SU1637169A1 - Cowling flap for aircraft - Google Patents

Cowling flap for aircraft

Info

Publication number
SU1637169A1
SU1637169A1 SU4765057/23A SU4765057A SU1637169A1 SU 1637169 A1 SU1637169 A1 SU 1637169A1 SU 4765057/23 A SU4765057/23 A SU 4765057/23A SU 4765057 A SU4765057 A SU 4765057A SU 1637169 A1 SU1637169 A1 SU 1637169A1
Authority
SU
USSR - Soviet Union
Prior art keywords
cowling
section
aircraft
flap
bushings
Prior art date
Application number
SU4765057/23A
Other languages
Russian (ru)
Inventor
А.Л. Доброскоков
Г.В. Степанов
И.В. Козлов
Original Assignee
А.Л. Доброскоков
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 А.Л. Доброскоков filed Critical А.Л. Доброскоков
Priority to SU4765057/23A priority Critical patent/SU1637169A1/en
Application granted granted Critical
Publication of SU1637169A1 publication Critical patent/SU1637169A1/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
    • Y02T50/40Weight reduction

Landscapes

  • Insulators (AREA)

Abstract

FIELD: aircraft engineering. SUBSTANCE: cowling flaps are interconnected through edging section 8 and bushings 9. Heads of bushings 9 are positioned in counterbores 13 provided in shelves of section 8 and skins and are in contact with faces of carbon fibres 10 resulting in discharging to the section and, from it, to pylon through a cross-piece. EFFECT: simplified design and enhanced reliability. 5 dwg
SU4765057/23A 1989-12-05 1989-12-05 Cowling flap for aircraft SU1637169A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4765057/23A SU1637169A1 (en) 1989-12-05 1989-12-05 Cowling flap for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4765057/23A SU1637169A1 (en) 1989-12-05 1989-12-05 Cowling flap for aircraft

Publications (1)

Publication Number Publication Date
SU1637169A1 true SU1637169A1 (en) 1994-12-15

Family

ID=60531738

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4765057/23A SU1637169A1 (en) 1989-12-05 1989-12-05 Cowling flap for aircraft

Country Status (1)

Country Link
SU (1) SU1637169A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2469922C2 (en) * 2007-08-20 2012-12-20 Эрсель Turbojet nacelle with dampers for side covers
RU2471678C2 (en) * 2007-08-20 2013-01-10 Эрсель Connecting device for connecting mutually movable first and second elements

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2469922C2 (en) * 2007-08-20 2012-12-20 Эрсель Turbojet nacelle with dampers for side covers
RU2471678C2 (en) * 2007-08-20 2013-01-10 Эрсель Connecting device for connecting mutually movable first and second elements

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