SU1099538A1 - Device for mounting engine pylon on wing - Google Patents
Device for mounting engine pylon on wingInfo
- Publication number
- SU1099538A1 SU1099538A1 SU3405665/23A SU3405665A SU1099538A1 SU 1099538 A1 SU1099538 A1 SU 1099538A1 SU 3405665/23 A SU3405665/23 A SU 3405665/23A SU 3405665 A SU3405665 A SU 3405665A SU 1099538 A1 SU1099538 A1 SU 1099538A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- mounting unit
- rear mounting
- wing
- secured
- pylon beam
- 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
- Vehicle Body Suspensions (AREA)
Abstract
FIELD: aeronautical engineering. SUBSTANCE: device has front and rear mounting units. Rear mounting unit has axle rigidly secured on end diaphragm of pylon beam and articulated with bracket secured on wing. Provision is made for avoidance of secondary torque caused by crosswind force at rear mounting unit, axle of rear mounting unit is secured in center of rigidity of end section of pylon beam. EFFECT: reduction of mass of airframe due to reduction of forces in pylon beam and front mounting unit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3405665/23A SU1099538A1 (en) | 1982-03-10 | 1982-03-10 | Device for mounting engine pylon on wing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3405665/23A SU1099538A1 (en) | 1982-03-10 | 1982-03-10 | Device for mounting engine pylon on wing |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1099538A1 true SU1099538A1 (en) | 1996-10-20 |
Family
ID=60524455
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3405665/23A SU1099538A1 (en) | 1982-03-10 | 1982-03-10 | Device for mounting engine pylon on wing |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1099538A1 (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7963479B2 (en) * | 2004-11-23 | 2011-06-21 | Airbus France | Method for fixing an engine strut to an airplane wing |
RU2571680C2 (en) * | 2009-07-28 | 2015-12-20 | Снекма | Aircraft gas turbine engine mount bar |
GB2577540A (en) * | 2018-09-28 | 2020-04-01 | Airbus Operations Ltd | Joint for connecting aircraft structures |
FR3105968A1 (en) * | 2020-01-07 | 2021-07-09 | Airbus Operations | REAR ATTACHMENT BETWEEN A RIGGING MAST AND A WING OF AN AIRCRAFT |
-
1982
- 1982-03-10 SU SU3405665/23A patent/SU1099538A1/en active
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7963479B2 (en) * | 2004-11-23 | 2011-06-21 | Airbus France | Method for fixing an engine strut to an airplane wing |
RU2571680C2 (en) * | 2009-07-28 | 2015-12-20 | Снекма | Aircraft gas turbine engine mount bar |
GB2577540A (en) * | 2018-09-28 | 2020-04-01 | Airbus Operations Ltd | Joint for connecting aircraft structures |
EP3628594A1 (en) * | 2018-09-28 | 2020-04-01 | Airbus Operations Limited | Joint for connecting aircraft structures |
CN110963054A (en) * | 2018-09-28 | 2020-04-07 | 空中客车营运有限公司 | Joint and aircraft |
US11161618B2 (en) | 2018-09-28 | 2021-11-02 | Airbus Operations Limited | Joint for connecting aircraft structures |
FR3105968A1 (en) * | 2020-01-07 | 2021-07-09 | Airbus Operations | REAR ATTACHMENT BETWEEN A RIGGING MAST AND A WING OF AN AIRCRAFT |
EP3848288A1 (en) | 2020-01-07 | 2021-07-14 | Airbus Operations (S.A.S.) | Rear tie between a mounting strut and a wing of an aircraft |
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