Patent US-1910-1065263

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Helicopter for aeroplanes ; adjustable blades ; wheel-rim which acts as gyroscope ; stabilizes the aeroplane and also as a fly-wheel for accumulating energy from the motor ; pilot can immediately jerk airplane up if needed ; VTOL

Claims: hollow shaft with spokes radiating from it and blades rotating on all sides, rings or bearings and springs, sleeve on the shaft slides and is controlled by the pilot

  • Tech class: CPC B64C11/343: Blade pitch-changing mechanisms mechanical automatic actuated by the centrifugal force or the aerodynamic drag acting on the blades
  • Inventor location: Dusseldorf, Germany ; citizen of German empire ; signed this document at Barmen

Inventor signed on 1910-01-03. 15 days later, this patent was recorded as filed at the patent office.

Sources


Year filed 1910
Year granted 1913
Office US
Patent number 1065263
Inventors Gustav Mees
Inventor country DE
Inventor location Düsseldorf
Applicant person Gustav Mees
Applicant firm
Applicant type INDIV
Applicant is inventor? 1
Original title Aeroplane steering and stabilizing mechanism
English title Aeroplane steering and stabilizing mechanism
Tech fields propulsion, control, gyroscope, helicopter
Filing date January 18, 1910
Full specification filed date
Application number 1910538686
Grant date June 17, 1913
Granted? 1
Publication date
Supplementary to patent
Related to aircraft? 1
Serial number 538686
Patent agent
Assigned to
National tech categories USPC 416/136, USPC 416/195, USPC 416/164, USPC 244/79
IPCs
CPCs CPC B64C11/343
Family year 1910
First filing? 1
Cites these patents
Citations from after 1930 1
Application ID 47583521
INPADOC family ID 43917313
Number of text pages 3
Number of diagram pages 2
Number of figures 7
Number of claims 2