SU1826409A1 - Power bay of wing torsion box in zone of attachment of engine pylon - Google Patents
Power bay of wing torsion box in zone of attachment of engine pylonInfo
- Publication number
- SU1826409A1 SU1826409A1 SU4745449/23A SU4745449A SU1826409A1 SU 1826409 A1 SU1826409 A1 SU 1826409A1 SU 4745449/23 A SU4745449/23 A SU 4745449/23A SU 4745449 A SU4745449 A SU 4745449A SU 1826409 A1 SU1826409 A1 SU 1826409A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- tight
- bay
- access hole
- attachment
- zone
- Prior art date
Links
Landscapes
- Body Structure For Vehicles (AREA)
Abstract
FIELD: aeronautical engineering. SUBSTANCE: one of ribs of transversal framework has non-tight access hole with detachable wall forming two inspection ports on opposite side of aperture of this access hole; detachable wall consists of panel with struts; subsequent non-tight rib is provided with aperture-access hole located between load-bearing unit for mounting the engine pylon and other tight access hole in lower panel of bay; engine mounting unit is secured on one of non-tight ribs located diagonally in bay. EFFECT: enhanced reliability due to easy access to pylon attachment unit and to wing load-bearing bay for condition inspection. 6 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4745449/23A SU1826409A1 (en) | 1989-10-05 | 1989-10-05 | Power bay of wing torsion box in zone of attachment of engine pylon |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU4745449/23A SU1826409A1 (en) | 1989-10-05 | 1989-10-05 | Power bay of wing torsion box in zone of attachment of engine pylon |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1826409A1 true SU1826409A1 (en) | 1995-12-27 |
Family
ID=60541086
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU4745449/23A SU1826409A1 (en) | 1989-10-05 | 1989-10-05 | Power bay of wing torsion box in zone of attachment of engine pylon |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1826409A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8398024B2 (en) | 2006-07-13 | 2013-03-19 | Airbus Operations Limited | Wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
RU194817U1 (en) * | 2019-09-12 | 2019-12-24 | Публичное акционерное общество (ПАО) "Туполев" | HATCH COVER ASSEMBLY IN THE CESSON OF THE AIRCRAFT WING AND HATCH PANEL |
-
1989
- 1989-10-05 SU SU4745449/23A patent/SU1826409A1/en active
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8398024B2 (en) | 2006-07-13 | 2013-03-19 | Airbus Operations Limited | Wing cover panel assembly and wing cover panel for an aircraft wing and a method of forming thereof |
RU194817U1 (en) * | 2019-09-12 | 2019-12-24 | Публичное акционерное общество (ПАО) "Туполев" | HATCH COVER ASSEMBLY IN THE CESSON OF THE AIRCRAFT WING AND HATCH PANEL |
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