BRPI0516131A - método para projetar um veìculo aéreo - Google Patents

método para projetar um veìculo aéreo

Info

Publication number
BRPI0516131A
BRPI0516131A BRPI0516131-2A BRPI0516131A BRPI0516131A BR PI0516131 A BRPI0516131 A BR PI0516131A BR PI0516131 A BRPI0516131 A BR PI0516131A BR PI0516131 A BRPI0516131 A BR PI0516131A
Authority
BR
Brazil
Prior art keywords
aerodynamic shape
designing
determining
preferred
aerodynamic
Prior art date
Application number
BRPI0516131-2A
Other languages
English (en)
Inventor
Jim C Narramore
Stacey Kelly
Robert Milliken
Original Assignee
Bell Helicopter Textron Inc
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
Application filed by Bell Helicopter Textron Inc filed Critical Bell Helicopter Textron Inc
Publication of BRPI0516131A publication Critical patent/BRPI0516131A/pt

Links

Classifications

    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/10—Geometric CAD
    • G06F30/15—Vehicle, aircraft or watercraft design
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F30/00—Computer-aided design [CAD]
    • G06F30/20—Design optimisation, verification or simulation
    • G06F30/23—Design optimisation, verification or simulation using finite element methods [FEM] or finite difference methods [FDM]
    • G—PHYSICS
    • G06—COMPUTING OR CALCULATING; COUNTING
    • G06F—ELECTRIC DIGITAL DATA PROCESSING
    • G06F2111/00—Details relating to CAD techniques
    • G06F2111/10—Numerical modelling
    • 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
    • Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Geometry (AREA)
  • Theoretical Computer Science (AREA)
  • General Physics & Mathematics (AREA)
  • Computer Hardware Design (AREA)
  • Evolutionary Computation (AREA)
  • General Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Computational Mathematics (AREA)
  • Mathematical Analysis (AREA)
  • Mathematical Optimization (AREA)
  • Pure & Applied Mathematics (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Automobile Manufacture Line, Endless Track Vehicle, Trailer (AREA)
  • Management, Administration, Business Operations System, And Electronic Commerce (AREA)

Abstract

MéTODO PARA PROJETAR UM VEìCULO AéREO. Trata-se de um método para projetar um veículo aéreo que inclui determinar um formato aerodinâmico preferido de uma estrutura do veículo; modificar o formato aerodinâmico preferido com base em restrições; e determinar, utilizando dinâmicas de fluido computacional aerodinâmicas, condições de carga limite para o formato aerodinâmico modificado. Um sistema implementado por computador para projetar um veículo aéreo inclui pelo menos um computador operável para determinar um formato aerodinâmico preferido de uma estrutura do veículo; modificar o formato aerodinâmico preferido com base em restrições; e determinar, utilizando dinâmicas de fluido computacional aerodinâmicas, condições de carga limite para o formato aerodinâmico modificado. Um software para projetar um veículo aéreo, incorporado em um meio legível por computador, é operável, quando executado, determina um formato aerodinâmico preferido de uma estrutura do veículo; modificar o formato aerodinâmico preferido com base em restrições; e determinar, utilizando dinâmicas de fluido computacional aerodinâmicas, condições de carga limite para o formato aerodinâmico modificado.
BRPI0516131-2A 2004-10-15 2005-10-17 método para projetar um veìculo aéreo BRPI0516131A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US61941004P 2004-10-15 2004-10-15
PCT/US2005/037033 WO2007001413A2 (en) 2004-10-15 2005-10-17 Method for designing a flight vehicle

Publications (1)

Publication Number Publication Date
BRPI0516131A true BRPI0516131A (pt) 2008-08-26

Family

ID=37595595

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0516131-2A BRPI0516131A (pt) 2004-10-15 2005-10-17 método para projetar um veìculo aéreo

Country Status (7)

Country Link
US (1) US7912681B2 (pt)
EP (1) EP1828883B1 (pt)
CN (1) CN100543754C (pt)
BR (1) BRPI0516131A (pt)
CA (1) CA2583468C (pt)
DE (1) DE05858238T1 (pt)
WO (1) WO2007001413A2 (pt)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8688408B2 (en) * 2006-11-08 2014-04-01 The Boeing Company Flight in factory
US8209839B1 (en) * 2006-11-28 2012-07-03 Florida Turbine Technologies, Inc. Process for re-designing a distressed component used under thermal and structural loading
ES2341065B1 (es) * 2007-10-25 2011-06-13 Airbus España, S.L. Metodos y sistemas para mejorar mallas usadas en dinamica de fluidos computacional.
US8280663B2 (en) * 2007-10-31 2012-10-02 Airbus Operations S.L. Methods and systems for assisting in the design of mobile surfaces of objects
GB0810645D0 (en) * 2008-06-11 2008-07-16 Airbus Uk Ltd Method of designing an airfoil assembly
FR2955797B1 (fr) * 2010-02-03 2012-05-25 Airbus Operations Sas Procede et dispositif pour realiser un outillage destine a fabriquer une pointe arriere d'un avion.
US8645114B1 (en) 2010-10-06 2014-02-04 The Boeing Company Data point averaging for computational fluid dynamics data
CN102023640B (zh) * 2010-11-23 2012-07-04 北京航空航天大学 飞行包线内标称设计点的选择方法
US8457939B2 (en) 2010-12-30 2013-06-04 Aerion Corporation Generating inviscid and viscous fluid-flow simulations over an aircraft surface using a fluid-flow mesh
US8538738B2 (en) 2011-03-22 2013-09-17 Aerion Corporation Predicting transition from laminar to turbulent flow over a surface
US8892408B2 (en) 2011-03-23 2014-11-18 Aerion Corporation Generating inviscid and viscous fluid flow simulations over a surface using a quasi-simultaneous technique
FR2982024B1 (fr) * 2011-10-28 2014-06-13 Airbus Operations Sas Procede de calcul de pression dynamique au niveau d'une surface d'aeronef
US8949087B2 (en) * 2012-03-01 2015-02-03 The Boeing Company System and method for structural analysis
US9977848B1 (en) 2014-07-10 2018-05-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method and system for predicting rocket nozzle deformation during engine start-up and shut-down transients
CN105468851A (zh) * 2015-11-26 2016-04-06 中国航空工业集团公司沈阳飞机设计研究所 一种确定飞机动态重量特性的方法
US11295046B2 (en) 2019-04-12 2022-04-05 Cnh Industrial America Llc Systems and methods for expediting design of physical components through use of computationally efficient virtual simulations
US11544425B2 (en) 2019-04-12 2023-01-03 Cnh Industrial America Llc Systems and methods for expediting design of physical components through use of computationally efficient virtual simulations

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3070999A (en) * 1956-05-07 1963-01-01 Garbell Res Foundation Fluid velocity measuring system for rotorcraft
US5939007A (en) * 1994-08-31 1999-08-17 Sikorsky Aircraft Corporation Method for manufacture of a fiber reinforced composite spar for rotary wing aircraft
JP4128626B2 (ja) * 1996-03-22 2008-07-30 ザ・ボーイング・カンパニー 決定的な翼アセンブリ
WO1998046418A1 (en) * 1997-04-16 1998-10-22 Sikorsky Aircraft Corporation Apparatus and method for installing a leading-edge sheath onto a helicopter main rotor blade subassembly
US5984511A (en) * 1997-05-12 1999-11-16 Mcdonnell Douglas Corporation Knowledge driven composite design optimization process and system therefor
US6793175B1 (en) * 1999-08-25 2004-09-21 The Boeing Company Supersonic external-compression diffuser and method for designing same
US20030048269A1 (en) * 2001-09-12 2003-03-13 Powell Donald T. System and method for generating finite element models
DE60321390D1 (de) * 2003-01-23 2008-07-10 Bell Helicopter Textron Inc Propellerblatt mit führungskantennut
EP1616228A4 (en) * 2003-03-31 2013-05-29 Sikorsky Aircraft Corp TECHNICAL DESIGN CONCEPTS TO IMPROVE HELICOPTER DISASTER PREVENTION AND OPERATION IN BROWNOUT CONDITIONS
US8016244B2 (en) * 2004-02-20 2011-09-13 The Boeing Company Active systems and methods for controlling an airfoil vortex

Also Published As

Publication number Publication date
EP1828883A4 (en) 2008-01-09
CA2583468A1 (en) 2007-01-04
WO2007001413A2 (en) 2007-01-04
WO2007001413A3 (en) 2007-04-19
CN101040284A (zh) 2007-09-19
EP1828883A2 (en) 2007-09-05
US7912681B2 (en) 2011-03-22
DE05858238T1 (de) 2008-03-13
CN100543754C (zh) 2009-09-23
US20080140359A1 (en) 2008-06-12
CA2583468C (en) 2013-12-17
EP1828883B1 (en) 2015-12-23

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Legal Events

Date Code Title Description
B08F Application fees: application dismissed [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 2328 DE 18-08-2015 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.