Abstract: An aircraft is disclosed, including a fuselage having a compartment configured to house refueling apparatus. An auxiliary power unit is mounted in the compartment.

Abstract: An aircraft is disclosed, including a fuselage having a compartment configured to house refueling apparatus. An auxiliary power unit is mounted in the compartment.

Abstract: An aircraft is disclosed, including a fuselage having a compartment configured to house refueling apparatus. An auxiliary power unit is mounted in the compartment.

Abstract: A stowable computer workstation (“SCW”) for a workplace within a vehicle is described, where the workplace has an inner sidewall of the vehicle. The SCW may include a video display mount assembly and a deployment support attached to the video display mount assembly. The deployment support is configured to deploy and stow the video display mount assembly against the inner sidewall and the deployment support is secured to the inner sidewall.

Abstract: A stowable computer workstation (“SCW”) for a workplace within a vehicle is described, where the workplace has an inner sidewall of the vehicle. The SCW may include a video display mount assembly and a deployment support attached to the video display mount assembly. The deployment support is configured to deploy and stow the video display mount assembly against the inner sidewall and the deployment support is secured to the inner sidewall.

Abstract: A stowable computer workstation (“SCW”) for a workplace within a vehicle is described, where the workplace has an inner sidewall of the vehicle. The SCW may include a video display mount assembly and a deployment support attached to the video display mount assembly. The deployment support is configured to deploy and stow the video display mount assembly against the inner sidewall and the deployment support is secured to the inner sidewall.

Abstract: A stowable computer workstation (“SCW”) for a workplace within a vehicle is described, where the workplace has an inner sidewall of the vehicle. The SCW may include a video display mount assembly and a deployment support attached to the video display mount assembly. The deployment support is configured to deploy and stow the video display mount assembly against the inner sidewall and the deployment support is secured to the inner sidewall.

Abstract: A nose landing gear assembly for an airplane which can be launched with catapult assistance. The landing gear assembly includes a nose strut, upper drag link, lower drag link, launch bar and launch bar actuator. When the nose shut is in the extended position, the upper drag link, lower drag link and launch bar form a direct load path between the catapult shuttle and the airplane thereby avoiding subjecting the nose strut to loads reacted from the shuttle. The nose strut, launch bar, launch bar actuator and airplane fuselage form a first four bar linkage. Furthermore, the nose strut, upper drag link, lower drag link and airplane fuselage form a second four bar linkage such that during retraction of the nose strut, the launch bar, launch bar linkage, upper drag link and lower drag link are caused to move up and into the airplane wheel well.