Difference between revisions of "Patent GB-1913-22493"
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m (Text replacement - "|Applicant is inventor=1 |Filing date=" to "|Applicant is inventor=1 |Original title= |English title= |Tech field= |Filing date=") |
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| + | "22,493. Green, r. M. Oct. 6. P l a n e s, arrangement and construction of.-The longitudinal spars D, E of the wing B of an aeroplane are connected by a single series of struts K to a lower wing C in the case of a biplane, and to a laterally-extending girder in the case of a monoplane. The struts are preferably I-shaped, and capable of bending fore-and-aft in order that the load on the lower wing may be transferred to the upper plane in case the centre of pressure of the lower plane is not coincident with the axis of the strut. A similar strut H connects the wings to the body A. Brace wires L, M, N are arranged as shown." | ||
| + | * B64C3/18 Spars; Ribs; Stringers | ||
| + | * Inventor location: | ||
| + | === Sources === | ||
| + | * {{GBpatentsources|191322493A}} | ||
{{Patent | {{Patent | ||
|Year filed=1913 | |Year filed=1913 | ||
| − | |Year granted= | + | |Year granted=1914 |
|Office=GB | |Office=GB | ||
|Patent number=22493 | |Patent number=22493 | ||
| − | |Inventors=Frederick Michael | + | |Inventors=Frederick Michael Green |
| − | |Applicant person= | + | |Inventor country=GB |
| + | |Applicant person=Frederick Michael Green | ||
| + | |Applicant firm= | ||
|Applicant type=INDIV | |Applicant type=INDIV | ||
|Applicant is inventor=1 | |Applicant is inventor=1 | ||
| − | |Original title= | + | |Original title=Improvements in or relating to the Construction of Aeroplanes |
| − | |English title= | + | |English title=Improvements in or relating to the Construction of Aeroplanes |
| − | |Tech field= | + | |Tech field=construction |
|Filing date=1913-10-06 | |Filing date=1913-10-06 | ||
| + | |Full specification filed date=1914-04-06 | ||
|Application number=191322493D | |Application number=191322493D | ||
| − | |Granted= | + | |Grant date=1914-07-09 |
| + | |Granted=1 | ||
| + | |Publication date= | ||
| + | |Supplementary to patent= | ||
| + | |Related to aircraft=1 | ||
| + | |Serial number= | ||
| + | |Patent agent=F. M. Rogers & Co. | ||
| + | |Assigned to= | ||
| + | |National tech categories= | ||
| + | |IPCs=IPC B64C3/18 | ||
|CPCs=CPC B64C3/18 | |CPCs=CPC B64C3/18 | ||
|Family year=1913 | |Family year=1913 | ||
|First filing=1 | |First filing=1 | ||
| + | |Cites these patents= | ||
| + | |Citations from after 1930=0 | ||
|Application ID=23657712 | |Application ID=23657712 | ||
|INPADOC family ID=11142564 | |INPADOC family ID=11142564 | ||
| + | |Number of text pages=2 | ||
| + | |Number of diagram pages=1 | ||
| + | |Number of figures=1 | ||
| + | |Number of claims=3 | ||
}} | }} | ||
| − | |||
| − | |||
| − | |||
Latest revision as of 00:40, 1 April 2024
"22,493. Green, r. M. Oct. 6. P l a n e s, arrangement and construction of.-The longitudinal spars D, E of the wing B of an aeroplane are connected by a single series of struts K to a lower wing C in the case of a biplane, and to a laterally-extending girder in the case of a monoplane. The struts are preferably I-shaped, and capable of bending fore-and-aft in order that the load on the lower wing may be transferred to the upper plane in case the centre of pressure of the lower plane is not coincident with the axis of the strut. A similar strut H connects the wings to the body A. Brace wires L, M, N are arranged as shown."
- B64C3/18 Spars; Ribs; Stringers
- Inventor location:
Sources
- Original patent document and bibliography entry on espacenet
- on google patents
| Year filed | 1913 |
|---|---|
| Year granted | 1914 |
| Office | GB |
| Patent number | 22493 |
| Inventors | Frederick Michael Green |
| Inventor country | GB |
| Applicant person | Frederick Michael Green |
| Applicant firm | |
| Applicant type | INDIV |
| Applicant is inventor? | 1 |
| Original title | Improvements in or relating to the Construction of Aeroplanes |
| English title | Improvements in or relating to the Construction of Aeroplanes |
| Tech fields | construction |
| Filing date | 1913-10-06 |
| Full specification filed date | 1914-04-06 |
| Application number | 191322493D |
| Grant date | 1914-07-09 |
| Granted? | 1 |
| Publication date | |
| Supplementary to patent | |
| Related to aircraft? | 1 |
| Serial number | |
| Patent agent | F. M. Rogers & Co. |
| Assigned to | |
| National tech categories | |
| IPCs | IPC B64C3/18 |
| CPCs | CPC B64C3/18 |
| Family year | 1913 |
| First filing? | 1 |
| Cites these patents | |
| Citations from after 1930 | 0 |
| Application ID | 23657712 |
| INPADOC family ID | 11142564 |
| Number of text pages | 2 |
| Number of diagram pages | 1 |
| Number of figures | 1 |
| Number of claims | 3 |
