FR856669A - Airplane hull - Google Patents

Airplane hull

Info

Publication number
FR856669A
FR856669A FR856669DA FR856669A FR 856669 A FR856669 A FR 856669A FR 856669D A FR856669D A FR 856669DA FR 856669 A FR856669 A FR 856669A
Authority
FR
France
Prior art keywords
airplane
hull
airplane hull
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
French (fr)
Inventor
Claude Dornier
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.)
Dornier Werke GmbH
Original Assignee
Dornier Werke GmbH
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 Dornier Werke GmbH filed Critical Dornier Werke GmbH
Application granted granted Critical
Publication of FR856669A publication Critical patent/FR856669A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061Frames
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/10Bulkheads
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0018Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
    • B64C2001/0027Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
FR856669D 1938-08-26 1939-06-20 Airplane hull Expired FR856669A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE856669X 1938-08-26

Publications (1)

Publication Number Publication Date
FR856669A true FR856669A (en) 1940-08-01

Family

ID=6789381

Family Applications (1)

Application Number Title Priority Date Filing Date
FR856669D Expired FR856669A (en) 1938-08-26 1939-06-20 Airplane hull

Country Status (1)

Country Link
FR (1) FR856669A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2693976A1 (en) * 1992-07-22 1994-01-28 Eurocopter France Helicopter fuselage structure.
US5893535A (en) * 1997-06-19 1999-04-13 Mcdonnell Douglas Corporation Rib for blended wing-body aircraft

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2693976A1 (en) * 1992-07-22 1994-01-28 Eurocopter France Helicopter fuselage structure.
EP0581626A1 (en) * 1992-07-22 1994-02-02 EUROCOPTER FRANCE, Société Anonyme dite: Helicopter fuselage structure
US5893535A (en) * 1997-06-19 1999-04-13 Mcdonnell Douglas Corporation Rib for blended wing-body aircraft

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