FR2316058A1 - Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure - Google Patents

Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure

Info

Publication number
FR2316058A1
FR2316058A1 FR7520449A FR7520449A FR2316058A1 FR 2316058 A1 FR2316058 A1 FR 2316058A1 FR 7520449 A FR7520449 A FR 7520449A FR 7520449 A FR7520449 A FR 7520449A FR 2316058 A1 FR2316058 A1 FR 2316058A1
Authority
FR
France
Prior art keywords
lining
flexible tube
aircraft
transferring
pressure
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.)
Granted
Application number
FR7520449A
Other languages
French (fr)
Other versions
FR2316058B1 (en
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.)
Tecalemit Flexibles SA
Original Assignee
Tecalemit Flexibles SA
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 Tecalemit Flexibles SA filed Critical Tecalemit Flexibles SA
Priority to FR7520449A priority Critical patent/FR2316058A1/en
Publication of FR2316058A1 publication Critical patent/FR2316058A1/en
Application granted granted Critical
Publication of FR2316058B1 publication Critical patent/FR2316058B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16L—PIPES; JOINTS OR FITTINGS FOR PIPES; SUPPORTS FOR PIPES, CABLES OR PROTECTIVE TUBING; MEANS FOR THERMAL INSULATION IN GENERAL
    • F16L11/00—Hoses, i.e. flexible pipes
    • F16L11/04—Hoses, i.e. flexible pipes made of rubber or flexible plastics
    • F16L11/12—Hoses, i.e. flexible pipes made of rubber or flexible plastics with arrangements for particular purposes, e.g. specially profiled, with protecting layer, heated, electrically conducting
    • F16L11/127—Hoses, i.e. flexible pipes made of rubber or flexible plastics with arrangements for particular purposes, e.g. specially profiled, with protecting layer, heated, electrically conducting electrically conducting

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)

Abstract

A flexible tube with a conductive inner lining is produced by forming a conductive coating on the outer surface of a mandrel. This is then inserted into a thermoplastic tube of which the dimensions have already been checked, and heat and pressure applied so that the conductive coating bonds to the inner surface of the tube, finally the mandrel is removed. The flexible tube is used in the aeronautics industry. The dimensions of the tube are accurate.
FR7520449A 1975-06-30 1975-06-30 Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure Granted FR2316058A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR7520449A FR2316058A1 (en) 1975-06-30 1975-06-30 Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7520449A FR2316058A1 (en) 1975-06-30 1975-06-30 Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure

Publications (2)

Publication Number Publication Date
FR2316058A1 true FR2316058A1 (en) 1977-01-28
FR2316058B1 FR2316058B1 (en) 1977-12-02

Family

ID=9157262

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7520449A Granted FR2316058A1 (en) 1975-06-30 1975-06-30 Flexible tube for aircraft having inner conductive lining - formed by transferring lining from a mandrel under heat and pressure

Country Status (1)

Country Link
FR (1) FR2316058A1 (en)

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
NEANT *

Also Published As

Publication number Publication date
FR2316058B1 (en) 1977-12-02

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Legal Events

Date Code Title Description
ST Notification of lapse