UA12317A - Фюзеляж літака - Google Patents

Фюзеляж літака

Info

Publication number
UA12317A
UA12317A UA4830507A UA4830507A UA12317A UA 12317 A UA12317 A UA 12317A UA 4830507 A UA4830507 A UA 4830507A UA 4830507 A UA4830507 A UA 4830507A UA 12317 A UA12317 A UA 12317A
Authority
UA
Ukraine
Prior art keywords
fuselage
floor
cab
symmetry
established
Prior art date
Application number
UA4830507A
Other languages
English (en)
Russian (ru)
Inventor
Рьодер Жан
Редер Жан
Джеймс Жерінг Леслі
Original Assignee
Ербюс Ендюстрі
Эрбюс Эндюстри
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 Ербюс Ендюстрі, Эрбюс Эндюстри filed Critical Ербюс Ендюстрі
Publication of UA12317A publication Critical patent/UA12317A/uk

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
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/061—Frames
    • 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
    • B64C1/064—Stringers; Longerons
    • 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
    • B64C1/10—Bulkheads
    • 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
    • B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
    • B64C2001/0027—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged one above the other
    • 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
    • B64C2001/0018—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only
    • B64C2001/0036—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like comprising two decks adapted for carrying passengers only arranged side by side at the same level

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Automatic Assembly (AREA)
  • Tires In General (AREA)

Abstract

Фюзеляж літака містить центральну частину, розташовану перед перегородкою наддування і виконану у вигляді двох долей, що мають шпангоути і сполучених між собою з утворенням верхнього і нижнього стиків, розташованих у вертикальній площині симетрії фюзеляжу, підлога кабіни, підлога вантажного відсіку, засоби кріплення підлоги кабіни, опори, встановлені на підлозі кабіни. Бічний люк вантажного відсіку, порівнянний з розмірами вантажного контейнера і розташований з протилежного боку від дверей кабіни, і розділені на групи, ряди крісел. Засоби кріплення і опори розташовані у вертикальній площині симетрії фюзеляжу. Фюзеляж забезпечений верхньою і нижньою підсилюючими балками встановленими відповідно над верхнім і під нижнім подовжніми стиками, опори сполучені з верхньою підсилюючою балкою і виконані у вигляді стійок, встановлених з кроком кратним 1-4 крокам шпангоутів. Пол кабіни розташований під горизонтальною площиною симетрії фюзеляжу.
UA4830507A 1989-07-12 1990-07-11 Фюзеляж літака UA12317A (uk)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8909397A FR2649665B1 (fr) 1989-07-12 1989-07-12 Fuselage de grande capacite pour avion

Publications (1)

Publication Number Publication Date
UA12317A true UA12317A (uk) 1996-12-25

Family

ID=9383727

Family Applications (1)

Application Number Title Priority Date Filing Date
UA4830507A UA12317A (uk) 1989-07-12 1990-07-11 Фюзеляж літака

Country Status (6)

Country Link
US (1) US5086996A (uk)
EP (1) EP0408432A1 (uk)
CA (1) CA2020932C (uk)
FR (1) FR2649665B1 (uk)
RU (1) RU1828445C (uk)
UA (1) UA12317A (uk)

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Also Published As

Publication number Publication date
FR2649665A1 (fr) 1991-01-18
RU1828445C (ru) 1993-07-15
CA2020932C (en) 2002-02-26
CA2020932A1 (en) 1991-01-13
EP0408432A1 (fr) 1991-01-16
US5086996A (en) 1992-02-11
FR2649665B1 (fr) 1991-11-08

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