FR2202809B1 - - Google Patents

Info

Publication number
FR2202809B1
FR2202809B1 FR7236756A FR7236756A FR2202809B1 FR 2202809 B1 FR2202809 B1 FR 2202809B1 FR 7236756 A FR7236756 A FR 7236756A FR 7236756 A FR7236756 A FR 7236756A FR 2202809 B1 FR2202809 B1 FR 2202809B1
Authority
FR
France
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
FR7236756A
Other languages
French (fr)
Other versions
FR2202809A1 (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.)
NALE INDLE AEROSPATI FR SOC
Original Assignee
NALE INDLE AEROSPATI FR SOC
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 NALE INDLE AEROSPATI FR SOC filed Critical NALE INDLE AEROSPATI FR SOC
Priority to FR7236756A priority Critical patent/FR2202809A1/fr
Priority to US406840A priority patent/US3910531A/en
Publication of FR2202809A1 publication Critical patent/FR2202809A1/fr
Application granted granted Critical
Publication of FR2202809B1 publication Critical patent/FR2202809B1/fr
Granted 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
    • B64C2001/0072—Fuselage structures substantially made from particular materials from composite 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
FR7236756A 1972-10-17 1972-10-17 Light aircraft sandwich structure - coated with resin impregnated reinforcing fabric Granted FR2202809A1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR7236756A FR2202809A1 (en) 1972-10-17 1972-10-17 Light aircraft sandwich structure - coated with resin impregnated reinforcing fabric
US406840A US3910531A (en) 1972-10-17 1973-10-16 Shell-type structure for light aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7236756A FR2202809A1 (en) 1972-10-17 1972-10-17 Light aircraft sandwich structure - coated with resin impregnated reinforcing fabric

Publications (2)

Publication Number Publication Date
FR2202809A1 FR2202809A1 (en) 1974-05-10
FR2202809B1 true FR2202809B1 (es) 1976-01-30

Family

ID=9105775

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7236756A Granted FR2202809A1 (en) 1972-10-17 1972-10-17 Light aircraft sandwich structure - coated with resin impregnated reinforcing fabric

Country Status (1)

Country Link
FR (1) FR2202809A1 (es)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4113910A (en) * 1977-04-27 1978-09-12 Rockwell International Corporation Composite load coupler for reinforcing composite structural joints
DE3826636A1 (de) * 1988-08-05 1990-02-08 Messerschmitt Boelkow Blohm Cockpit, insbesondere fuer einen hubschrauber
IT1282005B1 (it) * 1996-02-06 1998-03-06 Fiocco Engineering Di Luigino Aeromobile ultraleggero e procedimento per la fabbricazione dello stesso
GB9817778D0 (en) 1998-08-15 1998-10-14 British Aerospace A method of constructing skin for a member of a body such as an aircraft
EP1918193A1 (en) * 2006-10-31 2008-05-07 Airbus Espana, S.L. Integrated composite skin for aircraft mid-box lifting surfaces
FR3138476A1 (fr) 2022-07-27 2024-02-02 Renault S.A.S Procédé de contrôle de l’injection de carburant dans un moteur à combustion interne et système associé

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB604752A (en) * 1943-06-23 1948-07-09 Bendix Aviat Corp Improvements in composite panels and wall structures
NL80316C (es) * 1949-03-16
US3578526A (en) * 1968-01-22 1971-05-11 United Aircraft Corp Method of making reinforced honeycomb sandwich

Also Published As

Publication number Publication date
FR2202809A1 (en) 1974-05-10

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Legal Events

Date Code Title Description
ST Notification of lapse