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Hub-mounted actuators for blade pitch collective control
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Copyright Year | 1985 |
| Description | Blade collective pitch control is provided for a rotor system by rotary actuators located between adjacent blades. Each actuator is connected to the leading edge of one adjacent blade and the trailing edge of the other adjacent blade. |
| File Size | 518064 |
| Page Count | 8 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_20080005894 |
| Archival Resource Key | ark:/13960/t2t48kb6m |
| Language | English |
| Publisher Date | 1985-11-26 |
| Access Restriction | Open |
| Subject Keyword | Aircraft Propulsion And Power Patents Actuators Rotors Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Patent |