GB0104727D0 - Method for the production of a liquid-tight chamber in an aircraft construction - Google Patents

Method for the production of a liquid-tight chamber in an aircraft construction

Info

Publication number
GB0104727D0
GB0104727D0 GB0104727A GB0104727A GB0104727D0 GB 0104727 D0 GB0104727 D0 GB 0104727D0 GB 0104727 A GB0104727 A GB 0104727A GB 0104727 A GB0104727 A GB 0104727A GB 0104727 D0 GB0104727 D0 GB 0104727D0
Authority
GB
United Kingdom
Prior art keywords
production
liquid
tight chamber
aircraft construction
aircraft
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Withdrawn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
GB0104727A
Other versions
GB2359604A (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.)
GKN Fokker Aerospace BV
Original Assignee
Fokker Aerostructures BV
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 Fokker Aerostructures BV filed Critical Fokker Aerostructures BV
Publication of GB0104727D0 publication Critical patent/GB0104727D0/en
Publication of GB2359604A publication Critical patent/GB2359604A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/02—Lightning protectors; Static dischargers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D37/00—Arrangements in connection with fuel supply for power plant
    • B64D37/02—Tanks
    • B64D37/06—Constructional adaptations thereof
    • 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
    • F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
    • F16B11/00—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding
    • F16B11/006—Connecting constructional elements or machine parts by sticking or pressing them together, e.g. cold pressure welding by gluing
GB0104727A 2000-02-25 2001-02-26 A method for producing a liquid-tight joint for an aircraft fuel tank Withdrawn GB2359604A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US51227200A 2000-02-25 2000-02-25

Publications (2)

Publication Number Publication Date
GB0104727D0 true GB0104727D0 (en) 2001-04-18
GB2359604A GB2359604A (en) 2001-08-29

Family

ID=24038400

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0104727A Withdrawn GB2359604A (en) 2000-02-25 2001-02-26 A method for producing a liquid-tight joint for an aircraft fuel tank

Country Status (1)

Country Link
GB (1) GB2359604A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109050945A (en) * 2018-10-17 2018-12-21 沈阳橡胶研究设计院有限公司 A kind of aircraft flexible tank adjustable hanging connector and suspension hanging method
CN109050945B (en) * 2018-10-17 2024-04-26 沈阳橡胶研究设计院有限公司 Adjustable suspension connecting piece for aircraft flexible fuel tank and suspension hoisting method

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0906686D0 (en) 2009-04-20 2009-06-03 Airbus Uk Ltd Edge seal for fibre-reinforced composite structure
GB201207511D0 (en) 2012-04-30 2012-06-13 Airbus Operations Ltd Bush assembly
CN104454849B (en) * 2014-11-10 2016-06-22 沈阳黎明航空发动机(集团)有限责任公司 A kind of rubber and space curved surface component glue-joint technique method
CN109421940B (en) * 2017-08-22 2022-01-25 成都飞机工业（集团）有限责任公司 Method for pressing sealing rubber gasket on opening frame of sealed oil tank
CN111085660A (en) * 2018-10-24 2020-05-01 四川特飞科技股份有限公司 Oil tank manufacturing method and small unmanned aerial vehicle oil tank

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB513976A (en) * 1938-08-09 1939-10-26 Glenn L Martin Co Methods of forming a sealed connection between two structural members

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109050945A (en) * 2018-10-17 2018-12-21 沈阳橡胶研究设计院有限公司 A kind of aircraft flexible tank adjustable hanging connector and suspension hanging method
CN109050945B (en) * 2018-10-17 2024-04-26 沈阳橡胶研究设计院有限公司 Adjustable suspension connecting piece for aircraft flexible fuel tank and suspension hoisting method

Also Published As

Publication number Publication date
GB2359604A (en) 2001-08-29

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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)