SU1637169A1 - Cowling flap for aircraft - Google Patents
Cowling flap for aircraftInfo
- 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
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
- 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
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)
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 |
-
1989
- 1989-12-05 SU SU4765057/23A patent/SU1637169A1/en active
Cited By (2)
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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REG | Reference to a code of a succession state |
Ref country code: RU Ref legal event code: QB4A Effective date: 20060922 |