Difference between revisions of "Patent GB-1912-2473"
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"Void. [Published under Section 91 of the Act.] Balancing ; cars; tanks, arrangement of. In an aeroplane, the car B and petrol tank C are adjustably mounted on a mast A pivoted to the frame F carrying the planes D, E. The ends of the mast are connected by extensible cords m, n to the tips of the planes. An additional mass P may be attached to the lower end of the mast" | "Void. [Published under Section 91 of the Act.] Balancing ; cars; tanks, arrangement of. In an aeroplane, the car B and petrol tank C are adjustably mounted on a mast A pivoted to the frame F carrying the planes D, E. The ends of the mast are connected by extensible cords m, n to the tips of the planes. An additional mass P may be attached to the lower end of the mast" | ||
| − | * "Per Lewis H. Rittman" | + | * "Per Lewis H. Rittman" -- on last page of patent text. Meaning not clear yet. |
* Tech class: [[CPC B64C17/06]]: Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus | * Tech class: [[CPC B64C17/06]]: Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus | ||
* Inventor location: 25 rue Pigalle, Paris, France | * Inventor location: 25 rue Pigalle, Paris, France | ||
* Inventor occupation: Manufacturer | * Inventor occupation: Manufacturer | ||
* This patent application was NOT granted. It looks fine, so this is likely a case where the fee wasn't paid on time or some such. {{Not granted}} | * This patent application was NOT granted. It looks fine, so this is likely a case where the fee wasn't paid on time or some such. {{Not granted}} | ||
| + | {{Patent family|Patent FR-1911-426612}} | ||
=== Sources === | === Sources === | ||
* {{GBpatentsources|191202473A}} | * {{GBpatentsources|191202473A}} | ||
| Line 29: | Line 30: | ||
|Granted=0 | |Granted=0 | ||
|Publication date= | |Publication date= | ||
| − | |Supplementary to patent=Patent FR-1911- | + | |Supplementary to patent=Patent FR-1911-426612 |
|Related to aircraft=1 | |Related to aircraft=1 | ||
|Serial number= | |Serial number= | ||
| − | |Patent agent= | + | |Patent agent=None |
|Assigned to= | |Assigned to= | ||
|National tech categories= | |National tech categories= | ||
| Line 38: | Line 39: | ||
|CPCs=CPC B64C17/06; CPC B64C2700/6216 | |CPCs=CPC B64C17/06; CPC B64C2700/6216 | ||
|Family year=1911 | |Family year=1911 | ||
| − | |First filing= | + | |First filing=0 |
|Cites these patents= | |Cites these patents= | ||
|Citations from after 1930=0 | |Citations from after 1930=0 | ||
Latest revision as of 01:09, 27 March 2024
The pilot's seat and the petrol tank can slide around on a mast to help maintain balance and stability in the air.
"Void. [Published under Section 91 of the Act.] Balancing ; cars; tanks, arrangement of. In an aeroplane, the car B and petrol tank C are adjustably mounted on a mast A pivoted to the frame F carrying the planes D, E. The ends of the mast are connected by extensible cords m, n to the tips of the planes. An additional mass P may be attached to the lower end of the mast"
- "Per Lewis H. Rittman" -- on last page of patent text. Meaning not clear yet.
- Tech class: CPC B64C17/06: Aircraft stabilisation not otherwise provided for by gravity or inertia-actuated apparatus by gyroscopic apparatus
- Inventor location: 25 rue Pigalle, Paris, France
- Inventor occupation: Manufacturer
- This patent application was NOT granted. It looks fine, so this is likely a case where the fee wasn't paid on time or some such. Template:Not granted
Patent family descending from Patent FR-1911-426612
- Patent FI-1911-4527 (English title: Apparatus for stabilizing the equilibrium position of an aeroplane, Supplementary to patent: Patent FR-1911-426612)
- Patent FR-1911-426612 (English title: Stabilization system for airplanes, National tech categories: FR 6.4)
- Patent GB-1912-2473 (English title: A system of flight stabilisation for aeroplanes, Supplementary to patent: Patent FR-1911-426612)
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
| Year filed | 1912 |
|---|---|
| Year granted | |
| Office | GB |
| Patent number | 2473 |
| Inventors | Louis-Alphonse Canda |
| Inventor country | FR |
| Applicant person | Louis-Alphonse Canda |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | A System of Flight Stabilisation for Aeroplanes |
| English title | A system of flight stabilisation for aeroplanes |
| Tech fields | stability |
| Filing date | 1912-01-30 |
| Full specification filed date | |
| Application number | 191202473D |
| Grant date | |
| Granted? | 0 |
| Publication date | |
| Supplementary to patent | Patent FR-1911-426612 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | None |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64C1/00, IPC B64C17/06 |
| CPCs | CPC B64C17/06, CPC B64C2700/6216 |
| Family year | 1911 |
| First filing? | 0 |
| Cites these patents | |
| Citations from after 1930 | 0 |
| Application ID | 23628350 |
| INPADOC family ID | 11117375 |
| Number of text pages | 3 |
| Number of diagram pages | 1 |
| Number of figures | 4 |
| Number of claims | 9 |
