Difference between revisions of "Patent GB-1912-16059"
Jump to navigation
Jump to search
AvionHerbert (talk | contribs) |
|||
| (One intermediate revision by one other user not shown) | |||
| Line 1: | Line 1: | ||
| + | This original document makes reference to the French [[priority date]] 1911-07-11. | ||
| + | |||
"16,059. Duval, A. I. July 11, 1911, [Convention date]. Void. [Published under [[Section 91]] of the Act.] Balancing; shock of landing, deadening.-A depending rod 1, slidable in guides 2, 3 on the frame 9 of an aeroplane, is provided with a heavy mass 4 at its lower end and tends to preserve equilibrium when lowered with the aid of a cord 7 controlled by the aviator. A spring 5 is interposed between the weight and a collar 6 on the rod to deaden the shock on landing." | "16,059. Duval, A. I. July 11, 1911, [Convention date]. Void. [Published under [[Section 91]] of the Act.] Balancing; shock of landing, deadening.-A depending rod 1, slidable in guides 2, 3 on the frame 9 of an aeroplane, is provided with a heavy mass 4 at its lower end and tends to preserve equilibrium when lowered with the aid of a cord 7 controlled by the aviator. A spring 5 is interposed between the weight and a collar 6 on the rod to deaden the shock on landing." | ||
* Tech class: [[CPC B64C17/00]]: Aircraft stabilisation not otherwise provided for | * Tech class: [[CPC B64C17/00]]: Aircraft stabilisation not otherwise provided for | ||
| − | * Inventor location: 39 rue Richard Lenoir, Flers, Orne, France | + | * Inventor location: 39 rue Richard Lenoir, Flers, [[Orne]], France |
* Parent patent filing date: 1911-07-11 | * Parent patent filing date: 1911-07-11 | ||
| + | {{Patent family|Patent FR-1911-433082}} | ||
=== Sources === | === Sources === | ||
* {{GBpatentsources|191216059A}} | * {{GBpatentsources|191216059A}} | ||
| Line 13: | Line 16: | ||
|Inventor country=FR | |Inventor country=FR | ||
|Applicant person=Arsène-Isidore Duval | |Applicant person=Arsène-Isidore Duval | ||
| − | |||
|Applicant type=INDIV | |Applicant type=INDIV | ||
| − | |Applicant is inventor= | + | |Applicant is inventor=Yes |
|Original title=Improvements in and relating to Stabilising Devices applicable to Aeroplanes | |Original title=Improvements in and relating to Stabilising Devices applicable to Aeroplanes | ||
|English title=Improvements in and relating to Stabilising Devices applicable to Aeroplanes | |English title=Improvements in and relating to Stabilising Devices applicable to Aeroplanes | ||
| − | |Tech field=stability | + | |Tech field=stability; airplane |
| − | |Filing date=1912 | + | |Filing date=1912/07/09 |
| − | |||
|Application number=191216059D | |Application number=191216059D | ||
| − | + | |Granted=Yes | |
| − | |Granted= | ||
| − | |||
|Supplementary to patent=Patent FR-1911-433082 | |Supplementary to patent=Patent FR-1911-433082 | ||
|Related to aircraft=1 | |Related to aircraft=1 | ||
| − | |||
|Patent agent=Haseltine, Lake & Co. | |Patent agent=Haseltine, Lake & Co. | ||
| − | |||
| − | |||
|IPCs=IPC B64C17/00 | |IPCs=IPC B64C17/00 | ||
|CPCs=CPC B64C2700/6212; CPC B64C17/00 | |CPCs=CPC B64C2700/6212; CPC B64C17/00 | ||
| − | |Family year= | + | |Family year=1911 |
| − | |First filing= | + | |First filing=No |
| − | |||
| − | |||
|Application ID=23636352 | |Application ID=23636352 | ||
|INPADOC family ID=11124233 | |INPADOC family ID=11124233 | ||
Latest revision as of 05:51, 25 April 2024
This original document makes reference to the French priority date 1911-07-11.
"16,059. Duval, A. I. July 11, 1911, [Convention date]. Void. [Published under Section 91 of the Act.] Balancing; shock of landing, deadening.-A depending rod 1, slidable in guides 2, 3 on the frame 9 of an aeroplane, is provided with a heavy mass 4 at its lower end and tends to preserve equilibrium when lowered with the aid of a cord 7 controlled by the aviator. A spring 5 is interposed between the weight and a collar 6 on the rod to deaden the shock on landing."
- Tech class: CPC B64C17/00: Aircraft stabilisation not otherwise provided for
- Inventor location: 39 rue Richard Lenoir, Flers, Orne, France
- Parent patent filing date: 1911-07-11
Patent family descending from Patent FR-1911-433082
- Patent FR-1911-433082 (English title: Universal airplane balancer, National tech categories: FR 6.4)
- Patent GB-1912-16059 (English title: Improvements in and relating to Stabilising Devices applicable to Aeroplanes, Supplementary to patent: Patent FR-1911-433082)
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
| Year filed | 1912 |
|---|---|
| Year granted | 1912 |
| Office | GB |
| Patent number | 16059 |
| Inventors | Arsène-Isidore Duval |
| Inventor country | FR |
| Applicant person | Arsène-Isidore Duval |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Improvements in and relating to Stabilising Devices applicable to Aeroplanes |
| English title | Improvements in and relating to Stabilising Devices applicable to Aeroplanes |
| Tech fields | stability, airplane |
| Filing date | 1912/07/09 |
| Full specification filed date | |
| Application number | 191216059D |
| Grant date | |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | Patent FR-1911-433082 |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | Haseltine, Lake & Co. |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64C17/00 |
| CPCs | CPC B64C2700/6212, CPC B64C17/00 |
| Family year | 1911 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 23636352 |
| INPADOC family ID | 11124233 |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 1 |
| Number of claims | 1 |
