SU701204A1 - Pipe line joint for aircraft - Google Patents

Pipe line joint for aircraft

Info

Publication number
SU701204A1
SU701204A1 SU2609969/23A SU2609969A SU701204A1 SU 701204 A1 SU701204 A1 SU 701204A1 SU 2609969/23 A SU2609969/23 A SU 2609969/23A SU 2609969 A SU2609969 A SU 2609969A SU 701204 A1 SU701204 A1 SU 701204A1
Authority
SU
USSR - Soviet Union
Prior art keywords
flanges
rings
contact
pipe line
aircraft
Prior art date
Application number
SU2609969/23A
Other languages
Russian (ru)
Inventor
А.С. Гришанов
А.Л. Матвеев
В.А. Павлюченко
В.Г. Пильтенко
В.А. Привалихин
Original Assignee
А.С. Гришанов
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 А.С. Гришанов filed Critical А.С. Гришанов
Priority to SU2609969/23A priority Critical patent/SU701204A1/en
Application granted granted Critical
Publication of SU701204A1 publication Critical patent/SU701204A1/en

Links

Landscapes

  • Flanged Joints, Insulating Joints, And Other Joints (AREA)
  • Clamps And Clips (AREA)

Abstract

FIELD: aircraft engineering. SUBSTANCE: pipe lines with flanges 1 and 2 and rings 6 and 7 are mounted so that ends 5 of the flanges are in a contact. The belt and races 14 mounted on it are tightened with a tightening device. Sides 15 of the races effect on side inclined walls of locking rings 6 and 7 and, through them, on U-shaped ends of flanges 1 and 2. Ends 5 of the flanges in so doing begins to be deformed and angle between them decreases. The tightening stops when rings 6 and 7 are in contact. Further tightening is impossible in practice. Ends 5 of the flanges is in a tight contact with each other. If a pipe line is under pressure the tightness of the joint is enhanced due to the action of the pressure on flexible ends 5 of flanges 1 and 2 that it presses them to each other. It is possible to join pipe lines that are out of alignment without any stresses in the flanges. EFFECT: enhanced reliability. cl, dwg
SU2609969/23A 1978-05-03 1978-05-03 Pipe line joint for aircraft SU701204A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU2609969/23A SU701204A1 (en) 1978-05-03 1978-05-03 Pipe line joint for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU2609969/23A SU701204A1 (en) 1978-05-03 1978-05-03 Pipe line joint for aircraft

Publications (1)

Publication Number Publication Date
SU701204A1 true SU701204A1 (en) 1996-10-27

Family

ID=60518325

Family Applications (1)

Application Number Title Priority Date Filing Date
SU2609969/23A SU701204A1 (en) 1978-05-03 1978-05-03 Pipe line joint for aircraft

Country Status (1)

Country Link
SU (1) SU701204A1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2495316C2 (en) * 2011-01-22 2013-10-10 НОРМА Германи ГмбХ Connection device and its manufacturing method
RU2636597C2 (en) * 2012-04-11 2017-11-24 Снекма Turbomachine, such as aviation turbojet engine or turboprop engine

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2495316C2 (en) * 2011-01-22 2013-10-10 НОРМА Германи ГмбХ Connection device and its manufacturing method
RU2636597C2 (en) * 2012-04-11 2017-11-24 Снекма Turbomachine, such as aviation turbojet engine or turboprop engine
US10190430B2 (en) 2012-04-11 2019-01-29 Safran Aircraft Engines Turbine engine, such as a turbojet or a turboprop engine

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