Resources Contact Us Home
Flight control surface actuation system with redundantly configured and lockable actuator assemblies

Image Number 4 for United States Patent #7607611.

A flight control surface actuator assembly includes a pair of flight control surface actuators and a pivot arm. One of the flight control surface actuators is coupled to a flight control surface and a static airframe structure, the other flight control surface actuator is coupled to the flight control surface and the pivot arm. The pivot arm coupled to the static airframe structure and is configured to pivot relative to the second flight control surface actuator and the static airframe structure.

  Recently Added Patents
Method of and apparatus for evaluating an optimal irradiation amount of an electron beam for drawing a pattern onto a sample
System and method for predicting remaining useful life of device components
Model matching for trace link generation
Method and apparatus for supporting management actions for very high throughput in wireless communications
Porous polymeric resins
Tailoring the band gap of solar cells made of liquid silane by adding germanium
  Randomly Featured Patents
Combination spent shell deflector and catcher, and breech block actuator
Process for the removal of cyanide and other impurities from solution
Apparatus and method for booting NAND flash memory of a mobile terminal
Ball target assembly
Non monetary coin
Organ-specific targeting of cationic amphiphile/DNA complexes for gene therapy
Method and device for transferring spin-polarized charge carriers
Deformation resistance welding of sheet metal, tubes, and similar shapes
DVC as generic file format for plenoptic camera
CVD apparatus equipped with moisture monitoring