GB538047A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB538047A GB538047A GB7466/40A GB746640A GB538047A GB 538047 A GB538047 A GB 538047A GB 7466/40 A GB7466/40 A GB 7466/40A GB 746640 A GB746640 A GB 746640A GB 538047 A GB538047 A GB 538047A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gear
- clutch
- engines
- shaft
- aircraft
- 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
- 230000005540 biological transmission Effects 0.000 abstract 4
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
- B64D35/08—Transmitting power from power plants to propellers or rotors; Arrangements of transmissions characterised by the transmission being driven by a plurality of power plants
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Structure Of Transmissions (AREA)
Abstract
538,047. Driving and controlling aircraft. TAMPIER, R. April 25, 1940, No. 7466. [Class 4] An aircraft is driven by two engines 2, 3 which drive a power shaft 9 through bevel gear, sleeves 8, 8<1>, and clutches 10, 10<1>, change speed gear 30, 31, 32, 33 being arranged between the power shaft 9 and a transmission shaft geared to two propellers 22, 23. The transmission shaft is in two parts normally connected together by a clutch 24, but when the clutch is disengaged a gear 26, which may be integral with one part of the clutch, is brought into mesh with a gear 29 on the sleeve 8', and if the clutch 10<1> be then disengaged the two propellers can be driven independently by the two engines to give lateral control. The change speed gear, which has its wheels 32, 33 connected together and slidable on the transmission shaft, gives a step up speed ratio between the shaft 9 and the propeller shafts. The transmission between the engines and the gear box may be of the kind described in Specification 538,046.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7466/40A GB538047A (en) | 1940-04-25 | 1940-04-25 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB7466/40A GB538047A (en) | 1940-04-25 | 1940-04-25 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB538047A true GB538047A (en) | 1941-07-17 |
Family
ID=9833624
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB7466/40A Expired GB538047A (en) | 1940-04-25 | 1940-04-25 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB538047A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2452281A (en) * | 1944-07-06 | 1948-10-26 | United Aircraft Corp | Aircraft propulsion means |
| CN102514716A (en) * | 2011-11-29 | 2012-06-27 | 南京航空航天大学 | Single-engine power driving mechanism for tilting rotor aircraft |
| DE102019218100A1 (en) * | 2019-11-22 | 2021-05-27 | Rolls-Royce Deutschland Ltd & Co Kg | Wave mechanical drive system and method for an aircraft |
-
1940
- 1940-04-25 GB GB7466/40A patent/GB538047A/en not_active Expired
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2452281A (en) * | 1944-07-06 | 1948-10-26 | United Aircraft Corp | Aircraft propulsion means |
| CN102514716A (en) * | 2011-11-29 | 2012-06-27 | 南京航空航天大学 | Single-engine power driving mechanism for tilting rotor aircraft |
| CN102514716B (en) * | 2011-11-29 | 2014-05-14 | 南京航空航天大学 | Single-engine power driving mechanism for tilting rotor aircraft |
| DE102019218100A1 (en) * | 2019-11-22 | 2021-05-27 | Rolls-Royce Deutschland Ltd & Co Kg | Wave mechanical drive system and method for an aircraft |
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