GB230190A - Improvements in helicopters - Google Patents
Improvements in helicoptersInfo
- Publication number
- GB230190A GB230190A GB30945/23A GB3094523A GB230190A GB 230190 A GB230190 A GB 230190A GB 30945/23 A GB30945/23 A GB 30945/23A GB 3094523 A GB3094523 A GB 3094523A GB 230190 A GB230190 A GB 230190A
- Authority
- GB
- United Kingdom
- Prior art keywords
- shafts
- propellers
- planes
- casings
- propeller
- 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
- B64C27/08—Helicopters with two or more rotors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/22—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft
- B64C27/26—Compound rotorcraft, i.e. aircraft using in flight the features of both aeroplane and rotorcraft characterised by provision of fixed wings
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
Abstract
230,190. Armstrong, J. J. V., (Eerliner, H. A.). Dec. 10, 1923. Aeroplanes; helicopters; planes, arrangement of; propelling; steering.-A helicopter having one or more separate propellers arranged at the tail away from the centre of lift to control the tilting of the machine fore and aft, has oppositely rotating lifting-propellers, spaced from each other and having their axes normally parallel, one or both of these propelers being adapted to be tilted the one relatively to the other in a plane or planes at right angles to the plane normally containing the axes of the propellers in order to produca a horizontal steering-couple. A machine is described similar to that shown in Specification 204,079, having three superposed planes above which two propellers are mounted' on shafts in casings which can turn about a transverse tube containing the driving shaft. The propellershafts are connected to the driving shaft by bevel gear contained in the casings. The Figure shows the upper ends of the propeller-shafts 7, 8, connected by cables to four levers 18. 18<a>, 18<b>, 18<c>, on shafts carrying quadrants connected to an endless cable 24. This cable is connected by a lever 22 and a rod 21 to a rudder bar 20 which also actuates a rudder through cables 25, 26. Instead of pivoted casings being used, the propeller shafts may be mounted on planes made sufficiently warpable to permit the movement of the shafts. The propeller shafts may be mounted on the longitudinal centre line of the machine instead of transversely as shown.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB30945/23A GB230190A (en) | 1923-12-10 | 1923-12-10 | Improvements in helicopters |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB30945/23A GB230190A (en) | 1923-12-10 | 1923-12-10 | Improvements in helicopters |
Publications (1)
Publication Number | Publication Date |
---|---|
GB230190A true GB230190A (en) | 1925-03-10 |
Family
ID=10315562
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB30945/23A Expired GB230190A (en) | 1923-12-10 | 1923-12-10 | Improvements in helicopters |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB230190A (en) |
-
1923
- 1923-12-10 GB GB30945/23A patent/GB230190A/en not_active Expired
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