CA2820016C - Dispositif de couplage - Google Patents

Dispositif de couplage Download PDF

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Publication number
CA2820016C
CA2820016C CA2820016A CA2820016A CA2820016C CA 2820016 C CA2820016 C CA 2820016C CA 2820016 A CA2820016 A CA 2820016A CA 2820016 A CA2820016 A CA 2820016A CA 2820016 C CA2820016 C CA 2820016C
Authority
CA
Canada
Prior art keywords
coupling device
jackets
outer shell
annular
rib
Prior art date
Legal status (The legal status 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 status listed.)
Active
Application number
CA2820016A
Other languages
English (en)
Other versions
CA2820016A1 (fr
Inventor
Juergen Hartmann
Andreas Kaufmann
Stefan Gelbrich
Caroline Kauffmann
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
PFW Aerospace GmbH
Original Assignee
PFW Aerospace GmbH
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
Priority claimed from EP12005017.4A external-priority patent/EP2682659B1/fr
Priority claimed from US13/542,989 external-priority patent/US9611959B2/en
Application filed by PFW Aerospace GmbH filed Critical PFW Aerospace GmbH
Publication of CA2820016A1 publication Critical patent/CA2820016A1/fr
Application granted granted Critical
Publication of CA2820016C publication Critical patent/CA2820016C/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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  • Quick-Acting Or Multi-Walled Pipe Joints (AREA)

Abstract

La présente invention porte sur le dispositif de couplage (18) servant à connecter de manière amovible les extrémités de conduit dun conduit transportant un fluide (10,12). Lesdites extrémités de conduit (10, 12) respectivement portent chacune une chemise (14, 16) comportant au moins deux rainures annulaires (50, 52) logeant un premier élément de joint annulaire (46). Le premier élément de joint annulaire (46) est engagé par lenveloppe interne (22). Le dispositif de couplage (18), conformément à la présente invention, comprend une enveloppe extérieure (20, 66, 68) qui présente des rainures ou des portions de rainures sétendant radialement vers lintérieur (40). Ces rainures sont disposées à une distance axiale par rapport à une autre rainure annulaire (54) desdites chemises (14, 16) ou engagées dans un creux axial (103) fourni sur lesdites chemises (14, 16), défini entre ladite autre rainure annulaire (54) et la quatrième rainure annulaire (102).
CA2820016A 2012-07-06 2013-06-28 Dispositif de couplage Active CA2820016C (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US13/542,989 2012-07-06
EP12005017.4A EP2682659B1 (fr) 2012-07-06 2012-07-06 Dispositif de couplage
US13/542,989 US9611959B2 (en) 2012-07-06 2012-07-06 Coupling device
EP12005017.4 2012-07-06

Publications (2)

Publication Number Publication Date
CA2820016A1 CA2820016A1 (fr) 2014-01-06
CA2820016C true CA2820016C (fr) 2016-11-01

Family

ID=49911920

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2820016A Active CA2820016C (fr) 2012-07-06 2013-06-28 Dispositif de couplage

Country Status (1)

Country Link
CA (1) CA2820016C (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111237083A (zh) * 2018-11-28 2020-06-05 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111237083A (zh) * 2018-11-28 2020-06-05 海鹰航空通用装备有限责任公司 组合喷管结构及具有其的飞机

Also Published As

Publication number Publication date
CA2820016A1 (fr) 2014-01-06

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