GB600779A - Improvements in propulsion systems for aircraft - Google Patents
Improvements in propulsion systems for aircraftInfo
- Publication number
- GB600779A GB600779A GB14390/45A GB1439045A GB600779A GB 600779 A GB600779 A GB 600779A GB 14390/45 A GB14390/45 A GB 14390/45A GB 1439045 A GB1439045 A GB 1439045A GB 600779 A GB600779 A GB 600779A
- Authority
- GB
- United Kingdom
- Prior art keywords
- propellers
- wing
- aircraft
- slipstream
- driven
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
600,779. Propelling aircraft. ALMONACID, V. A. June 7, 1945, No. 14390. [Class 4] A series of propellers 9 are arranged along the leading edges 10 of an aircraft wing, their disc circles 40 overlapping to furnish a continuous unbroken slipstream across the wing span. To avoid blade interference, the propellers are driven in the same or opposite directions at a predetermined relative angular relationship, as shown in Figs. 8 and 11, the propeller shafts being spaced apart by a distance approximately equal to three-quarters of the propeller diameter. As shown in Fig. 2, the propellers are driven from one or more engines in the fuselage through cranks interconnected by flexible connecting rods 4, which may be of the type described in Specification 485,053. Fig. 16 shows the invention applied to a flying boat in which the ailerons 44 and tail surfaces 42, 43 are arranged in the slipstream from the propellers. An auxiliary wing 47 is mounted forwardly of the main wing to facilitate take-off.
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB600779A true GB600779A (en) | 1948-04-19 |
Family
ID=1730707
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB14390/45A Expired GB600779A (en) | 1945-06-07 | Improvements in propulsion systems for aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB600779A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102016007934A1 (en) * | 2016-06-28 | 2017-12-28 | Jakob Berns | Device for transmitting the rotary power for very large center distances between the drive and output axles |
-
1945
- 1945-06-07 GB GB14390/45A patent/GB600779A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE102016007934A1 (en) * | 2016-06-28 | 2017-12-28 | Jakob Berns | Device for transmitting the rotary power for very large center distances between the drive and output axles |
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