Patent GB-1918-121464

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"121,464. Soc. des Moteurs Salmson, (Système Canton Unné). Dec. 11, 1917, [Convention date]. Cars and cabins; framework; steering and balancing. - The pivotal members for the elevators and rudder of an aeroplane are supported by a vertical tube welded to sockets which receive the rear ends of the fuselage longerons, the sockets being held in position by the fuselage stay-wires. Figs. 1 and 2 show the sockets b welded to a vertical tube a and held on the ends of the longerons d, e by the stay wires f, g. The tubular shaft j for the elevators is carried by bearings i supported by a crosstube h passing through and welded to the tube a. The rudder is pivoted on the tube a by means of pivots m, m<1>. Inclined tubular braces o, n and stay-wires p are arranged as shown in Fig. 5."

  • Tech class CPC B64C9/00: Adjustable control surfaces or members, e.g. rudders
  • Applicant location: Société des Moteurs Salmson, No. 74, rue St. Lazare, Paris ; Manufacturers

Patent family descending from Patent FR-1917-12-11-Salmson

Sources


Year filed 1918
Year granted 1919
Office GB
Patent number 121464
Inventors
Inventor country FR
Inventor location Paris
Applicant person
Applicant firm Moteurs Salmson
Applicant type INDIV
Applicant is inventor? 1
Original title An Improved Tail-piece for Aeroplanes
English title An Improved Tail-piece for Aeroplanes
Tech fields tail
Filing date 1918-11-27
Full specification filed date
Application number 1958018
Grant date 1919-04-17
Granted? 1
Publication date
Supplementary to patent Patent FR-1917-12-11-Salmson
Related to aircraft? 1
Serial number 19580
Patent agent Marks & Clerk
Assigned to
National tech categories
IPCs IPC B64C9/00
CPCs CPC B64C9/00
Family year 1917
First filing? 1
Cites these patents
Citations from after 1930 0
Application ID
INPADOC family ID
Number of text pages 2
Number of diagram pages 1
Number of figures 5
Number of claims 6