SU1376424A1 - Fuselage-to-center section joint of flying vehicle - Google Patents

Fuselage-to-center section joint of flying vehicle

Info

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
Application number
SU3976230/23A
Other languages
Russian (ru)
Inventor
Г.Г. Демьяненко
Е.А. Тимофеев
Б.М. Львовский
Original Assignee
Г.Г. Демьяненко
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 Г.Г. Демьяненко filed Critical Г.Г. Демьяненко
Priority to SU3976230/23A priority Critical patent/SU1376424A1/en
Application granted granted Critical
Publication of SU1376424A1 publication Critical patent/SU1376424A1/en

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  • 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
SU3976230/23A 1985-11-19 1985-11-19 Fuselage-to-center section joint of flying vehicle SU1376424A1 (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (5)

* Cited by examiner, † Cited by third party
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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