Garrison et al., 2006 - Google Patents
Two-fault tolerant electric actuation systems for space applicationsGarrison et al., 2006
- Document ID
- 16929693626765970473
- Author
- Garrison M
- Steffan S
- Publication year
- Publication venue
- 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit
External Links
Snippet
Conventional mechanical feedback and servo-valve commanded hydraulic actuation technology has been used reliably in aerospace and industrial applications for many years; however these systems are facing increasing competition from “more” or all electric …
- 238000005516 engineering process 0 abstract description 12
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/42—Transmitting means with power amplification using fluid pressure having duplication or stand-by provisions
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/50—Transmitting means with power amplification using electrical energy
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/24—Transmitting means
- B64C13/26—Transmitting means without power amplification or where power amplification is irrelevant
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US5074495A (en) | Load-adaptive hybrid actuator system and method for actuating control surfaces | |
Garrison et al. | Two-fault tolerant electric actuation systems for space applications | |
Wang et al. | Commercial Aircraft Hydraulic Systems: Shanghai Jiao Tong University Press Aerospace Series | |
US7191593B1 (en) | Electro-hydraulic actuator system | |
Li et al. | A review of electromechanical actuation system for more electric aircraft | |
US8567715B2 (en) | Flight control system for an aircraft | |
US11603209B2 (en) | Aviation hydraulic propulsion system utilizing secondary controlled drives | |
CN110374946B (en) | Hydraulic system for an aircraft | |
US11313391B2 (en) | Actuator system for a fly-by-wire aircraft | |
CN110374944B (en) | Aircraft hydraulic system with dual spool valve and method of use | |
Li et al. | Review on electro-hydrostatic actuator: System configurations, design methods and control technologies | |
CN103661940A (en) | Independent blade control system with hydraulic cyclic control | |
CN110374952B (en) | Aircraft hydraulic system with dual slide valves and method of use | |
US20180274563A1 (en) | Aircraft Hydraulic Systems Having Shared Components | |
CN103661939A (en) | Independent blade control system with hydraulic pitch link | |
Rubertus et al. | Electromechanical actuation technology for the all-electric aircraft | |
CN113357233A (en) | Control surface actuator assembly, aircraft hydraulic system including same, and associated aircraft and method | |
EP2354008A1 (en) | Turbine powered electromechanical actuation system | |
CN103569358A (en) | Independent blade control system with rotary blade actuator | |
US10570936B2 (en) | Symmetrically loaded dual hydraulic fly-by-wire actuator | |
EP2927506A1 (en) | Pneumatic positioning system | |
Li et al. | Review of Aerospace Actuator Technology | |
Borello et al. | Flap control systems actuators: mathematical and computational model for dynamic simulation | |
EP3453892B1 (en) | Electric hydraulic actuation system for a safety critical application | |
CN103661941B (en) | There is the radial fluid device of variable phase and amplitude |