GB910185A - Improvements in or relating to transmission gearing of twin-engined hub-driven, coaxial, contrarotative aircraft-lifting or/and-sustaining rotors - Google Patents
Improvements in or relating to transmission gearing of twin-engined hub-driven, coaxial, contrarotative aircraft-lifting or/and-sustaining rotorsInfo
- Publication number
- GB910185A GB910185A GB23461/58A GB2346158A GB910185A GB 910185 A GB910185 A GB 910185A GB 23461/58 A GB23461/58 A GB 23461/58A GB 2346158 A GB2346158 A GB 2346158A GB 910185 A GB910185 A GB 910185A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- coaxial
- pinion
- driven
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Retarders (AREA)
- Gear Transmission (AREA)
Abstract
910,185. Rotary wing aircraft. SHAPIRO, J. S., MEADS, B. A. G., and PRESTON, R. L. Oct. 22, 1959 [July 22, 1958], No. 23461/58. Class 4. A coaxial contra-rotating aircraft lifting rotor assembly comprises two coaxial rotor drive shafts, Oi, O 2 , driven by two independent engines, the axes of whose output shafts Ii, I 2 , enclose an acute angle in a plane perpendicular to the common axis of shafts O 1 , O 2 and meet on the common axis, each output shaft carrying a pinion P 1 , P 2 , meshing with two opposed crown wheels C 1 , C 2 , one on each of shafts Oi, O 2 . A third pinion P 3 relieving bending stresses on the crown wheels may be idle, or be connected to drive auxiliaries, or to a brake drum. The gear casing is in two parts H 1 , H 2 , between which is secured a rigid diaphragm D affording bearings for the ends of shafts Ii, I 2 , and for the inner end of the pinion P 3 , which has a bearing for its outer end in the casing.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23461/58A GB910185A (en) | 1958-07-22 | 1958-07-22 | Improvements in or relating to transmission gearing of twin-engined hub-driven, coaxial, contrarotative aircraft-lifting or/and-sustaining rotors |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB23461/58A GB910185A (en) | 1958-07-22 | 1958-07-22 | Improvements in or relating to transmission gearing of twin-engined hub-driven, coaxial, contrarotative aircraft-lifting or/and-sustaining rotors |
Publications (1)
Publication Number | Publication Date |
---|---|
GB910185A true GB910185A (en) | 1962-11-14 |
Family
ID=10196002
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB23461/58A Expired GB910185A (en) | 1958-07-22 | 1958-07-22 | Improvements in or relating to transmission gearing of twin-engined hub-driven, coaxial, contrarotative aircraft-lifting or/and-sustaining rotors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB910185A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3364681A (en) * | 1965-08-24 | 1968-01-23 | Clarence D. Glover | Power plant |
EP0068677A1 (en) * | 1981-06-17 | 1983-01-05 | WESTLAND plc | Transmission systems |
DE3729231A1 (en) * | 1987-09-02 | 1989-03-16 | Hans Mueller | VTOL (vertical take-off and landing) aircraft |
-
1958
- 1958-07-22 GB GB23461/58A patent/GB910185A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3364681A (en) * | 1965-08-24 | 1968-01-23 | Clarence D. Glover | Power plant |
EP0068677A1 (en) * | 1981-06-17 | 1983-01-05 | WESTLAND plc | Transmission systems |
US4484491A (en) * | 1981-06-17 | 1984-11-27 | Westland Plc | Transmission systems |
DE3729231A1 (en) * | 1987-09-02 | 1989-03-16 | Hans Mueller | VTOL (vertical take-off and landing) aircraft |
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