2018-12-06 | 2023-08-25 | 中国航空工业集团公司沈阳空气动力研究所 | 一种内式同轴波纹管天平*** |
GB2593196A (en) * | 2020-03-19 | 2021-09-22 | Airbus Operations Ltd | Aircraft fuel system monitoring |
CN112478197A (zh) * | 2020-12-07 | 2021-03-12 | 中国民用航空上海航空器适航审定中心 | 飞机操纵面间隙动态测量方法 |
US11905840B2 (en) * | 2021-02-01 | 2024-02-20 | Pratt & Whitney Canada Corp. | System and method for detecting failure of a propeller feedback device |
CN114608794B (zh) * | 2022-05-11 | 2022-07-19 | 中国航空工业集团公司哈尔滨空气动力研究所 | 一种模型风洞虚拟飞行试验气动力系数测量方法 |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3691356A (en) * | 1970-12-10 | 1972-09-12 | Sperry Rand Corp | Speed command and throttle control system for aircraft |
JPH06336199A (ja) * | 1993-05-28 | 1994-12-06 | Mitsubishi Heavy Ind Ltd | 航空機用部材損傷検出装置 |
FR2739683B1 (fr) * | 1995-10-05 | 1997-12-05 | France Etat | Projectile d'exercice sous-calibre a energie cinetique du type fleche |
JPH10167194A (ja) * | 1996-12-12 | 1998-06-23 | Mitsubishi Heavy Ind Ltd | 操縦舵面損傷検出機能を有する飛行制御装置 |
US6246929B1 (en) * | 1999-06-16 | 2001-06-12 | Lockheed Martin Corporation | Enhanced stall and recovery control system |
JP2003175896A (ja) * | 2001-12-10 | 2003-06-24 | Mitsubishi Heavy Ind Ltd | 舵面の故障・損傷検出装置 |
JP3637326B2 (ja) * | 2002-04-03 | 2005-04-13 | 三菱重工業株式会社 | 制御システム、航空機・宇宙機の飛行制御システム、車両の運動制御システム |
JP5128766B2 (ja) * | 2005-11-08 | 2013-01-23 | 東洋電装株式会社 | 舵角センサ |
DE102005058192A1 (de) * | 2005-12-06 | 2007-06-28 | Airbus Deutschland Gmbh | Vorrichtung zur Fehlererkennung von verstellbaren Klappen |
FR2908107B1 (fr) * | 2006-11-06 | 2008-12-19 | Airbus France Sa | Procede et dispositif pour estimer les forces s'exercant sur une surface de controle d'un aeronef. |
FR2916868B1 (fr) * | 2007-06-01 | 2009-07-24 | Airbus France Sas | Procede et dispositif de determination de la marge de stabilite dynamique d'un avion. |
US8380473B2 (en) * | 2009-06-13 | 2013-02-19 | Eric T. Falangas | Method of modeling dynamic characteristics of a flight vehicle |
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2010
- 2010-03-18 JP JP2010062708A patent/JP5550398B2/ja active Active
-
2011
- 2011-03-16 US US13/575,365 patent/US8954208B2/en active Active
- 2011-03-16 EP EP11756348.6A patent/EP2548799B1/en active Active
- 2011-03-16 CA CA2788536A patent/CA2788536C/en not_active Expired - Fee Related
- 2011-03-16 WO PCT/JP2011/056191 patent/WO2011115164A1/ja active Application Filing
- 2011-03-16 CN CN201180008999.9A patent/CN102753435B/zh not_active Expired - Fee Related
- 2011-03-16 RU RU2012131672/11A patent/RU2515947C1/ru active
- 2011-03-16 BR BR112012020284A patent/BR112012020284A2/pt not_active Application Discontinuation
Also Published As
Publication number | Publication date |
---|---|
EP2548799A1 (en) | 2013-01-23 |
US8954208B2 (en) | 2015-02-10 |
RU2012131672A (ru) | 2014-04-27 |
US20120296500A1 (en) | 2012-11-22 |
EP2548799B1 (en) | 2019-08-14 |
CN102753435A (zh) | 2012-10-24 |
JP2011194974A (ja) | 2011-10-06 |
EP2548799A4 (en) | 2017-10-11 |
CA2788536A1 (en) | 2011-09-22 |
RU2515947C1 (ru) | 2014-05-20 |
JP5550398B2 (ja) | 2014-07-16 |
WO2011115164A1 (ja) | 2011-09-22 |
CA2788536C (en) | 2016-06-21 |
CN102753435B (zh) | 2016-05-04 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B06F | Objections, documents and/or translations needed after an examination request according [chapter 6.6 patent gazette] | ||
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B06A | Patent application procedure suspended [chapter 6.1 patent gazette] | ||
B11B | Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements |