SU1840518A1 - Flying vehicle - Google Patents

Flying vehicle

Info

Publication number
SU1840518A1
SU1840518A1 SU3019504/11A SU3019504A SU1840518A1 SU 1840518 A1 SU1840518 A1 SU 1840518A1 SU 3019504/11 A SU3019504/11 A SU 3019504/11A SU 3019504 A SU3019504 A SU 3019504A SU 1840518 A1 SU1840518 A1 SU 1840518A1
Authority
SU
USSR - Soviet Union
Prior art keywords
flying vehicle
vortex generators
sweep
dwg
fuselage
Prior art date
Application number
SU3019504/11A
Other languages
Russian (ru)
Inventor
Георгий Петрович Свищев
Ростислав Аполлосович Беляков
Евгений Семенович Вождаев
Юрий Васильевич Андреев
Николай Николаевич Долженко
Владимир Алексеевич Головкин
Михаил Алексеевич Головкин
Валентин Иванович Пятахин
Борис Федорович Демидов
Максим Михайлович Михайлов
Ирма Леоновна Добролюбова
Original Assignee
Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского"
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 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" filed Critical Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского"
Priority to SU3019504/11A priority Critical patent/SU1840518A1/en
Application granted granted Critical
Publication of SU1840518A1 publication Critical patent/SU1840518A1/en

Links

Classifications

    • 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

Abstract

FIELD: aviation industry.SUBSTANCE: proposed flying vehicle has fuselage, wing with extensions and vortex generators with acute vertex, sweep-back sweep-forward edges. Vortex generators are installed along leading edge of extension.EFFECT: enlarged operating range of angles of attack.3 dwg
SU3019504/11A 1981-05-29 1981-05-29 Flying vehicle SU1840518A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU3019504/11A SU1840518A1 (en) 1981-05-29 1981-05-29 Flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU3019504/11A SU1840518A1 (en) 1981-05-29 1981-05-29 Flying vehicle

Publications (1)

Publication Number Publication Date
SU1840518A1 true SU1840518A1 (en) 2007-05-20

Family

ID=60521963

Family Applications (1)

Application Number Title Priority Date Filing Date
SU3019504/11A SU1840518A1 (en) 1981-05-29 1981-05-29 Flying vehicle

Country Status (1)

Country Link
SU (1) SU1840518A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2556745C1 (en) * 2014-05-21 2015-07-20 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Device for improvement of aircraft lifting properties
RU2671595C1 (en) * 2017-11-30 2018-11-02 Сергей Николаевич Низов Multi-mode aerodynamic surface

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2556745C1 (en) * 2014-05-21 2015-07-20 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Device for improvement of aircraft lifting properties
RU2671595C1 (en) * 2017-11-30 2018-11-02 Сергей Николаевич Низов Multi-mode aerodynamic surface
WO2019108090A1 (en) * 2017-11-30 2019-06-06 Сергей Николаевич НИЗОВ Multi-mode airfoil

Similar Documents

Publication Publication Date Title
US4245804B1 (en) Minimum drag wing configuration for aircraft operating at transonic speeds
DE3471634D1 (en) Aircraft wing and winglet arrangement
GB2010761B (en) Tapered variable camber leading edge flap for aircraft wing
DE3568317D1 (en) Aircraft trailing edge flap apparatus
DE69511836T2 (en) Brake flap with adjustable gap for an airplane wing
DE3169141D1 (en) Aircraft wing provided with a high-lift device in the leading edge, and aircraft provided with such a wing
BR8305580A (en) TAIL ROTOR ARRANGEMENT FOR TURNING WING AIRCRAFT AND DEVICE FOR INCREASING THE TAIL ARRANGEMENT FOR TURNING WING AIRCRAFT
EP0239138A3 (en) Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps
AU5239098A (en) Airplane with unswept slotted cruise wing airfoil
DE3671874D1 (en) COUPLING SYSTEM FOR TWO FLAPS OF AN AIRPLANE WING AND WINGS THAT ARE EQUIPPED WITH IT.
ATE27126T1 (en) AIRPLANE.
DE3279604D1 (en) Aileron system for aircraft and method of operating the same
EP0076907A3 (en) Aerofoil, in particular for aircraft wing
GB2186849B (en) Variable camber leading edge arrangements for aircraft wings
GB1485683A (en) Helicopter rotor blade
FR2639608B1 (en) DEFROSTER FOR AIRCRAFT PROPELLERS, HELICOPTER ROTORS AND THE LIKE
AU7678281A (en) Airplane wing and undercarriage
EP0141895A3 (en) Aircraft with folding and/or pivoting wings
GB2136746B (en) Mechanism for increasing the flutter speeds of transonic aircraft wings
CA1002027A (en) Wingtip vortex dissipator for aircraft
SU1840518A1 (en) Flying vehicle
DE3177060D1 (en) Leading edge vortex flap for wings
DE3868774D1 (en) REAR EDGE FLAPS OF AN AIRCRAFT WING.
SU1840516A1 (en) Flying vehicle
GB2100684B (en) Flap arrangement for the leading edge of an aircraft wing