FR2239381B2 - - Google Patents

Info

Publication number
FR2239381B2
FR2239381B2 FR7328582A FR7328582A FR2239381B2 FR 2239381 B2 FR2239381 B2 FR 2239381B2 FR 7328582 A FR7328582 A FR 7328582A FR 7328582 A FR7328582 A FR 7328582A FR 2239381 B2 FR2239381 B2 FR 2239381B2
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
FR7328582A
Other languages
French (fr)
Other versions
FR2239381A2 (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 Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Priority to FR7328582A priority Critical patent/FR2239381A2/en
Priority to US406840A priority patent/US3910531A/en
Publication of FR2239381A2 publication Critical patent/FR2239381A2/en
Application granted granted Critical
Publication of FR2239381B2 publication Critical patent/FR2239381B2/fr
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/24—Moulded or cast structures
FR7328582A 1972-10-17 1973-08-03 Lightweight plane aerofoil section has upper and lower walls - with tabs secured in moulded edging piece at leading edge Granted FR2239381A2 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR7328582A FR2239381A2 (en) 1973-08-03 1973-08-03 Lightweight plane aerofoil section has upper and lower walls - with tabs secured in moulded edging piece at leading edge
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
FR7328582A FR2239381A2 (en) 1973-08-03 1973-08-03 Lightweight plane aerofoil section has upper and lower walls - with tabs secured in moulded edging piece at leading edge

Publications (2)

Publication Number Publication Date
FR2239381A2 FR2239381A2 (en) 1975-02-28
FR2239381B2 true FR2239381B2 (en) 1976-11-12

Family

ID=9123585

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7328582A Granted FR2239381A2 (en) 1972-10-17 1973-08-03 Lightweight plane aerofoil section has upper and lower walls - with tabs secured in moulded edging piece at leading edge

Country Status (1)

Country Link
FR (1) FR2239381A2 (en)

Families Citing this family (2)

* 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
US4448372A (en) * 1981-09-30 1984-05-15 The Boeing Company Aircraft vertical fin-fuselage structural integration system

Also Published As

Publication number Publication date
FR2239381A2 (en) 1975-02-28

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