Methods of moving an aircraft undercarriage that is movable between a retracted position and a deployed position generally include: using a rotary electromechanical type drive actuator coupled to a portion of the aircraft undercarriage to raise it from the deployed position to the retracted position; disengaging the drive actuator during a descent of the undercarriage from the retracted position to the deployed position and using a hydraulic linear shock absorber coupled to a portion of the undercarriage to regulate the rate of descent and to absorb shock on arrival of the undercarriage in the deployed position; and neutralizing the shock absorber while raising the undercarriage.

A damping force generation structure includes a damping force generation mechanism, and a damping force adjustment mechanism. The damping force adjustment mechanism includes a drive mechanism configured to be able to drive the valve body, and a coupling member having a first end fixed to the drive mechanism and a second end fixed to the fixing member, thereby coupling the drive mechanism and the fixing member. At least one of a position of the damping force generation mechanism relative to the fixing member, a position of the coupling member relative to the fixing member, and a position of the drive mechanism relative to the coupling member is adjustable in the advancing and retracting direction of the valve body by a position adjustment mechanism.

An oscillation damper includes a damper inner pipe with a damper inner pipe wall thickness and a damper inner pipe outer wall. A piston rod and piston are reciprocally movable in the damper inner pipe. The damper inner pipe is divided into a piston-rod-side operating space and an operating space remote from the piston rod. A damper outer pipe has a damper outer pipe wall thickness and a damper outer pipe inner wall. The damper outer pipe is arranged around the damper inner pipe and the damper outer pipe is fluidly connected to the damper inner pipe at the side of the operating space remote from the piston rod. The oscillation damper includes support elements arranged between the damper outer pipe inner wall and the damper inner pipe outer wall wherein the damper inner pipe is at least partially supported with respect to the damper outer pipe.

An oscillation damper includes a damper inner pipe with a damper inner pipe wall thickness and a damper inner pipe outer wall. A piston rod and piston are reciprocally movable in the damper inner pipe. The damper inner pipe is divided into a piston-rod-side operating space and an operating space remote from the piston rod. A damper outer pipe has a damper outer pipe wall thickness and a damper outer pipe inner wall. The damper outer pipe is arranged around the damper inner pipe and the damper outer pipe is fluidly connected to the damper inner pipe at the side of the operating space remote from the piston rod. The oscillation damper includes support elements arranged between the damper outer pipe inner wall and the damper inner pipe outer wall wherein the damper inner pipe is at least partially supported with respect to the damper outer pipe.

A modified shock absorber for tiltable vehicles, with means to maintain the vertical of the vehicle without offering resistance to the extension movements during tilting maneuvers.

An adjustment control for adjusting a damping curve of a shock absorber includes an aperture seat coupled to a base of the shock absorber. The aperture seat defines a flow tube. A plug, in mechanical communication with a spring, slidably engages the flow tube. A plug nut is threadably coupled to an adjustment nut shaft stud and is in mechanical communication with the spring. An adjustment nut is coupled to the base. The adjustment nut has a non-circular cavity to receive at least a portion of the adjustment nut shaft stud and at least a portion of the non-circular region of the plug nut such that the plug nut cannot rotate relative to the non-circular cavity of the adjustment nut. An adjustment knob causes rotation of the adjustment nut shaft stud. The rotation of the adjustment nut shaft stud causes axial movement of the plug nut.

A shock absorbing apparatus includes a flexible membrane defining an accumulator cavity, and a compression assembly defining a compression cavity. The compression assembly is disposed within the flexible membrane such that viscous fluid contained within the cavities may be exchanged therebetween by a damping orifice, fluid conduit and or valve mechanism. The accumulator cavity deforms in response to the application of a transmitted impact load, and is capable of storing and releasing potential energy in response to the application and cessation of the transmitted impact load.

A rigid substructure (12) tied to a restrained column (16) at different floors undergoes rigid body rotation due to lateral dynamic loading. Flexural members (18) that are connected to the substructure (12) and another anchor column (14) resist the rigid body rotation and undergo vertical deflections. Damped diagonals (20) connected to common nodes of the rigid substructure and flexural members, for one embodiment, receive amplified displacements and more effectively dissipate energy. Flexural members restore the structure to the unloaded position. The system does not require moment connections and can work with flexure induced in simply supported beams. The system is highly effective and may remain elastic under maximum considered earthquake ground motions.

A structure having at least one generally horizontal flexural member extending between a pair of spaced-apart, upright columns, is protected from seismic forces by connecting one end of an elongated damping member to a first structural node on one of the columns, and by connecting an opposite end to a nodal junction on the flexural member. An undamped, rigid body is connected to the nodal junction and to a second structural node on the other of the columns. In response to the seismic forces, the rigid body is turned about the second structural node, the flexural member is flexed, an amplified force is exerted, and the damping member is displaced along an amplified working stroke.

A structure having at least one generally horizontal flexural member extending between a pair of spaced-apart, upright columns, is protected from seismic forces by connecting one end of an elongated damping member to a first structural node on one of the columns, and by connecting an opposite end to a nodal junction on the flexural member. An undamped, rigid body is connected to the nodal junction and to a second structural node on the other of the columns. In response to the seismic forces, the rigid body is turned about the second structural node, the flexural member is flexed, an amplified force is exerted, and the damping member is displaced along an amplified working stroke.