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SU1600214A3 - Flying vehicle wing - Google Patents

Flying vehicle wing

Info

Publication number
SU1600214A3
SU1600214A3 SU4662090/23A SU4662090A SU1600214A3 SU 1600214 A3 SU1600214 A3 SU 1600214A3 SU 4662090/23 A SU4662090/23 A SU 4662090/23A SU 4662090 A SU4662090 A SU 4662090A SU 1600214 A3 SU1600214 A3 SU 1600214A3
Authority
SU
USSR - Soviet Union
Prior art keywords
airfoils
flying vehicle
area
vehicle wing
antiflutter
Prior art date
Application number
SU4662090/23A
Other languages
Russian (ru)
Inventor
М.С. Комаров
Original Assignee
ЦАГИ им.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 ЦАГИ им.профессора Н.Е.Жуковского filed Critical ЦАГИ им.профессора Н.Е.Жуковского
Priority to SU4662090/23A priority Critical patent/SU1600214A3/en
Application granted granted Critical
Publication of SU1600214A3 publication Critical patent/SU1600214A3/en

Links

Classifications

    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

FIELD: aircraft engineering. SUBSTANCE: antiflutter device is made in the form of airfoils 5, 6 mounted in the nose part of the engine nacelles 1 in a horizontal plane or in combination relative to the axis of symmetry of the engines. The area of the airfoils is 1-20% of the area of the outer surface of nacelle 1. EFFECT: reduced weight and increased critical flutter velocity at improved elastic vibration damping. 2 dwg
SU4662090/23A 1989-03-15 1989-03-15 Flying vehicle wing SU1600214A3 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4662090/23A SU1600214A3 (en) 1989-03-15 1989-03-15 Flying vehicle wing

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4662090/23A SU1600214A3 (en) 1989-03-15 1989-03-15 Flying vehicle wing

Publications (1)

Publication Number Publication Date
SU1600214A3 true SU1600214A3 (en) 1994-02-15

Family

ID=60521656

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4662090/23A SU1600214A3 (en) 1989-03-15 1989-03-15 Flying vehicle wing

Country Status (1)

Country Link
SU (1) SU1600214A3 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2423289C2 (en) * 2006-03-31 2011-07-10 Эрбюс Франс Aircraft wing with engine attachment strut with lateral channel for flow arranged in its front area

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2423289C2 (en) * 2006-03-31 2011-07-10 Эрбюс Франс Aircraft wing with engine attachment strut with lateral channel for flow arranged in its front area

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