Patent FR-1910-421257

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This patent has two additions within the French system. We have virtually no data on the first addition. While this parent patent features a pendulum, responsive to aircraft tilt, an element we have found before in the context of specifically automatic airplane stability, the second addition, Patent FR-1911-421257.14854, upon which we have good data, focuses on the specific application, to the ailerons. of the compressed air which is crucial throughout this patent family.

So, the tilt of the aircraft affects the pendulum, and the pendulum directs the compressed air, which in turn affects the specific movement of the ailerons, and the resulting affect on control and stability.

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Patent family descending from Patent FR-1910-421257


Year filed 1910
Year granted 1910
Office FR
Patent number 421257
Inventors Jules Sandret
Inventor country FR
Applicant person Jules Sandret
Applicant firm
Applicant type INDIV
Applicant is inventor? Yes
Original title Appareil stabilisateur automatique pour aéroplanes
English title Automatic stabilizer apparatus for airplanes
Tech fields airplane, stability, subsystem, aerodynamics, aileron, control, pistons, wings, pendulum, automatic stability
Filing date 1910/10/08
Full specification filed date
Application number 421257D
Grant date 1910/12/16
Granted? Yes
Publication date 1911/02/18
Supplementary to patent
Related to aircraft? Yes
Serial number
Patent agent E. Blétry
Assigned to
National tech categories FR 6.4
IPCs IPC B64C17/00
CPCs CPC B64C17/00, CPC B64C2700/6212
Family year 1910
First filing? Yes
Cites these patents
Citations from after 1930
Application ID 19240126
INPADOC family ID 5199158
Number of text pages 3
Number of diagram pages 1
Number of figures 1
Number of claims 4