GB8625263D0 - Carbon fibre fabric band - Google Patents

Carbon fibre fabric band

Info

Publication number
GB8625263D0
GB8625263D0 GB868625263A GB8625263A GB8625263D0 GB 8625263 D0 GB8625263 D0 GB 8625263D0 GB 868625263 A GB868625263 A GB 868625263A GB 8625263 A GB8625263 A GB 8625263A GB 8625263 D0 GB8625263 D0 GB 8625263D0
Authority
GB
United Kingdom
Prior art keywords
band
weft threads
production
threads
carbon fibre
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.)
Withdrawn
Application number
GB868625263A
Other versions
GB2182072A (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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of GB8625263D0 publication Critical patent/GB8625263D0/en
Publication of GB2182072A publication Critical patent/GB2182072A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • D—TEXTILES; PAPER
    • D03—WEAVING
    • D03D—WOVEN FABRICS; METHODS OF WEAVING; LOOMS
    • D03D5/00—Selvedges
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite materials
    • 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
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Woven Fabrics (AREA)
  • Moulding By Coating Moulds (AREA)
  • Laminated Bodies (AREA)
  • Inorganic Fibers (AREA)

Abstract

A carbon fibre fabric band comprises warp and weft threads and is used for the production of protective layers for structural members, or for the production of structural members, subject to a medium having a high temperature and a high flow velocity for example for the production of a nozzle lining for a rocket propulsion unit with a short burning time. The weft threads (3) are in the form of U-shaped individual threads wherein their straight portions (limbs of the "U") are aligned parallel to one another and transversally to the warp threads (2) which take the longitudinal direction (4) of the band. The free ends of the weft threads (3) are all positioned on the same side of the band (5) and the free ends of the weft threads extend from the fabric of the band (5) by a distance at least equal to the width thereof. <IMAGE>
GB08625263A 1985-10-24 1986-10-22 Carbon fibre fabric band and method for its use Withdrawn GB2182072A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853537844 DE3537844A1 (en) 1985-10-24 1985-10-24 CARBON FIBER TAPE AND METHOD FOR ITS PROCESSING

Publications (2)

Publication Number Publication Date
GB8625263D0 true GB8625263D0 (en) 1986-11-26
GB2182072A GB2182072A (en) 1987-05-07

Family

ID=6284355

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08625263A Withdrawn GB2182072A (en) 1985-10-24 1986-10-22 Carbon fibre fabric band and method for its use

Country Status (4)

Country Link
JP (1) JPS62117844A (en)
DE (1) DE3537844A1 (en)
FR (1) FR2591618A1 (en)
GB (1) GB2182072A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10245741B4 (en) * 2002-10-01 2005-10-06 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Discharge nozzle for a solid rocket

Also Published As

Publication number Publication date
FR2591618A1 (en) 1987-06-19
GB2182072A (en) 1987-05-07
JPS62117844A (en) 1987-05-29
DE3537844A1 (en) 1987-04-30

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)