GB223023A - Improvements in and relating to a combined motorcycle and aeroplane - Google Patents

Improvements in and relating to a combined motorcycle and aeroplane

Info

Publication number
GB223023A
GB223023A GB22286/23A GB2228623A GB223023A GB 223023 A GB223023 A GB 223023A GB 22286/23 A GB22286/23 A GB 22286/23A GB 2228623 A GB2228623 A GB 2228623A GB 223023 A GB223023 A GB 223023A
Authority
GB
United Kingdom
Prior art keywords
aeroplane
motor
cycle
propeller
frame
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
GB22286/23A
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
Priority to GB22286/23A priority Critical patent/GB223023A/en
Publication of GB223023A publication Critical patent/GB223023A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft

Abstract

223,023. Johnson, B. Sept. 4,1923. Aeroplanes; propelling; steering; land wheels. -A combined aeroplane and motor-cycle comprises, in combination, a complete motor-cycle, an aeroplane body 16, partially enclosing the frame of the cycle, and including a drivers pit 17, vertical and horizontal stablizing fins 21 at the rear, a rudder 22 connected by links to a cross-bar associated with the handle bars, planes arranged in advance of the driver's seat and pivoted as a unit to the body or frame, a lever 28 for controlling the angular position of the planes and a propeller 35. The propeller is carried by a shaft 34, Fig. 2, enclosed in a tube 33 and driven from the motor by an oblique shaft 38 and bevel gearing.
GB22286/23A 1923-09-04 1923-09-04 Improvements in and relating to a combined motorcycle and aeroplane Expired GB223023A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB22286/23A GB223023A (en) 1923-09-04 1923-09-04 Improvements in and relating to a combined motorcycle and aeroplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB22286/23A GB223023A (en) 1923-09-04 1923-09-04 Improvements in and relating to a combined motorcycle and aeroplane

Publications (1)

Publication Number Publication Date
GB223023A true GB223023A (en) 1924-10-16

Family

ID=10176913

Family Applications (1)

Application Number Title Priority Date Filing Date
GB22286/23A Expired GB223023A (en) 1923-09-04 1923-09-04 Improvements in and relating to a combined motorcycle and aeroplane

Country Status (1)

Country Link
GB (1) GB223023A (en)

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