BRPI1107040B8 - Método de prover um aerofólio - Google Patents

Método de prover um aerofólio

Info

Publication number
BRPI1107040B8
BRPI1107040B8 BRPI1107040A BRPI1107040A BRPI1107040B8 BR PI1107040 B8 BRPI1107040 B8 BR PI1107040B8 BR PI1107040 A BRPI1107040 A BR PI1107040A BR PI1107040 A BRPI1107040 A BR PI1107040A BR PI1107040 B8 BRPI1107040 B8 BR PI1107040B8
Authority
BR
Brazil
Prior art keywords
airfoil
control point
span
edge
main portion
Prior art date
Application number
BRPI1107040A
Other languages
English (en)
Inventor
Brocklehurst Alan
Original Assignee
Westland Helicopters
Agustawestland Ltd
Leonardo UK Ltd
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.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=43531346&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BRPI1107040(B8) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Westland Helicopters, Agustawestland Ltd, Leonardo UK Ltd filed Critical Westland Helicopters
Publication of BRPI1107040A2 publication Critical patent/BRPI1107040A2/pt
Publication of BRPI1107040B1 publication Critical patent/BRPI1107040B1/pt
Publication of BRPI1107040B8 publication Critical patent/BRPI1107040B8/pt

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/463Blade tips
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/32Rotors
    • B64C27/46Blades
    • B64C27/467Aerodynamic features
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/49332Propeller making

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Wind Motors (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Catching Or Destruction (AREA)

Abstract

AEROFÓLIO. Um aerofólio tem uma porção principal de seção transversal de aerofólio, uma extremidade de raiz no sentido do vão interna onde o aerofólio está em uso fixado a uma estrutura de suporte, e em uma extremidade no sentido do vão mais externo fora da porção principal, além de uma estação de ponta, uma região de ponta, e a região de ponta incluindo uma borda extrema, a configuração de forma de planta da borda extrema situada em uma primeira curva de Bezier construída a partir de pelo menos quatro pontos de controle P1, P2, P3 e P4, os pontos de controle P1, P2, P3 e P4 estando individualmente situados na periferia de um polígono que limita a região de ponta, o ponto de controle de Bezier P1 estando localizado em uma borda dianteira do aerofólio na estação de ponta, a qual está em uma posição no sentido do vão entre 93,5%R e 95,9%R, onde se encontram o primeiro e o segundo lado do polígono, o primeiro lado estando na estação de ponta que se estende perpendicularmente até um eixo de referência de hélice, que se estende no sentido do vão da porção principal do aerofólio, e o segundo lado sendo uma tangente em relação à borda dianteira do aerofólio no ponto de controle P1, que se estende entre o ponto de controle P1 até uma posição onde o segundo lado encontra um terceiro lado do polígono de limite em uma posição no sentido para fora da borda extrema, o terceiro lado sendo paralelo ao primeiro lado e se estendendo entre a posição onde o terceiro lado encontra o segundo lado, até onde se encontram o terceiro lado e o quarto lado, o ponto de controle P2 estando localizado no segundo lado em uma posição entre 30% e 80% ao longo do segundo lado a partir de P1, o ponto de controle P3 estando localizado no terceiro lado em uma posição entre 30% e 90% ao longo do terceiro lado a partir de onde o segundo e o terceiro lado se encontram, e o ponto de controle P4 estando localizado no ponto extremo de extremidade mais externa em uma borda traseira do aerofólio, onde R é o vão de aerofólio, efetivo.
BRPI1107040A 2010-12-02 2011-11-30 Método de prover um aerofólio BRPI1107040B8 (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB1020426.1 2010-12-02
GB1020426.1A GB2486021B (en) 2010-12-02 2010-12-02 Aerofoil

Publications (3)

Publication Number Publication Date
BRPI1107040A2 BRPI1107040A2 (pt) 2015-07-28
BRPI1107040B1 BRPI1107040B1 (pt) 2020-06-23
BRPI1107040B8 true BRPI1107040B8 (pt) 2022-12-13

Family

ID=43531346

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI1107040A BRPI1107040B8 (pt) 2010-12-02 2011-11-30 Método de prover um aerofólio

Country Status (9)

Country Link
US (1) US9085359B2 (pt)
EP (1) EP2508423B1 (pt)
JP (2) JP6068792B2 (pt)
KR (1) KR101808331B1 (pt)
CN (1) CN102582831B (pt)
BR (1) BRPI1107040B8 (pt)
CA (1) CA2759909C (pt)
GB (1) GB2486021B (pt)
RU (1) RU2513355C2 (pt)

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GB2486021B (en) * 2010-12-02 2017-07-19 Agustawestland Ltd Aerofoil
US9216821B1 (en) * 2012-01-03 2015-12-22 The Boeing Company Methods and systems for helicopter rotor blade balancing
FR3009104B1 (fr) * 2013-07-29 2015-08-21 Snecma Procede de modelisation d'une pale d'une helice non-carenee
FR3045564B1 (fr) 2015-12-21 2018-08-17 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'amelioration acoustique lors de vols d'approche et l'amelioration des performances en vols stationnaire et d'avancement
FR3045565B1 (fr) * 2015-12-21 2018-07-27 Airbus Helicopters Pale de rotor d'aeronef a geometrie adaptee pour l'ameloration acoustique lors d'un vol d'approche et l'amelioration des performances en vol d'avancement
GB2555429B (en) * 2016-10-27 2020-04-01 Ge Aviation Systems Llc Propeller assembly
US10899440B2 (en) 2017-03-09 2021-01-26 Sikorsky Aircraft Corporation Rotor blade tip design for improved hover and cruise performance
CN207000809U (zh) * 2017-04-07 2018-02-13 深圳市大疆创新科技有限公司 桨叶、螺旋桨、动力套装及无人飞行器
CN107194122B (zh) * 2017-06-23 2021-01-15 南京理工大学 一种变速风机叶片的多工况气动优化的改进方法
CN107945243B (zh) * 2017-11-23 2021-04-27 杭州电魂网络科技股份有限公司 图像移动方法及装置
WO2019195153A1 (en) * 2018-04-02 2019-10-10 Aero Design Labs, Inc. Elliptical wing tip and method of fabricating same
CN208439418U (zh) * 2018-06-26 2019-01-29 深圳市大疆创新科技有限公司 螺旋桨、动力组件及飞行器
CN109896009B (zh) * 2019-02-20 2024-06-21 丰翼科技(深圳)有限公司 螺旋桨及无人机
CN114658595B (zh) * 2022-03-22 2024-11-22 华能湖北新能源有限责任公司 一种具有前缘延伸增功装置的风力机叶片及其设计方法
US12116119B2 (en) * 2022-03-28 2024-10-15 Lockheed Martin Corporation High speed rotor blade design
CN115577466A (zh) * 2022-09-15 2023-01-06 中国航空研究院 一种大型自适应叶片参数化有限元直接建模方法
US20250223025A1 (en) * 2024-01-04 2025-07-10 United States Of America As Represented By The Administrator Of Nasa Improved propeller
CN117646708B (zh) * 2024-01-30 2024-04-05 清华大学深圳国际研究生院 一种海上风电机组状态的监测分析方法

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Also Published As

Publication number Publication date
BRPI1107040B1 (pt) 2020-06-23
JP6068792B2 (ja) 2017-01-25
US20120237354A1 (en) 2012-09-20
JP2017024717A (ja) 2017-02-02
CA2759909C (en) 2018-09-18
GB2486021A (en) 2012-06-06
RU2513355C2 (ru) 2014-04-20
CN102582831B (zh) 2016-05-04
CA2759909A1 (en) 2012-06-02
BRPI1107040A2 (pt) 2015-07-28
US9085359B2 (en) 2015-07-21
JP2012116477A (ja) 2012-06-21
GB2486021B (en) 2017-07-19
EP2508423A3 (en) 2014-10-08
CN102582831A (zh) 2012-07-18
KR20120060756A (ko) 2012-06-12
RU2011148749A (ru) 2013-06-10
KR101808331B1 (ko) 2017-12-12
EP2508423A2 (en) 2012-10-10
EP2508423B1 (en) 2017-11-15
GB201020426D0 (en) 2011-01-19

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Legal Events

Date Code Title Description
B03A Publication of a patent application or of a certificate of addition of invention [chapter 3.1 patent gazette]
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]
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 30/11/2011, OBSERVADAS AS CONDICOES LEGAIS.

B25D Requested change of name of applicant approved

Owner name: AGUSTAWESTLAND LIMITED (GB)

B25G Requested change of headquarter approved

Owner name: AGUSTAWESTLAND LIMITED (GB)

B25A Requested transfer of rights approved

Owner name: LEONARDO UK LTD (GB)