GB366898A - Improvements in or relating to aeroplane bodies - Google Patents

Improvements in or relating to aeroplane bodies

Info

Publication number
GB366898A
GB366898A GB23547/30A GB2354730A GB366898A GB 366898 A GB366898 A GB 366898A GB 23547/30 A GB23547/30 A GB 23547/30A GB 2354730 A GB2354730 A GB 2354730A GB 366898 A GB366898 A GB 366898A
Authority
GB
United Kingdom
Prior art keywords
aeroplane
fuselages
relating
glazed
aug
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
GB23547/30A
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.)
UGO ABATE
Original Assignee
UGO ABATE
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 UGO ABATE filed Critical UGO ABATE
Publication of GB366898A publication Critical patent/GB366898A/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
    • B64C1/32—Severable or jettisonable parts of fuselage facilitating emergency escape

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Superconductors And Manufacturing Methods Therefor (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

366,898. Aeroplane fuselages. ABATE, U. and BONOMI, V., 6, Via Gesu, Milan, Italy. Aug. 6, 1930, No. 23547. Convention date, Aug. 7, 1929. Void [Published under Sect. 91 of the Acts]. [Class 4.] In aeroplane fuselages exit openings are provided at the part where the wings join the fuselages and as shown the front opening is provided with glazed doors B while the rear opening is also provided with glazed doors A. Glazed surfaces C are provided between the underside of the front portion of the wing P and the fuselage.
GB23547/30A 1929-08-07 1930-08-06 Improvements in or relating to aeroplane bodies Expired GB366898A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT366898X 1929-08-07

Publications (1)

Publication Number Publication Date
GB366898A true GB366898A (en) 1932-02-11

Family

ID=11245799

Family Applications (1)

Application Number Title Priority Date Filing Date
GB23547/30A Expired GB366898A (en) 1929-08-07 1930-08-06 Improvements in or relating to aeroplane bodies

Country Status (1)

Country Link
GB (1) GB366898A (en)

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