Patent FR-1911-428887
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- Full title: Aéronef de combat à air condensé (à condensateur, à ailes élévatrices et ramantes, à hélices condensatrices, à moteur et hélice encagés et mobiles, à plate-forme pour ballons, à nacelle de guerre, à sabot d'atterrissage à buttée mobile, à queue mobile)
- In English: Aircraft with condensed air (condenser, lifting and rowing wings, condensing propellers, motor and propeller, caged and mobile, balloon platform, warplane, moveable abutment, mobile tail)
- Possibly the wings flap
This aircraft retains as much force as possible along the lines of earlier aircraft, wastes less of it, and, by way of condensing the air resulting from movement and other processes, maximizes speed, weight carried, lift and stability. The "condensateur" mentioned above, with all the described factors of enhancement, does all this via what we usually call compression, the opposite in principle of rarefaction.
- Inventor location: 44 rue de la Prévoyance, Vincennes, département Seine, France
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
Year filed | 1911 |
---|---|
Year granted | 1911 |
Office | FR |
Patent number | 428887 |
Inventors | Ferdinand-Corinthe Dandois |
Inventor country | FR |
Applicant person | Ferdinand-Corinthe Dandois |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Aéronef de combat à air condensé (à condensateur, à ailes élévatrices et ramantes, à hélices condensatrices, à moteur et hélice encagés et mobiles, à plate-forme pour ballons, à nacelle de guerre, à sabot d'atterrissage à buttée mobile, à queue mobile) |
English title | Combat aircraft with condensed air(with condenser, wings of both lift and ascension, condenser propellers, with encased and mobile motors and propellers, balloon platform, war pod, landing shoe with movable stop, and movable tail) |
Tech fields | aircraft, hybrid, wings, military, flapping, motors, propellers, balloons, control, steering, stability, sustentation, propulsion, automatic stability, texture, compression |
Filing date | 1911/04/25 |
Full specification filed date | |
Application number | 428887D |
Grant date | 1911/07/01 |
Granted? | Yes |
Publication date | 1911/09/09 |
Supplementary to patent | |
Related to aircraft? | Yes |
Serial number | |
Patent agent | |
Assigned to | |
National tech categories | FR 6.4 |
IPCs | IPC B64C39/00 |
CPCs | CPC B64C2700/6297, CPC B64C39/00 |
Family year | 1911 |
First filing? | Yes |
Cites these patents | |
Citations from after 1930 | |
Application ID | 19247596 |
INPADOC family ID | 5319988 |
Number of text pages | 6 |
Number of diagram pages | 1 |
Number of figures | 6 |
Number of claims | 1 |