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BR0316038A - Combinação de uma asa e fuselagem de aeronave - Google Patents

Combinação de uma asa e fuselagem de aeronave

Info

Publication number
BR0316038A
BR0316038A BR0316038-6A BR0316038A BR0316038A BR 0316038 A BR0316038 A BR 0316038A BR 0316038 A BR0316038 A BR 0316038A BR 0316038 A BR0316038 A BR 0316038A
Authority
BR
Brazil
Prior art keywords
wing
combination
fuselage
aircraft fuselage
aircraft
Prior art date
Application number
BR0316038-6A
Other languages
English (en)
Other versions
BR0316038B1 (pt
Inventor
Richard R Tracy
James D Chase
Illan Kroo
Original Assignee
Aerion Corp
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 Aerion Corp filed Critical Aerion Corp
Publication of BR0316038A publication Critical patent/BR0316038A/pt
Publication of BR0316038B1 publication Critical patent/BR0316038B1/pt

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C30/00—Supersonic type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/146—Aerofoil profile comprising leading edges of particular shape
    • 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
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Tires In General (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Exhaust Silencers (AREA)
  • Structure Of Belt Conveyors (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

"COMBINAçãO DE UMA ASA E FUSELAGEM DE AERONAVE". A invenção se refere a uma combinação de uma asa de aeronave e fuselagem, compreendendo a asa tendo convexidade na ou próximo à borda dianteira de asa que tem agudeza cega e baixo ângulo de inclinação, e a fuselagem tendo endentação ao longo do lado de asa da mesma, e ao longo do comprimento da fuselagem.
BRPI0316038-6B1A 2002-11-07 2003-11-06 combinaÇço de uma asa e fuselagem de aeronave BR0316038B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US42403902P 2002-11-07 2002-11-07
US10/693,411 US7000870B2 (en) 2002-11-07 2003-10-23 Laminar flow wing for transonic cruise
PCT/US2003/035393 WO2004043780A2 (en) 2002-11-07 2003-11-06 Laminar flow wing for transonic cruise

Publications (2)

Publication Number Publication Date
BR0316038A true BR0316038A (pt) 2005-09-13
BR0316038B1 BR0316038B1 (pt) 2013-06-25

Family

ID=32314520

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0316038-6B1A BR0316038B1 (pt) 2002-11-07 2003-11-06 combinaÇço de uma asa e fuselagem de aeronave

Country Status (9)

Country Link
US (1) US7000870B2 (pt)
EP (1) EP1583690B1 (pt)
JP (1) JP4520306B2 (pt)
AT (1) ATE455034T1 (pt)
AU (1) AU2003287542B2 (pt)
BR (1) BR0316038B1 (pt)
CA (1) CA2503270C (pt)
DE (1) DE60331004D1 (pt)
WO (1) WO2004043780A2 (pt)

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US20060289679A1 (en) * 2005-06-27 2006-12-28 Johnson Kaj A Modular sprayer
US8272594B2 (en) * 2009-10-26 2012-09-25 Aerion Corporation Laminar flow wing optimized for supersonic cruise aircraft
US8448893B2 (en) * 2009-10-26 2013-05-28 Aerion Corporation Laminar flow wing optimized for transonic cruise aircraft
US8317128B2 (en) * 2009-10-26 2012-11-27 Aerion Corporation Laminar flow wing optimized for transonic cruise aircraft
CN104897006A (zh) * 2015-04-24 2015-09-09 江西洪都航空工业集团有限责任公司 一种靶机气动布局
CN106828875B (zh) * 2016-12-27 2018-11-16 西北工业大学 一种适用于通用飞行器偏重爬升特性的层流翼型
EP3348470B1 (en) * 2017-01-16 2019-03-06 Deutsches Zentrum für Luft- und Raumfahrt e.V. Airplane or vehicle with configuration of a t junction of a flow obstacle on a wall bounding a flow
CN107444612B (zh) * 2017-08-15 2023-04-18 中国空气动力研究与发展中心高速空气动力研究所 一种λ机翼飞翼布局无人飞行器的变机翼前缘装置
JP7038404B2 (ja) 2017-12-12 2022-03-18 国立研究開発法人宇宙航空研究開発機構 遷音速翼型、翼及び航空機
WO2021005892A1 (ja) * 2019-07-10 2021-01-14 浜松ホトニクス株式会社 半導体デバイス検査方法及び半導体デバイス検査装置
DE102019129998B4 (de) * 2019-11-07 2022-04-28 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeug mit Strahltriebwerken oberhalb der Tragflügel und mit einer lokalen Erweiterung des Rumpfs zur Reduktion aerodynamischer Widerstände bei transsonischen Fluggeschwindigkeiten
JP7015582B2 (ja) * 2020-09-03 2022-02-03 国立研究開発法人宇宙航空研究開発機構 翼及び航空機

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Also Published As

Publication number Publication date
JP2006517162A (ja) 2006-07-20
EP1583690A2 (en) 2005-10-12
DE60331004D1 (de) 2010-03-04
CA2503270A1 (en) 2004-05-27
WO2004043780A3 (en) 2005-08-18
JP4520306B2 (ja) 2010-08-04
AU2003287542A1 (en) 2004-06-03
AU2003287542B2 (en) 2009-07-02
US7000870B2 (en) 2006-02-21
CA2503270C (en) 2011-05-17
EP1583690A4 (en) 2009-02-18
ATE455034T1 (de) 2010-01-15
US20040129837A1 (en) 2004-07-08
WO2004043780A2 (en) 2004-05-27
EP1583690B1 (en) 2010-01-13
BR0316038B1 (pt) 2013-06-25

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Legal Events

Date Code Title Description
B06A Patent application procedure suspended [chapter 6.1 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 06/11/2003, OBSERVADAS AS CONDICOES LEGAIS.

B21F Lapse acc. art. 78, item iv - on non-payment of the annual fees in time

Free format text: REFERENTE A 11A ANUIDADE.

B24J Lapse because of non-payment of annual fees (definitively: art 78 iv lpi, resolution 113/2013 art. 12)

Free format text: EM VIRTUDE DA EXTINCAO PUBLICADA NA RPI 2279 DE 09-09-2014 E CONSIDERANDO AUSENCIA DE MANIFESTACAO DENTRO DOS PRAZOS LEGAIS, INFORMO QUE CABE SER MANTIDA A EXTINCAO DA PATENTE E SEUS CERTIFICADOS, CONFORME O DISPOSTO NO ARTIGO 12, DA RESOLUCAO 113/2013.