WO2010005341A3 - Полое крыло с воздухосборником в носке - Google Patents

Полое крыло с воздухосборником в носке Download PDF

Info

Publication number
WO2010005341A3
WO2010005341A3 PCT/RU2009/000335 RU2009000335W WO2010005341A3 WO 2010005341 A3 WO2010005341 A3 WO 2010005341A3 RU 2009000335 W RU2009000335 W RU 2009000335W WO 2010005341 A3 WO2010005341 A3 WO 2010005341A3
Authority
WO
WIPO (PCT)
Prior art keywords
leading edge
air intake
hollow wing
wing
hollow
Prior art date
Application number
PCT/RU2009/000335
Other languages
English (en)
French (fr)
Other versions
WO2010005341A2 (ru
Inventor
Юрий Витальевич ШВЕД
Original Assignee
Shved Yuriy Vitalievich
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 Shved Yuriy Vitalievich filed Critical Shved Yuriy Vitalievich
Priority to CN2009801268560A priority Critical patent/CN102271997A/zh
Priority to UAA201015567A priority patent/UA98558C2/ru
Publication of WO2010005341A2 publication Critical patent/WO2010005341A2/ru
Publication of WO2010005341A3 publication Critical patent/WO2010005341A3/ru
Priority to IL210329A priority patent/IL210329A0/en

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C21/00Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)

Abstract

Изобретение относится к области авиации. Полое крыло с воздухозаборником в носке включает нижнюю поверхность, верхнюю поверхность. Верхняя поверхность снабжена карманами, образующими соответствующие сужающиеся каналы с выходом потока через щель в верхней поверхности крыла. Изобретение направлено на улучшение аэродинамических характеристик.
PCT/RU2009/000335 2008-07-11 2009-07-03 Использование избыточного давления внутри мягкого крыла для организации выдува части набегающего потока на его верхнюю поверхность через профилированную щель WO2010005341A2 (ru)

Priority Applications (3)

Application Number Priority Date Filing Date Title
CN2009801268560A CN102271997A (zh) 2008-07-11 2009-07-03 前缘带有进气口的中空机翼
UAA201015567A UA98558C2 (ru) 2008-07-11 2009-07-03 Полое крыло с воздухозаборником в носке профиля и профилированной щелью на верхней поверхности
IL210329A IL210329A0 (en) 2008-07-11 2010-12-28 The use of excess pressure in a paraglider wing to blow out a portion of approach flow onto the wing upper wall through a shaped slot

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2008128067/11A RU2389644C2 (ru) 2008-07-11 2008-07-11 Полое мягкое крыло с воздухозаборником в носке и профилированной щелью на верхней поверхности
RU2008128067 2008-07-11

Publications (2)

Publication Number Publication Date
WO2010005341A2 WO2010005341A2 (ru) 2010-01-14
WO2010005341A3 true WO2010005341A3 (ru) 2010-03-04

Family

ID=41507614

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2009/000335 WO2010005341A2 (ru) 2008-07-11 2009-07-03 Использование избыточного давления внутри мягкого крыла для организации выдува части набегающего потока на его верхнюю поверхность через профилированную щель

Country Status (5)

Country Link
CN (1) CN102271997A (ru)
IL (1) IL210329A0 (ru)
RU (1) RU2389644C2 (ru)
UA (1) UA98558C2 (ru)
WO (1) WO2010005341A2 (ru)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2444462C1 (ru) * 2010-06-28 2012-03-10 Юрий Витальевич Швед Мягкое двухоболочковое крыло с распорными элементами жесткости
RU2508228C1 (ru) * 2012-12-11 2014-02-27 Алексей Николаевич Пеков Способ управления пограничным слоем на аэродинамической поверхности летательного аппарата и устройство для его осуществления

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191349A (en) * 1978-03-24 1980-03-04 Cabinet Lavoix Parachute having an improved multi-cell canopy
FR2633248A1 (fr) * 1988-06-28 1989-12-29 Degraces Jacques Dispositif d'alveoles etanches pour ailes-parachutes
RU1782869C (ru) * 1989-05-29 1992-12-23 Нижегородское авиационное производственное объединение им.С.Орджоникидзе Параплан

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004024007B4 (de) * 2004-05-13 2007-10-11 Airbus Deutschland Gmbh Flugzeugkomponente, insbesondere Flügel

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4191349A (en) * 1978-03-24 1980-03-04 Cabinet Lavoix Parachute having an improved multi-cell canopy
FR2633248A1 (fr) * 1988-06-28 1989-12-29 Degraces Jacques Dispositif d'alveoles etanches pour ailes-parachutes
RU1782869C (ru) * 1989-05-29 1992-12-23 Нижегородское авиационное производственное объединение им.С.Орджоникидзе Параплан

Also Published As

Publication number Publication date
CN102271997A (zh) 2011-12-07
RU2008128067A (ru) 2010-01-20
UA98558C2 (ru) 2012-05-25
RU2389644C2 (ru) 2010-05-20
WO2010005341A2 (ru) 2010-01-14
IL210329A0 (en) 2011-03-31

Similar Documents

Publication Publication Date Title
USD736140S1 (en) Vertical takeoff and landing vehicle
EP2493758A4 (en) LAMINAR FLOW WING FOR AIRPLANES FLYING WITH SUPERIOR AND HIGH UNTERSCHALL SPEED
WO2008154066A3 (en) Methods and apparatus for aircraft
JP2011504149A5 (ja) 航空機翼の後縁フラップを移動させるための装置及び同装置を備えた航空機
EP2157305A3 (en) Gas turbine engine with variable area fan nozzle
WO2013106120A3 (en) Device, assembly, and system for reducing aerodynamic drag
GB201303606D0 (en) Scalloped surface turbine stage with purge trough
WO2010084025A3 (de) Hochauftriebsklappe, anordnung einer hochauftriebsklappe mit einer vorrichtung zur strömungsbeeinflussung an derselben sowie flugzeug mit einer derartigen anordnung
EP2567892A3 (en) Aircraft tail surface with a leading edge section of undulated shape
DK201270120A (en) Lift device for rotor blade in wind turbine
EP2597037A3 (en) An Aircraft
PL2368035T3 (pl) Łopata turbiny wiatrowej zaopatrzona w spoiler o skutecznym rozdzielaniu przepływu powietrza
WO2011139316A3 (en) Aircraft vertical lift device
WO2012138841A3 (en) Surface flow enhancement device and method of using the same on a vehicle
EP2444645A3 (en) Gas turbine engine with variable area fan nozzle
EP2612990A3 (en) Gas turbine nozzle with a flow fence
BRPI0921378A2 (pt) entrada de ar de um motor de avião do tipo com hélices propulsoras não carenadas, motor de avião e avião
CA2867791C (en) Total air temperature sensors
WO2010001009A3 (fr) Support d'appareils de mesure intercale entre une motorisation et une entree d'air d'une nacelle d'aeronef
EP2447519A3 (en) Gas turbine engine with variable area fan nozzle
WO2013173769A8 (en) Fluid turbine with rotor upwind of ringed airfoil
EP2610179A3 (en) Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
FR2974563B1 (fr) Profil aerodynamique reduisant le deficit de vitesse dans son sillage
WO2012010965A3 (en) Vtol aircraft with a thrust-to-weight ratio smaller than 1
FR2927609B1 (fr) Entree d'air pour nacelle d'aeronef, et nacelle equipee d'une telle entree d'air

Legal Events

Date Code Title Description
WWE Wipo information: entry into national phase

Ref document number: 200980126856.0

Country of ref document: CN

121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 09794705

Country of ref document: EP

Kind code of ref document: A2

WWE Wipo information: entry into national phase

Ref document number: 210329

Country of ref document: IL

NENP Non-entry into the national phase

Ref country code: DE

WWE Wipo information: entry into national phase

Ref document number: A201015567

Country of ref document: UA

122 Ep: pct application non-entry in european phase

Ref document number: 09794705

Country of ref document: EP

Kind code of ref document: A2