Patent FR-1913-460044
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Sources
- Original patent document and bibliography entry on espacenet
- on google patents
- Original via Espacenet
(A vast structural lengthwise "beam" constitutes the nacelle of this aircraft. This is actually called a "poutre-nacelle". This is situated only slightly below the gas-containing bulk of the aircraft and is fairly well subsumed therein. Rigid cones, attached to this beam-nacelle at either end, facilitate the form of the overall surface and aid in the lowering of control or lift ballonets, the envelope modifying its section under the increase in exterior pressure thanks to the weight of the beam-nacelle. The circular forward armature segments are "élastiques" and thereby compliant with the oscillations in envelope shape. All apparatus of propulsion, control, defense and attack are situated within the "poutre-nacelle".)
- Inventor location: Seine, France
Year filed | 1913 |
---|---|
Year granted | 1913 |
Office | FR |
Patent number | 460044 |
Inventors | Camille Lacoste |
Inventor country | FR |
Applicant person | Camille Lacoste |
Applicant firm | |
Applicant type | INDIV |
Applicant is inventor? | Yes |
Original title | Perfectionnements aux ballons dirigeables |
English title | Improvements in the frame and design of military dirigibles |
Tech fields | LTA, balloon, dirigible, construction, frame, airship, military |
Filing date | July 4, 1913 |
Full specification filed date | |
Application number | 460044D |
Grant date | September 24, 1913 |
Granted? | Yes |
Publication date | November 21, 1913 |
Supplementary to patent | |
Related to aircraft? | Yes |
Serial number | |
Patent agent | Hippolyte Josse |
Assigned to | |
National tech categories | FR 6.4 |
IPCs | IPC B64B1/00 |
CPCs | CPC B64B1/00 |
Family year | 1913 |
First filing? | No |
Cites these patents | |
Citations from after 1930 | |
Application ID | 19278067 |
INPADOC family ID | 5346016 |
Number of text pages | 3 |
Number of diagram pages | 1 |
Number of figures | 4 |
Number of claims | 4 |