BR112017005234A2 - sistema para calcular desempenho de aeronave e método para realizar o mesmo - Google Patents
sistema para calcular desempenho de aeronave e método para realizar o mesmoInfo
- Publication number
- BR112017005234A2 BR112017005234A2 BR112017005234A BR112017005234A BR112017005234A2 BR 112017005234 A2 BR112017005234 A2 BR 112017005234A2 BR 112017005234 A BR112017005234 A BR 112017005234A BR 112017005234 A BR112017005234 A BR 112017005234A BR 112017005234 A2 BR112017005234 A2 BR 112017005234A2
- Authority
- BR
- Brazil
- Prior art keywords
- same
- aircraft performance
- performance
- terminal
- files
- Prior art date
Links
Classifications
-
- 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
- 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
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/60—Testing or inspecting aircraft components or systems
Abstract
a presente invenção se refere a um sistema para determinar desempenho de aeronave para pelo menos uma fase de voo. o sistema (10) compreende um primeiro terminal (11) que compreende meios para se conectar a um primeiro, segundo e terceiro repositório, respectivamente, que compreende pelo menos um primeiro conjunto de arquivos de dados (22) de um segundo conjunto de scripts executáveis (23) e um terceiro conjunto de arquivos de configuração (17). pelo menos o terceiro conjunto de arquivos de configuração está disposto para ser acessado por meio de uma segunda interface de usuário de um segundo terminal (18). o sistema compreende adicionalmente um módulo de chamada (12) disposto para selecionar, com base nos parâmetros de entrada recebidos e no arquivo de configuração selecionado, pelo menos um arquivo de script executável (23) para processamento dos arquivos de dados associados (22) de modo a determinar por meio de um mecanismo de cálculo (26) o desempenho da aeronave para a pelo menos uma fase de voo.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
EP14185012.3 | 2014-09-16 | ||
EP14185012.3A EP2998817B1 (en) | 2014-09-16 | 2014-09-16 | System for calculating aircraft performance and method for performing the same |
PCT/EP2015/071247 WO2016042036A1 (en) | 2014-09-16 | 2015-09-16 | System for calculating aircraft performance and method for performing the same |
Publications (2)
Publication Number | Publication Date |
---|---|
BR112017005234A2 true BR112017005234A2 (pt) | 2018-06-19 |
BR112017005234B1 BR112017005234B1 (pt) | 2022-05-24 |
Family
ID=51570294
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112017005234-2A BR112017005234B1 (pt) | 2014-09-16 | 2015-09-16 | Sistema para calcular desempenho de aeronave e método para realizar o mesmo |
Country Status (8)
Country | Link |
---|---|
US (1) | US10274339B2 (pt) |
EP (1) | EP2998817B1 (pt) |
CN (1) | CN107077141A (pt) |
BE (1) | BE1022548B1 (pt) |
BR (1) | BR112017005234B1 (pt) |
CA (1) | CA2961117A1 (pt) |
HK (1) | HK1221524A1 (pt) |
WO (1) | WO2016042036A1 (pt) |
Families Citing this family (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10936958B2 (en) * | 2017-02-28 | 2021-03-02 | International Business Machines Corporation | Sequencing of input prompts for data structure completion |
US10616241B2 (en) * | 2017-06-05 | 2020-04-07 | Honeywell International Inc. | Systems and methods for performing external data validation for aircraft onboard systems |
BR112020004572A2 (pt) * | 2017-09-06 | 2020-09-08 | Aviovision | sistema e método para gerenciar as operações de um veículo de transporte comercial |
US10946977B2 (en) | 2017-11-20 | 2021-03-16 | Honeywell International Inc. | Method and system for integrating offboard generated parameters into a flight management system |
US10748359B2 (en) * | 2018-01-24 | 2020-08-18 | Honeywell International Inc. | Method and system for data reporting using customized triggers |
US10991255B2 (en) | 2018-04-05 | 2021-04-27 | Ge Aviation Systems Llc | Providing an open interface to a flight management system |
US10971155B2 (en) * | 2018-04-12 | 2021-04-06 | Honeywell International Inc. | Aircraft systems and methods for monitoring onboard communications |
US10960985B2 (en) * | 2018-10-31 | 2021-03-30 | The Boeing Company | Integrating an application running on a portable electronic device into a flight deck display of an aircraft |
GB201900477D0 (en) * | 2019-01-14 | 2019-02-27 | Rolls Royce Plc | Optimisation method |
CN109918709A (zh) * | 2019-01-21 | 2019-06-21 | 中国南方航空股份有限公司 | 一种起飞性能分析方法、电子设备及存储介质 |
CN110083358B (zh) * | 2019-04-29 | 2023-06-20 | 南京国电南自轨道交通工程有限公司 | 基于脚本语言的修改牵引自投装置开关编号的工具 |
CN111309723B (zh) * | 2019-10-18 | 2023-11-21 | 中国航空工业集团公司西安飞行自动控制研究所 | 一种基于固定翼飞机的机载性能数据库建立方法 |
US11427353B2 (en) * | 2019-12-13 | 2022-08-30 | Pratt & Whitney Canada Corp. | System and method for testing engine performance in-flight |
US11386069B2 (en) | 2019-12-17 | 2022-07-12 | Honeywell Interational Inc. | System and method for offboard validation of variable parameters |
CN111846284B (zh) * | 2020-07-30 | 2023-01-03 | 贵州大鸟创新科技有限公司 | 无人机性能测试系统及方法 |
US20220106059A1 (en) * | 2020-10-07 | 2022-04-07 | General Electric Company | Flexible engine monitoring |
CN113256843B (zh) * | 2021-05-20 | 2022-05-31 | 中国商用飞机有限责任公司 | 集成式飞行记录设备及方法 |
CN114841676A (zh) * | 2022-05-25 | 2022-08-02 | 中航材导航技术(北京)有限公司 | 一种基于scap协议批量计算多机型性能图表数据的方法 |
Family Cites Families (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE19640606C1 (de) * | 1996-10-01 | 1997-09-11 | Nord Micro Elektronik Feinmech | Meßeinrichtung zur Erfassung von Stau- und Statikdrücken bei einem Fluggerät |
AUPQ710600A0 (en) * | 2000-04-20 | 2000-05-18 | Commonwealth Of Australia, The | Simulation and modelling method and apparatus |
US7529603B2 (en) * | 2006-03-20 | 2009-05-05 | The Boeing Company | Integrated performance application |
CA2782414C (en) * | 2009-12-14 | 2021-08-03 | Ab Initio Technology Llc | Specifying user interface elements |
CN101794226B (zh) * | 2010-03-08 | 2012-11-07 | 山东大学 | 一种适应多业务抽象层次的服务化软件构造方法和系统 |
US20120224058A1 (en) * | 2011-03-02 | 2012-09-06 | Rosemount Aerospace Inc. | Airplane cockpit video system |
US8630752B2 (en) * | 2011-09-08 | 2014-01-14 | Honeywell International Inc. | System and method of displaying airspeed information for an aircraft |
US20130204544A1 (en) * | 2012-02-03 | 2013-08-08 | Gulfstream Aerospace Corporation | Methods and systems for determining airspeed of an aircraft |
US8825233B2 (en) * | 2012-05-31 | 2014-09-02 | Sikorsky Aircraft Corporation | Synthetic estimation of rotorcraft airspeed |
FR3000195B1 (fr) * | 2012-12-21 | 2019-08-09 | Airbus Operations | Architecture hybride pour systeme aeronautique |
FR3002320B1 (fr) * | 2013-02-20 | 2016-05-20 | Airbus Operations Sas | Sonde de mesure angulaire a bord d'un aeronef et aeronef mettant en oeuvre au moins une telle sonde |
CN103926928B (zh) * | 2014-05-04 | 2016-08-17 | 威海新北洋正棋机器人股份有限公司 | 一种模块动态调度的机器人控制器 |
FR3035209B1 (fr) * | 2015-04-20 | 2018-10-05 | Thales | Sonde multifonctions de references primaires pour aeronef, systeme de mesure, aeronef et procede d'obtention de grandeurs physiques associes |
US20160376003A1 (en) * | 2015-06-26 | 2016-12-29 | Yuri Feldman | Aircraft |
US9939459B2 (en) * | 2016-04-19 | 2018-04-10 | The Boeing Company | System and method for performing a test on a pitot probe heating element |
-
2014
- 2014-09-16 EP EP14185012.3A patent/EP2998817B1/en active Active
-
2015
- 2015-08-05 BE BE2015/5498A patent/BE1022548B1/nl active
- 2015-09-16 WO PCT/EP2015/071247 patent/WO2016042036A1/en active Application Filing
- 2015-09-16 CN CN201580053523.5A patent/CN107077141A/zh active Pending
- 2015-09-16 US US15/511,105 patent/US10274339B2/en active Active
- 2015-09-16 BR BR112017005234-2A patent/BR112017005234B1/pt active IP Right Grant
- 2015-09-16 CA CA2961117A patent/CA2961117A1/en not_active Abandoned
-
2016
- 2016-08-15 HK HK16109727.3A patent/HK1221524A1/zh unknown
Also Published As
Publication number | Publication date |
---|---|
EP2998817B1 (en) | 2017-06-07 |
CA2961117A1 (en) | 2016-03-24 |
US20170241798A1 (en) | 2017-08-24 |
BR112017005234B1 (pt) | 2022-05-24 |
BE1022548B1 (nl) | 2016-05-26 |
EP2998817A1 (en) | 2016-03-23 |
CN107077141A (zh) | 2017-08-18 |
BE1022548A1 (nl) | 2016-05-26 |
HK1221524A1 (zh) | 2017-06-02 |
US10274339B2 (en) | 2019-04-30 |
WO2016042036A1 (en) | 2016-03-24 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B25G | Requested change of headquarter approved |
Owner name: AVIOVISION (BE) |
|
B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B09A | Decision: intention to grant [chapter 9.1 patent gazette] | ||
B16A | Patent or certificate of addition of invention granted [chapter 16.1 patent gazette] |
Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 16/09/2015, OBSERVADAS AS CONDICOES LEGAIS |