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SU1683269A1 - Device for connecting fin with fuselage of flying vehicle - Google Patents

Device for connecting fin with fuselage of flying vehicle

Info

Publication number
SU1683269A1
SU1683269A1 SU4488721/23A SU4488721A SU1683269A1 SU 1683269 A1 SU1683269 A1 SU 1683269A1 SU 4488721/23 A SU4488721/23 A SU 4488721/23A SU 4488721 A SU4488721 A SU 4488721A SU 1683269 A1 SU1683269 A1 SU 1683269A1
Authority
SU
USSR - Soviet Union
Prior art keywords
fuselage
flying vehicle
stringer
shoe
angle
Prior art date
Application number
SU4488721/23A
Other languages
Russian (ru)
Inventor
Б.А. Волков
Original Assignee
Б.А. Волков
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 Б.А. Волков filed Critical Б.А. Волков
Priority to SU4488721/23A priority Critical patent/SU1683269A1/en
Application granted granted Critical
Publication of SU1683269A1 publication Critical patent/SU1683269A1/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Support Of The Bearing (AREA)

Abstract

FIELD: manufacture of aircraft. SUBSTANCE: longitudinal load-bearing shapes are made in form of angle 5 located outside the fuselage according to contour of fin and stringer 6 pressed to ear of bracket; fitted in between them in shoe 7 whose thrust surface is engageable with flat surface of bracket projecting above fuselage. Shoe is connected with angle 5 and stringer 6 by means of bolts 8. EFFECT: simplified construction and assembly and reduced mass. 4 dwg
SU4488721/23A 1988-10-30 1988-10-30 Device for connecting fin with fuselage of flying vehicle SU1683269A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU4488721/23A SU1683269A1 (en) 1988-10-30 1988-10-30 Device for connecting fin with fuselage of flying vehicle

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU4488721/23A SU1683269A1 (en) 1988-10-30 1988-10-30 Device for connecting fin with fuselage of flying vehicle

Publications (1)

Publication Number Publication Date
SU1683269A1 true SU1683269A1 (en) 1995-02-27

Family

ID=60520196

Family Applications (1)

Application Number Title Priority Date Filing Date
SU4488721/23A SU1683269A1 (en) 1988-10-30 1988-10-30 Device for connecting fin with fuselage of flying vehicle

Country Status (1)

Country Link
SU (1) SU1683269A1 (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7931234B2 (en) 2005-08-17 2011-04-26 Airbus Deutschland Gmbh Continuous fuselage connection
US8104709B2 (en) 2005-07-26 2012-01-31 Airbus Deutschland Gmbh Lateral force joint
RU2446986C2 (en) * 2006-10-03 2012-04-10 Эйрбас Оперейшнз Лимитед Connection element
ES2378702A1 (en) * 2009-04-21 2012-04-17 Airbus Operations, S.L. Metal fittings for engaging the vertical tailplane of an aircraft
ES2400769A1 (en) * 2010-10-19 2013-04-12 Airbus Operations, S.L. Hermetic fitting for holding the vertical stabiliser of the tail unit of an aircraft
CN115258036A (en) * 2022-08-11 2022-11-01 上海外高桥造船有限公司 Hoisting rib structure and ship body

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8104709B2 (en) 2005-07-26 2012-01-31 Airbus Deutschland Gmbh Lateral force joint
US7931234B2 (en) 2005-08-17 2011-04-26 Airbus Deutschland Gmbh Continuous fuselage connection
RU2446986C2 (en) * 2006-10-03 2012-04-10 Эйрбас Оперейшнз Лимитед Connection element
ES2378702A1 (en) * 2009-04-21 2012-04-17 Airbus Operations, S.L. Metal fittings for engaging the vertical tailplane of an aircraft
RU2524803C2 (en) * 2009-04-21 2014-08-10 Эйрбас Оперейшнз, С.Л. Aircraft tail unit attachment connectors
ES2400769A1 (en) * 2010-10-19 2013-04-12 Airbus Operations, S.L. Hermetic fitting for holding the vertical stabiliser of the tail unit of an aircraft
CN115258036A (en) * 2022-08-11 2022-11-01 上海外高桥造船有限公司 Hoisting rib structure and ship body
CN115258036B (en) * 2022-08-11 2024-04-16 上海外高桥造船有限公司 Hoisting rib structure and hull

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