GB360643A - Improvements in propelling means for aircraft - Google Patents
Improvements in propelling means for aircraftInfo
- Publication number
- GB360643A GB360643A GB32120/30A GB3212030A GB360643A GB 360643 A GB360643 A GB 360643A GB 32120/30 A GB32120/30 A GB 32120/30A GB 3212030 A GB3212030 A GB 3212030A GB 360643 A GB360643 A GB 360643A
- Authority
- GB
- United Kingdom
- Prior art keywords
- oct
- aircraft
- shafts
- crank shafts
- propellers
- 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
- JHIVVAPYMSGYDF-UHFFFAOYSA-N cyclohexanone Chemical compound O=C1CCCCC1 JHIVVAPYMSGYDF-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D35/00—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Operated Clutches (AREA)
- Retarders (AREA)
Abstract
360,643. Plant. FIAT SOC. ANON., 250, Via Nizza, Turin, Italy. Oct. 25, 1930, No. 32120. Convention date, Oct. 25, 1929. Addition to 360,167. [Class 7 (ii).] The engines used to drive tandem aircraft propellers are coupled together by a hand operated or automatic clutch 25, which connects the two crank shafts 1, 13 together. The propellers rotate in opposite directions their hubs being fast on concentric shafts 9, 21 driven through reducing gear 3, 15 from the crank shafts.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT360643X | 1929-10-25 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB360643A true GB360643A (en) | 1931-11-12 |
Family
ID=11244556
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB32120/30A Expired GB360643A (en) | 1929-10-25 | 1930-10-25 | Improvements in propelling means for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB360643A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11746727B2 (en) | 2021-11-23 | 2023-09-05 | Rolls-Royce Plc | Aircraft propulsion system configured to substantially cancel component gyroscopic forces |
-
1930
- 1930-10-25 GB GB32120/30A patent/GB360643A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US11746727B2 (en) | 2021-11-23 | 2023-09-05 | Rolls-Royce Plc | Aircraft propulsion system configured to substantially cancel component gyroscopic forces |
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