GB226558A - Improvements in and connected with aeroplane flying machines - Google Patents

Improvements in and connected with aeroplane flying machines

Info

Publication number
GB226558A
GB226558A GB30594/24A GB3059424A GB226558A GB 226558 A GB226558 A GB 226558A GB 30594/24 A GB30594/24 A GB 30594/24A GB 3059424 A GB3059424 A GB 3059424A GB 226558 A GB226558 A GB 226558A
Authority
GB
United Kingdom
Prior art keywords
planes
arrangement
forming
central
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
GB30594/24A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of GB226558A publication Critical patent/GB226558A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Tents Or Canopies (AREA)
  • Toys (AREA)

Abstract

226,558. Mattioni, A. Dec. 22, 1923, [Convention date]. Void [Published under Sect. 91 of the Act]. Aeroplanes; planes, arrangement and construction of; propelling; steering and balancing; cabins; wind deflecting screens, arrangement of. -An aeroplane comprises a central cylindrical, octagonal or hexagonal body a forming a supporting-surface and having laterally extending planes c shaped as shown in Fig. 4. The wings c may be folded along hinges s. An engine r drives a propellor q which is of smaller diameter than the central body and is arranged just at the entrance thereto. A fin k at the upper forward part of the body has divergent rear extensions l forming a protective screen for a pilot's cockpit m. Lateral openings b are formed in the body beneath the planes c. Ailerons h, hinged along their inner edges g, elevators o, and a rudder i are provided. The machine may be constructed as a biplane, and land wheels or floats may be fitted.
GB30594/24A 1923-12-22 1924-12-19 Improvements in and connected with aeroplane flying machines Expired GB226558A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT226558X 1923-12-22

Publications (1)

Publication Number Publication Date
GB226558A true GB226558A (en) 1925-08-20

Family

ID=11198918

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30594/24A Expired GB226558A (en) 1923-12-22 1924-12-19 Improvements in and connected with aeroplane flying machines

Country Status (1)

Country Link
GB (1) GB226558A (en)

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