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GB329615A - Improvements in aeroplane fuselage construction - Google Patents

Improvements in aeroplane fuselage construction

Info

Publication number
GB329615A
GB329615A GB5969/30A GB596930A GB329615A GB 329615 A GB329615 A GB 329615A GB 5969/30 A GB5969/30 A GB 5969/30A GB 596930 A GB596930 A GB 596930A GB 329615 A GB329615 A GB 329615A
Authority
GB
United Kingdom
Prior art keywords
members
bulkheads
fuselage construction
aeroplane fuselage
aeroplane
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
GB5969/30A
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.)
VINCENT JUSTINE BURNELLI
Original Assignee
VINCENT JUSTINE BURNELLI
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 VINCENT JUSTINE BURNELLI filed Critical VINCENT JUSTINE BURNELLI
Publication of GB329615A publication Critical patent/GB329615A/en
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
    • B64C1/10—Bulkheads

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Sheets, Magazines, And Separation Thereof (AREA)
  • Catching Or Destruction (AREA)

Abstract

329,615. Burnelli, V. J. Feb. 4. 1929, [Convention date]. Divided on 329,489. Fuselages.-An aerofoil section fuselage has main longerons 1, 2 and bulkheads 9, 10, 13, 14, 15, 16, longitudinal compression members 37 being arranged betwem the bulkheads 9, 10 and 13 intersected by vertical members 38 and braced by members 39, 40, to enable window openings 41 to be inserted as clear of obstruction as possible. Specification 329,489 is referred to.
GB5969/30A 1929-02-04 1929-05-01 Improvements in aeroplane fuselage construction Expired GB329615A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US329615XA 1929-02-04 1929-02-04

Publications (1)

Publication Number Publication Date
GB329615A true GB329615A (en) 1930-05-22

Family

ID=21867812

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5969/30A Expired GB329615A (en) 1929-02-04 1929-05-01 Improvements in aeroplane fuselage construction

Country Status (1)

Country Link
GB (1) GB329615A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014113464A1 (en) * 2013-01-16 2014-07-24 Otto William M Aircraft fuselage
US9446835B2 (en) 2013-01-16 2016-09-20 Otto Aviation Group Aircraft wing
US9669939B2 (en) 2013-01-16 2017-06-06 Otto Aviation Group Aircraft supplemental thrust device and method of operating the same

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014113464A1 (en) * 2013-01-16 2014-07-24 Otto William M Aircraft fuselage
US9090324B2 (en) 2013-01-16 2015-07-28 Ottoa Aviation Group Aircraft support structure
US9308989B2 (en) 2013-01-16 2016-04-12 Otto Aviation Group Aircraft front landing gear and method of operating the same
US9308988B2 (en) 2013-01-16 2016-04-12 Otto Aviation Group Aircraft main landing gear and method of operating the same
US9446835B2 (en) 2013-01-16 2016-09-20 Otto Aviation Group Aircraft wing
US9533755B2 (en) 2013-01-16 2017-01-03 Otto Aviation Group Aircraft fuselage
US9669939B2 (en) 2013-01-16 2017-06-06 Otto Aviation Group Aircraft supplemental thrust device and method of operating the same

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