SU1376424A1 - Fuselage-to-center section joint of flying vehicle - Google Patents
Fuselage-to-center section joint of flying vehicleInfo
- Publication number
- SU1376424A1 SU1376424A1 SU3976230/23A SU3976230A SU1376424A1 SU 1376424 A1 SU1376424 A1 SU 1376424A1 SU 3976230/23 A SU3976230/23 A SU 3976230/23A SU 3976230 A SU3976230 A SU 3976230A SU 1376424 A1 SU1376424 A1 SU 1376424A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- fuselage
- load
- center section
- section joint
- bearing members
- Prior art date
Links
Landscapes
- Body Structure For Vehicles (AREA)
Abstract
FIELD: manufacture of aircraft. SUBSTANCE: fuselage-to-center section joint has skin 1, longitudinal load-bearing members 2 of fuselage between which spars 3 and ribs 4 of center plane and additional load- bearing longitudinal members 5 are arranged. Skin 1 and load- bearing members 2 of fuselage are secured on spars 3. Additional longitudinal load-bearing members 5 are mounted inside center plane on ribs 4 and are secured on spars 3 in line with longitudinal load-bearing members 2 of fuselage. EFFECT: simplified construction, reduction of labour consumption and mass. 4 dwg
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3976230/23A SU1376424A1 (en) | 1985-11-19 | 1985-11-19 | Fuselage-to-center section joint of flying vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU3976230/23A SU1376424A1 (en) | 1985-11-19 | 1985-11-19 | Fuselage-to-center section joint of flying vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
SU1376424A1 true SU1376424A1 (en) | 1995-10-27 |
Family
ID=60533776
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU3976230/23A SU1376424A1 (en) | 1985-11-19 | 1985-11-19 | Fuselage-to-center section joint of flying vehicle |
Country Status (1)
Country | Link |
---|---|
SU (1) | SU1376424A1 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008105805A2 (en) * | 2006-09-15 | 2008-09-04 | The Boeing Company | Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
RU2564561C2 (en) * | 2010-12-15 | 2015-10-10 | Дзе Боинг Компани | Butt strap and fuselage compartments connection process related therewith |
-
1985
- 1985-11-19 SU SU3976230/23A patent/SU1376424A1/en active
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2008105805A2 (en) * | 2006-09-15 | 2008-09-04 | The Boeing Company | Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
WO2008105805A3 (en) * | 2006-09-15 | 2009-01-15 | Boeing Co | Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
US7546979B1 (en) | 2006-09-15 | 2009-06-16 | The Boeing Company | Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
CN101516726B (en) * | 2006-09-15 | 2011-11-09 | 波音公司 | Trapezoidal panel pin joint allowing free deflection between fuselage and wing |
RU2564561C2 (en) * | 2010-12-15 | 2015-10-10 | Дзе Боинг Компани | Butt strap and fuselage compartments connection process related therewith |
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