GB300499A - Improvements in or relating to propelling means for aircraft - Google Patents

Improvements in or relating to propelling means for aircraft

Info

Publication number
GB300499A
GB300499A GB30788/28A GB3078828A GB300499A GB 300499 A GB300499 A GB 300499A GB 30788/28 A GB30788/28 A GB 30788/28A GB 3078828 A GB3078828 A GB 3078828A GB 300499 A GB300499 A GB 300499A
Authority
GB
United Kingdom
Prior art keywords
engines
petrol
cabin
accessible
plane
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
GB30788/28A
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 GB300499A publication Critical patent/GB300499A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C11/00—Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft

Abstract

300,499. Bratu, R. Nov. 12, 1927, [Convention date]. Propelling; cabins; tanks, arrangement and disposition of.-Monoplanes or biplanes are provided with three engines in the vertical plane of symmetry, one at the front of the fuselage, the other two in tandem above the plane 3 or lower plane. The two upper engines are enclosed in a cabin S accessible from the navigating cabin C, from which the engine M is also accessible. The common axis of traction of the upper engines is inclined at an angle of 80‹. Other engines may be symmetrically arranged on both sides of the upper engines. Petrol and oil tanks R may be replaced by seating accommodation. Petrol reservoirs are in any case provided in the central portion of the wing spread.
GB30788/28A 1927-11-12 1928-10-24 Improvements in or relating to propelling means for aircraft Expired GB300499A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR300499X 1927-11-12

Publications (1)

Publication Number Publication Date
GB300499A true GB300499A (en) 1929-03-07

Family

ID=8888457

Family Applications (1)

Application Number Title Priority Date Filing Date
GB30788/28A Expired GB300499A (en) 1927-11-12 1928-10-24 Improvements in or relating to propelling means for aircraft

Country Status (1)

Country Link
GB (1) GB300499A (en)

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