GB233787A - Improvements in aeroplanes - Google Patents

Improvements in aeroplanes

Info

Publication number
GB233787A
GB233787A GB3978/24A GB397824A GB233787A GB 233787 A GB233787 A GB 233787A GB 3978/24 A GB3978/24 A GB 3978/24A GB 397824 A GB397824 A GB 397824A GB 233787 A GB233787 A GB 233787A
Authority
GB
United Kingdom
Prior art keywords
plane
nacelles
nacelle
supported
construction
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
GB3978/24A
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.)
CLARENCE PERCY LUCAS
Original Assignee
CLARENCE PERCY LUCAS
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 CLARENCE PERCY LUCAS filed Critical CLARENCE PERCY LUCAS
Priority to GB3978/24A priority Critical patent/GB233787A/en
Publication of GB233787A publication Critical patent/GB233787A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Toys (AREA)
  • Prostheses (AREA)

Abstract

233,787. Lucas, C. P. Feb. 15, 1924. Aeroplanes; nacelles; planes, construction of; steering.-The main supporting plane of an aeroplane is kite-shaped in plan, the nacelle b being supported upon or suspended under the front part, and the elevators c, rudder d, fin e, and tail skid f being supported by the narrow rear part. The framework of the plane comprises straight or stream-lined longitudinal sides and intermediate spars with top and bottom booms k separated by vertical braced struts, lateral members m running through the longitudinal members being braced by cross-wires n. Ailerons g are mounted on outwardly-projecting shafts. Two or more nacelles, each furnished wifh an engine unit, may be provided. The construction of plane and the relative arrangement of the nacelle and tail surfaces are also applicable to biplanes and seaplanes.
GB3978/24A 1924-02-15 1924-02-15 Improvements in aeroplanes Expired GB233787A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3978/24A GB233787A (en) 1924-02-15 1924-02-15 Improvements in aeroplanes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3978/24A GB233787A (en) 1924-02-15 1924-02-15 Improvements in aeroplanes

Publications (1)

Publication Number Publication Date
GB233787A true GB233787A (en) 1925-05-15

Family

ID=9768472

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3978/24A Expired GB233787A (en) 1924-02-15 1924-02-15 Improvements in aeroplanes

Country Status (1)

Country Link
GB (1) GB233787A (en)

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