BRPI0518456A2 - sistema de gerenciamento de gelo para aeronave tiltrotor - Google Patents
sistema de gerenciamento de gelo para aeronave tiltrotorInfo
- Publication number
- BRPI0518456A2 BRPI0518456A2 BRPI0518456-8A BRPI0518456A BRPI0518456A2 BR PI0518456 A2 BRPI0518456 A2 BR PI0518456A2 BR PI0518456 A BRPI0518456 A BR PI0518456A BR PI0518456 A2 BRPI0518456 A2 BR PI0518456A2
- Authority
- BR
- Brazil
- Prior art keywords
- rotor
- management system
- aircraft
- ice management
- heater
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
- B64C29/0033—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers the propellers being tiltable relative to the fuselage
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D15/00—De-icing or preventing icing on exterior surfaces of aircraft
- B64D15/12—De-icing or preventing icing on exterior surfaces of aircraft by electric heating
Abstract
SISTEMA DE GERENCIAMENTO DE GELO PARA AERONAVE TILTROTOR. Trata-se de um sistema de gerenciamento de gelo que é configurado para uma aeronave que possui pelo menos um rotor, sendo que cada rotor possui uma pluralidade de hélices. O sistema possui um fornecedor de energia elétrica adaptado para ser transportado pela aeronave à distância do rotor, e pelo menos um aquecedor é transportado pelo rotor para aquecer pelo menos uma parte do rotor. Um relé de controle em estado sólido é transportado pelo rotor e acoplado, de Ibrma condutiva, entre o fornecedor de energia e cada aquecedor para controlar seletivamente o fluxo de energia elétrica do fornecedor de energia para cada aquecedor. Ademais, o sistema pode incorporar um relé de alimentação em estado sólido é transportado pela aeronave à distância do e acoplado, de forma condutiva, entre o fornecedor de energia e o relé de controle para controlar seletivamente o fluxo de energia elétrica para o relé de controle.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/US2005/005854 WO2006093480A1 (en) | 2005-02-24 | 2005-02-24 | Ice management system for tiltrotor aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
BRPI0518456A2 true BRPI0518456A2 (pt) | 2008-11-18 |
Family
ID=36941455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BRPI0518456-8A BRPI0518456A2 (pt) | 2005-02-24 | 2005-02-24 | sistema de gerenciamento de gelo para aeronave tiltrotor |
Country Status (7)
Country | Link |
---|---|
US (1) | US7604202B2 (pt) |
EP (1) | EP1851110B1 (pt) |
CN (1) | CN101068715B (pt) |
BR (1) | BRPI0518456A2 (pt) |
CA (2) | CA2704249C (pt) |
DE (1) | DE05723643T1 (pt) |
WO (1) | WO2006093480A1 (pt) |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8550402B2 (en) * | 2005-04-06 | 2013-10-08 | Sikorsky Aircraft Corporation | Dual-channel deicing system for a rotary wing aircraft |
DE05750600T1 (de) * | 2005-05-16 | 2008-08-21 | Bell Helicopter Textron, Inc., Fort Worth | Eis-verwaltungssystem für neigungsrotor-flugzeuge |
US8251313B2 (en) * | 2005-10-21 | 2012-08-28 | Honda Patents & Technologies North America, Llc | Ice protection system for aircraft |
GB2450503A (en) * | 2007-06-26 | 2008-12-31 | Ultra Electronics Ltd | Ice protection system with plural heating elements |
US8466390B2 (en) * | 2008-01-08 | 2013-06-18 | Rosemount Aerospace Inc. | Heater control architecture for an ice protection system |
US8120228B2 (en) * | 2008-07-15 | 2012-02-21 | Hamilton Sundstrand Corporation | Slip ring assembly |
US9656757B2 (en) * | 2008-09-16 | 2017-05-23 | Hamilton Sundstrand Corporation | Propeller deicing system |
GB2463675A (en) * | 2008-09-19 | 2010-03-24 | Vestas Wind Sys As | Wind turbine de-icing |
CN101695959B (zh) * | 2009-10-22 | 2012-01-11 | 北京航空航天大学 | 直升机旋翼防除冰装置 |
US8779945B2 (en) * | 2010-03-17 | 2014-07-15 | Sikorsky Aircraft Corporation | Virtual ice accretion meter display |
FR2962271B1 (fr) * | 2010-07-02 | 2012-08-17 | Hispano Suiza Sa | Alimentation electrique des equipements portes par un support rotatif |
US8890032B2 (en) | 2010-09-17 | 2014-11-18 | Hamilton Sundstrand Corporation | Propeller heater lead |
US8827207B2 (en) | 2011-05-03 | 2014-09-09 | Goodrich Corporation | Ice protection system |
US10513340B2 (en) | 2012-08-02 | 2019-12-24 | Rosemount Aerospace Inc. | Rotor ice protection systems and methods |
GB201301789D0 (en) * | 2013-02-01 | 2013-03-20 | Rolls Royce Plc | A de-icing apparatus and a method of using the same |
US9745070B2 (en) * | 2014-11-11 | 2017-08-29 | The Boeing Company | Systems for multiple zone heaters for rotor craft and methods of operation |
US20180086470A1 (en) * | 2015-03-06 | 2018-03-29 | Sikorsky Aircraft Corporation | Heating design for rotorcraft blade de-icing and anti-icing |
USD808328S1 (en) | 2016-09-14 | 2018-01-23 | Bell Helicopter Textron Inc. | Foldable tiltrotor aircraft |
CN106737368A (zh) * | 2016-12-13 | 2017-05-31 | 惠阳航空螺旋桨有限责任公司 | 一种调整导电环与径向刷架组件位置的工具 |
US10710732B2 (en) * | 2017-09-15 | 2020-07-14 | Bell Helicopter Textron Inc. | Rotary aircraft ice protection system |
US10752367B2 (en) | 2018-05-02 | 2020-08-25 | Bell Helicopter Textron Inc. | Scavenged-power ice-management system and method for an aircraft |
US11427314B2 (en) | 2018-05-15 | 2022-08-30 | Textron Innovations Inc. | Control systems and methods for rotating systems |
CN109558650B (zh) * | 2018-11-09 | 2023-09-01 | 中国直升机设计研究所 | 直升机旋翼结冰对旋翼性能影响的分析方法 |
US11427335B2 (en) * | 2018-11-13 | 2022-08-30 | Textron Innovations Inc. | Enclosure for contacts of aircraft wing heater blanket |
USD909278S1 (en) | 2018-11-15 | 2021-02-02 | Bell Helicopter Textron Inc. | Foldable tiltrotor aircraft |
USD974277S1 (en) | 2018-11-15 | 2023-01-03 | Textron Innovations, Inc. | Aircraft payload enclosure |
USD974276S1 (en) | 2018-11-15 | 2023-01-03 | Textron Innovations, Inc. | Aircraft spinner |
USD909949S1 (en) | 2018-11-15 | 2021-02-09 | Bell Helicopter Textron Inc. | Tiltrotor aircraft |
CN111114792B (zh) * | 2019-12-19 | 2021-04-23 | 武汉航空仪表有限责任公司 | 一种可解算结冰速率的结冰传感器及方法 |
USD944331S1 (en) * | 2021-02-26 | 2022-02-22 | Shantou Chenghai Longman Technology Co., Ltd | Quadrotor |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2393635A (en) * | 1942-04-17 | 1946-01-29 | Robert H Wendt | Ice removing device for aircraft |
US2473147A (en) * | 1946-01-15 | 1949-06-14 | United Aircraft Corp | Slip-ring structure |
US2638295A (en) * | 1947-04-19 | 1953-05-12 | Curtiss Wright Corp | Propeller deicing mechanism |
US2678181A (en) * | 1948-07-20 | 1954-05-11 | Gen Motors Corp | Propeller deicing control system |
US3002718A (en) * | 1960-07-08 | 1961-10-03 | Kaman Aircraft Corp | Rotor blade deicing system |
US3196254A (en) * | 1961-02-21 | 1965-07-20 | Allied Chem | Heater control systems |
US3657514A (en) * | 1970-06-03 | 1972-04-18 | Goodrich Co B F | Electrical deicer for aircraft propeller |
US4292502A (en) * | 1979-02-05 | 1981-09-29 | The B.F. Goodrich Company | Helicopter deicer control system |
DE3164856D1 (en) * | 1980-05-08 | 1984-08-23 | Lucas Ind Plc | Switching system for sequential connection of loads to an electrical supply |
DE3437304A1 (de) * | 1984-10-11 | 1986-04-17 | Licentia Patent-Verwaltungs-Gmbh, 6000 Frankfurt | Verfahren zur bestimmung der temperatur, vorzugsweise der eisgrenzschichttemperatur, eines elektrischen widerstandsheizelementes einer enteisungsanlage fuer flugzeuge, hubschrauber oder dergleichen |
US4690353A (en) * | 1985-05-31 | 1987-09-01 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Electro-expulsive separation system |
US5523959A (en) * | 1994-04-25 | 1996-06-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Ice detector and deicing fluid effectiveness monitoring system |
GB2293522B (en) * | 1994-09-02 | 1999-01-20 | Ultra Electronics Ltd | Rotary apparatus |
US5709532A (en) * | 1994-12-29 | 1998-01-20 | The B.F. Goodrich Company | Propeller ice protection system and method providing reduced sliding contact maintenance |
US5704567A (en) * | 1995-10-16 | 1998-01-06 | The United States Of America As Represented By The Secretary Of The Army | Blade de-icer for rotary wing aircraft |
FR2756254B1 (fr) * | 1996-11-27 | 1999-01-29 | Eurocopter France | Dispositif de chauffage d'un profil aerodynamique |
US6753513B2 (en) | 2002-03-19 | 2004-06-22 | Hamilton Sundstrand | Propeller de-icing system |
US8550402B2 (en) * | 2005-04-06 | 2013-10-08 | Sikorsky Aircraft Corporation | Dual-channel deicing system for a rotary wing aircraft |
-
2005
- 2005-02-24 EP EP05723643.2A patent/EP1851110B1/en active Active
- 2005-02-24 DE DE05723643T patent/DE05723643T1/de active Pending
- 2005-02-24 CN CN2005800410753A patent/CN101068715B/zh not_active Expired - Fee Related
- 2005-02-24 WO PCT/US2005/005854 patent/WO2006093480A1/en active Application Filing
- 2005-02-24 US US11/662,859 patent/US7604202B2/en active Active
- 2005-02-24 CA CA2704249A patent/CA2704249C/en active Active
- 2005-02-24 CA CA2586094A patent/CA2586094C/en active Active
- 2005-02-24 BR BRPI0518456-8A patent/BRPI0518456A2/pt not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
CA2586094A1 (en) | 2006-09-08 |
DE05723643T1 (de) | 2008-04-03 |
CA2586094C (en) | 2010-06-29 |
US7604202B2 (en) | 2009-10-20 |
CN101068715B (zh) | 2012-01-25 |
EP1851110A1 (en) | 2007-11-07 |
CA2704249C (en) | 2013-02-12 |
WO2006093480A1 (en) | 2006-09-08 |
CN101068715A (zh) | 2007-11-07 |
CA2704249A1 (en) | 2006-09-08 |
EP1851110A4 (en) | 2012-04-18 |
EP1851110B1 (en) | 2016-06-22 |
US20070257153A1 (en) | 2007-11-08 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
BRPI0518456A2 (pt) | sistema de gerenciamento de gelo para aeronave tiltrotor | |
BR112015011248A2 (pt) | micrograde baseada em sistema de trigeração híbrido combinada com resfriamento, aquecimento e fornecimento de energia de aquecimento, resfriamento, geração de energia elétrica e armazenamento de energia usando um sistema de automação integrado para monitoramento, análise e controle. | |
BRPI0818967A2 (pt) | Sistema de fornecimento de energia, sistema de ar condicionado e método para prover ar condicionado a aeronaves com operação do ar de sangria em modo hídrico | |
BR112012017396A2 (pt) | sistema multifuncional de descongelamento / anticongelamento | |
BRPI0514963A (pt) | fluido de transferência térmica colorido, sistema de transferência térmica, método para colorir um fluido de transferência térmica possuindo baixa condutividade, e dispositivo acionado por uma fonte de energia alternativa | |
BR102016007236A8 (pt) | Montagem de conversão de potência refrigerada | |
BRPI0518686A2 (pt) | sistema de suprimento para suprimento de energia em uma aeronave, aeronave e mÉtodo de suprimento de energia para uma aeronave | |
IN2012DN05106A (pt) | ||
BR112014016567A8 (pt) | dispositivo de campo continuamente energizado | |
MX2022001589A (es) | Unidad de calentamiento/enfriamiento de flujo variable de refrigerante, de multiples zonas, centralizado. | |
WO2014173572A3 (de) | Kraftwerkssystem mit thermochemischem speicher | |
WO2012120097A3 (en) | Thermal energy system and method of operation | |
SA518392156B1 (ar) | وحدة تبريد لحجرة إمداد طاقة كهربائية لمركبة سكة حديد، وحجرة إمداد طاقة كهربائية ومركبة سكة حديد ذات صلة | |
BR112014030970A2 (pt) | sistema de energia solar; e método para aquecer ou arrefecer uma região com o uso de um sistema de energia solar | |
PL2142704T3 (pl) | Zespół wymiennika ciepła do ogrzewania urządzeń i powierzchni oraz ogrzewania zwrotnic | |
BR112013020990A2 (pt) | sistema doméstico com múltiplos sistemas peltier | |
BR112016002434B8 (pt) | Sistema de coleta de energia térmica e conversão de potência, e, método para geração de energia elétrica suplementar do calor desperdiçado | |
BRPI0716690A2 (pt) | refrigeraÇço para instalaÇço em aeronave | |
BR112012015635A2 (pt) | avião e sistema de controle de um avião propelido por pelo menos um motor a jato alojado em uma nacela. | |
BR112017006538A2 (pt) | fonte de alimentação do tipo soldagem com túnel de vento? | |
BR112014031905A2 (pt) | conjunto de pilha de células de combustível, e, método para operação de uma pilha de células de combustível | |
CY1117669T1 (el) | Εγκατασταση αιολικης ενεργειας | |
BR112013023753A2 (pt) | sistema de escape para um motor de combustão interna com um gerador termoelétrico integrado, e, uso de um sistema de escape | |
BR112012020769A2 (pt) | aparelho para resfriamento, e, uso de um aparelho | |
FR2963866B1 (fr) | Bloc de chauffe pour radiateur electrique de chauffage |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] |
Free format text: REFERENTE A 11A 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 2364 DE 26-04-2016 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. |