FR1084809A - Noyaux d'armature en métal destinés à former l'intérieur de panneaux rigides - Google Patents

Noyaux d'armature en métal destinés à former l'intérieur de panneaux rigides

Info

Publication number
FR1084809A
FR1084809A FR1084809DA FR1084809A FR 1084809 A FR1084809 A FR 1084809A FR 1084809D A FR1084809D A FR 1084809DA FR 1084809 A FR1084809 A FR 1084809A
Authority
FR
France
Prior art keywords
interior
forming
metal reinforcing
rigid panels
reinforcing cores
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.)
Expired
Application number
Other languages
English (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.)
AV Roe and Co Ltd
Original Assignee
AV Roe and Co Ltd
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 AV Roe and Co Ltd filed Critical AV Roe and Co Ltd
Application granted granted Critical
Publication of FR1084809A publication Critical patent/FR1084809A/fr
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • 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
FR1084809D 1952-12-12 1953-10-08 Noyaux d'armature en métal destinés à former l'intérieur de panneaux rigides Expired FR1084809A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1084809X 1952-12-12

Publications (1)

Publication Number Publication Date
FR1084809A true FR1084809A (fr) 1955-01-24

Family

ID=10872893

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1084809D Expired FR1084809A (fr) 1952-12-12 1953-10-08 Noyaux d'armature en métal destinés à former l'intérieur de panneaux rigides

Country Status (1)

Country Link
FR (1) FR1084809A (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214091B (de) * 1962-06-14 1966-04-07 Aviation Louis Breguet Sa Unter inneren UEberdruck setzbarer Luftfahrzeugrumpf
US4228943A (en) * 1976-12-28 1980-10-21 Shinko-Pfaudler Company, Ltd. Device for separating suspended material from a fluid stream by specific gravity difference
US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1214091B (de) * 1962-06-14 1966-04-07 Aviation Louis Breguet Sa Unter inneren UEberdruck setzbarer Luftfahrzeugrumpf
US4228943A (en) * 1976-12-28 1980-10-21 Shinko-Pfaudler Company, Ltd. Device for separating suspended material from a fluid stream by specific gravity difference
US4642993A (en) * 1985-04-29 1987-02-17 Avco Corporation Combustor liner wall

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