Resources Contact Us Home
Landing gear

Image Number 18 for United States Patent #8104711.

An auxiliary actuator (49) comprises a two stage telescopic hydraulic unit comprising first (59, 63) and second (56, 50) stage piston and cylinder actuators operating coaxially within an outer casing (50). A respective actuator is connected to a respective one of the strut (1) and bogie beam (4). The second stage actuator (56, 60) serves to control the tilt position of the bogie beam (4) relative to the strut (1). The second stage actuator (56. 60), when in the retracted position with the first stage actuator (59, 63) in the extended position, limits the length ol the auxiliary actuator (9) between its connections (62,67) to the strut (1) and bogie beam (4), so as to assume a predetermined intermediate length in which the bogie beam (4) is restrained to tilt about the auxiliary pivot (14) and thereby lengthens the landing gear during take-off.

  Recently Added Patents
Method and system for utilizing native ethernet as a virtual memory interconnect
Fuel cell and a method of manufacturing a fuel cell
Medical injector
Mobile communication device monitoring systems and methods
Integrating map-reduce into a distributed relational database
Method and system for automatically hiding irrelevant parts of hierarchical structures in computer user interfaces
  Randomly Featured Patents
Garbage collection extensibility via managed code
Outboard motor
Apparatus and method for controlling packet data to provide multimedia broadcast/multicast services in a CDMA mobile communication system
Brushless polyphase DC motor
Signalling in a digital mobile communications system
Three-way media recommendation method and system
Surface of a headlight assembly
Method for providing online submission of requests for proposals for forwarding to identified vendors
Waist bag
Transducer suspension system with high conductivity leads having two layers