Patent US-1916-1210376
Control planes with dihedral; different from ailerons. Description is 6 pages (long). Series of wings and control planes longitudinally ; normally 3 -- a big wing and a forward elevator and tail). Control planes can be set to have high or low dihedral. Goal: greater longitudinal stability, simple efficient control of elevation, and low resistance of elevation control. each control planes has dihedral angle which can be different from the others. The fixed planes and the control planes are all supporting planes. Control planes "always have the same angle of incidence". For take-off, the most-forward pair of control planes are set to horizontal plane and the aft-most pair are raised to dihedral of 30 degrees, the normal dihedral angle being 15. When gliding horizontally, the control planes are brought to their normal angle, matching the wings. In descent, the front pair are angled maximally and the back ones are either horizontal or match the wings. (Useful service of these adjustments is not transparent; would changing dihedral affect altitude significantly?) Ailerons and warping arrangements are not illustrated "as their application is well understood."
- Inventor location: Manchester, County of Lancaster, England
- Assignee (Urquhart) location: Liscard, near Birkenhead, England ; assigned one half of the patent; this is Ridley James Urquhart
- serial number 34227 and 100360 ; 100360 is the serial number of patent number 1210376, as such ; there is likely another patent number associated with the serial number 34227, filed 1915-05-15. For tracking these small categories, tag them: Tag: Divided patents Tag: Renewed patents
- Witnesses as shown on the final text page: Malcolm Smethurst and Ernald Simpson Moseley
Sources
- Patent 1210376 document and bibliographic info on espacenet
- Patent 1210376 at google patents
| Year filed | 1916 |
|---|---|
| Year granted | 1916 |
| Office | US |
| Patent number | 1210376 |
| Inventors | William Morton James |
| Inventor country | GB |
| Inventor location | |
| Applicant person | William Morton James |
| Applicant firm | |
| Applicant type | |
| Applicant is inventor? | No |
| Original title | Aeroplane |
| English title | Aeroplane |
| Tech fields | control, stability, airplane, skids, design, cables, HTA, wings, sustentation |
| Filing date | 1916/05/27 |
| Full specification filed date | 1916/05/27 |
| Application number | 10036016 |
| Grant date | 1916/12/26 |
| Granted? | Yes |
| Publication date | |
| Supplementary to patent | Patent US-1915-05-15 William Morton James |
| Related to aircraft? | 1 |
| Serial number | 100869 |
| Patent agent | Herbert E. Smith (?) |
| Assigned to | Ridley J. Urquhart |
| National tech categories | USPC 244/89, USPC 244/45R, USPC 244/48 |
| IPCs | |
| CPCs | CPC B64C13/00 |
| Family year | 1915 |
| First filing? | No |
| Cites these patents | |
| Citations from after 1930 | |
| Application ID | 47834384 |
| INPADOC family ID | 43014553 |
| Number of text pages | 6 |
| Number of diagram pages | 2 |
| Number of figures | 11 |
| Number of claims | 8 |
