Patent US-1917-1225711

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The invention refers to the structure of components of an aerofoil. Some claims refer to nose-piece (a strong/rigid front edge I believe), and others to ribs or spars. Refers to "aerofoils of aeroplanes of the variable camber type", either "the main supporting planes or auxiliary planes employed for controlling and stabilizing purposes." The design proposed is a rigid front edge of the aerofoil and a flexible deformable rear edge so the tilt aka angle-of-incidence can be changed and so can the camber. The patent text refers to what this can accomplish:

  • expanding the range of speeds of the aircraft both horizontally and vertically
  • "to extend its range of angles of ascent and descent"
  • to raise its maximum altitude
  • check original for more
  • Tech classification: CPC B64C3/48: Varying camber by relatively-movable parts of wing structures -- a category that expanded a lot later
  • Inventor location: residing at Bisham Lodge, Speer Road, Thames Ditton, in the county of Surrey, England
  • Inventor citizenship: a subject of the Queen of the Netherlands

Sources


Year filed 1916
Year granted 1917
Office US
Patent number 1225711
Inventors Alexander Albert Holle
Inventor country GB, NL
Applicant person Alexander Albert Holle
Applicant firm
Applicant type INDIV
Applicant is inventor? Yes
Original title Plane and the like for aeroplanes
English title Plane and the like for aeroplanes
Tech fields aerofoil, camber, shape, angle of incidence
Filing date December 22, 1916
Full specification filed date
Application number 13846416
Grant date May 8, 1917
Granted? Yes
Publication date
Supplementary to patent
Related to aircraft? Yes
Serial number
Patent agent
Assigned to Varioplane Company
National tech categories USPC 244/219
IPCs IPC B64C3/48, IPC B64C3/00
CPCs CPC B64C3/48
Family year 1916
First filing? Yes
Cites these patents
Citations from after 1930
Application ID 47861406
INPADOC family ID 43248158
Number of text pages
Number of diagram pages
Number of figures
Number of claims