Difference between revisions of "Patent US-1909-943120"
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| + | Pendulum stabilizer attached to the body of the vessel; "Assuming the wholly automatic operation of the controlling means by the weighted lever or pendulum, the relative movement between the machine and the pendulum caused by the pitching or rolling of the machine will effect such movement of the longitudinal and lateral rudders as to steer the machine back into a horizontal position.:; weight may serve as a training device for inexperienced operator | ||
| + | |||
| + | Inventor location (imputed by [[HistPat]]): Boston, MA, Suffolk county, MA (FIPSloc=25025) | ||
| + | |||
| + | Earlier patent referred to by serial number 418679 (filed 1908/03/02),later granted: [[Patent US-1911-989022]]. | ||
| + | |||
| + | === Sources === | ||
| + | * Short's DB | ||
| + | * PTO 244 | ||
| + | * Neilson | ||
| + | * [http://worldwide.espacenet.com/publicationDetails/biblio?FT=D&CC=US&NR=943120A espacenet] | ||
| + | |||
| + | {{Patent family|{{PAGENAME}}}} | ||
| + | |||
{{Patent | {{Patent | ||
|Year filed=1909 | |Year filed=1909 | ||
| Line 4: | Line 18: | ||
|Office=US | |Office=US | ||
|Patent number=943120 | |Patent number=943120 | ||
| − | |Inventors=James | + | |Inventors=James Means |
|Inventor country=US | |Inventor country=US | ||
| − | |Applicant person= | + | |Applicant person=James Means |
|Applicant type=INDIV | |Applicant type=INDIV | ||
| − | |Applicant is inventor= | + | |Applicant is inventor=Yes |
|Original title=Aerial navigation | |Original title=Aerial navigation | ||
|English title=Aerial navigation | |English title=Aerial navigation | ||
| − | |Tech | + | |Tech fields=navigation; stability; pendulum; rudder; airplane; training; subsystem; automatic stability |
| − | |Filing date= | + | |Filing date=March 10, 1909 |
| − | | | + | |Grant date=December 14, 1909 |
| − | + | |Granted=Yes | |
| − | |Granted= | + | |Supplementary to patent=Patent US-1908-989022 |
| − | | | + | |Related to aircraft=Yes |
| − | | | + | |Serial number=482484 |
| − | |Serial number= | + | |National tech categories=USPC 244/80 |
| − | | | + | |CPCs=CPC B64C17/00 |
| − | + | |Family year=1909 | |
| − | |CPCs= | + | |First filing=Yes |
| − | |Family year= | + | |Application ID=47257056 |
| − | |First filing= | + | |INPADOC family ID=43885765 |
| − | | | + | |Number of text pages=3 |
| − | | | + | |Number of diagram pages=2 |
| − | | | + | |Number of figures=3 |
| − | |Number of diagram pages= | + | |Number of claims=14 |
| − | |Number of figures= | ||
}} | }} | ||
Latest revision as of 18:53, 28 December 2024
Pendulum stabilizer attached to the body of the vessel; "Assuming the wholly automatic operation of the controlling means by the weighted lever or pendulum, the relative movement between the machine and the pendulum caused by the pitching or rolling of the machine will effect such movement of the longitudinal and lateral rudders as to steer the machine back into a horizontal position.:; weight may serve as a training device for inexperienced operator
Inventor location (imputed by HistPat): Boston, MA, Suffolk county, MA (FIPSloc=25025)
Earlier patent referred to by serial number 418679 (filed 1908/03/02),later granted: Patent US-1911-989022.
Sources
- Short's DB
- PTO 244
- Neilson
- espacenet
Patent family descending from Patent US-1909-943120
- Patent US-1909-943120 (English title: Aerial navigation, Supplementary to patent: Patent US-1908-989022, Filing date: 1909-03-10, National tech categories: USPC 244/80)
- Patent GB-1909-15402 (English title: Improvements in Aerial Navigation, Supplementary to patent: Patent US-1909-943120, Filing date: 1909-07-01)
| Year filed | 1909 |
|---|---|
| Year granted | 1909 |
| Office | US |
| Patent number | 943120 |
| Inventors | James Means |
| Inventor country | US |
| Inventor location | |
| Applicant person | James Means |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | Yes |
| Original title | Aerial navigation |
| English title | Aerial navigation |
| Tech fields | navigation, stability, pendulum, rudder, airplane, training, subsystem, automatic stability |
| Filing date | March 10, 1909 |
| Full specification filed date | |
| Application number | |
| Grant date | December 14, 1909 |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | Patent US-1908-989022 |
| Related to aircraft? | Yes |
| Serial number | 482484 |
| Patent agent | |
| Assigned to | |
| National tech categories | USPC 244/80 |
| IPCs | |
| CPCs | CPC B64C17/00 |
| Family year | 1909 |
| First filing? | Yes |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 47257056 |
| INPADOC family ID | 43885765 |
| Number of text pages | 3 |
| Number of diagram pages | 2 |
| Number of figures | 3 |
| Number of claims | 14 |
