Title:
遠隔装置の制御及び電力供給
Document Type and Number:
Japanese Patent JP2012503574
Kind Code:
A
Abstract:
An actuator controller with a power supply that steps down a high voltage for use by remote auxiliary loads in an aircraft is provided. A high voltage power bus running through the aircraft may use high gage or smaller diameter wiring, resulting in weight savings in the power bus. A control network running through the aircraft may use fiber optic cabling, providing further weight reductions. An actuator controller may receive the high voltage from the power bus and provide a lower voltage to a remote device. The actuator controller may facilitate communication between the control network and the remote device. The integration of control and power supply may enhance endurance, reliability, and enable localized calibration of the remote device. Modular wing components may include interface controllers, high and low power busswork, and remote devices. The modular wing components may include power and control interconnections.
More Like This:
Inventors:
Secrist, William, Stuart
Application Number:
JP2011529184A
Publication Date:
February 09, 2012
Filing Date:
September 23, 2009
Export Citation:
Assignee:
AEROVIRONMENT, INC.
International Classes:
B64C13/50; B64D47/00
Domestic Patent References:
| JP2010514603A | 2010-05-06 | |||
| JP2007015423A | 2007-01-25 | |||
| JP2008526620A | 2008-07-24 | |||
| JPH0937482A | 1997-02-07 |
Foreign References:
| WO2008063271A1 | 2008-05-29 |
Attorney, Agent or Firm:
Shigeru Ito