A shock or vibration absorption device, comprising: (1) a housing comprising a spring-guiding surface; (2) a piston positioned within the housing and comprising a spring-engagement surface, wherein the piston is configured to move relative to the housing in response to an applied force; and (3) a closed-loop resilient element positioned between the spring-engagement surface of the piston and the spring-guiding surface of the housing such that a ring axis of the resilient element is substantially parallel to a direction of the applied force; wherein the resilient element is configured to absorb kinetic energy as the piston moves relative to the housing in response to the applied force.

According to the present invention, there is disclosed a torque impact mitigator including a hydraulic cylinder having a compression end and a rebound end. A piston rod mounted to the piston and extends out from the hydraulic cylinder through the first end cap. A compression spring is compressed when the piston rod is moved out of the hydraulic cylinder and in a relaxed state when the piston rod is moved towards a second end cap. Bores through the piston allow the passage of hydraulic fluid from the rebound end to the compression end of the cylinder. A relief valve is secured to the piston within the rebound end to momentarily reduce the pressure of the hydraulic fluid caused by an instantaneous hydraulic pressure increase due to the initial movement of the piston from the rebound end to the compression end.

A container system including an outer shell, a deck disposed within the outer shell and configured to support cargo, and at least one vibration isolator member to support the deck within the outer shell and reduce or dampen a transfer of shock or vibration to the deck. Each vibration isolator member includes a hollow, flexible body configured to resiliently compress in response to a force. At least one fastener interface secures the flexible body to the bottom wall or to the deck. The hollow, flexible body has one or more apertures to allow fluid flow into and out of an inner cavity of the flexible body during compression or expansion.

A method for monitoring a dual-stage, separated gas/fluid shock strut includes receiving, by a controller, a primary chamber temperature sensor reading, a primary chamber pressure sensor reading, and a shock strut stroke sensor reading, calculating, by the controller, a secondary chamber nominal pressure based upon the primary chamber temperature sensor reading, determining, by the controller, a shock strut stroke associated with the secondary chamber nominal pressure, calculating, by the controller, a volume of oil in an oil chamber, a volume of gas in a primary gas chamber, a number of moles of gas in the primary gas chamber, a volume of oil leaked into the primary gas chamber, a volume of gas in a secondary chamber, and a number of moles of gas in the secondary chamber.

A method for monitoring a dual-stage, separated gas/fluid shock strut includes receiving, by a controller, primary chamber temperature and pressure sensor readings, secondary chamber pressure and temperature sensor readings, and a shock strut stroke sensor reading, determining, by the controller, a shock strut stroke at which a secondary chamber is activated, calculating, by the controller, a volume of oil in an oil chamber of the shock strut, a primary chamber gas volume of, a number of moles of gas in, and a volume of oil leaked into, a primary gas chamber of the shock strut, a secondary chamber gas volume in, a volume of oil leaked into, and a number of moles of gas in, the secondary chamber, based upon at least one of the secondary chamber pressure sensor reading, and the secondary chamber temperature sensor reading.

Shock and vibration isolators and their use to isolate loads from vibration and shock, where the isolators include a fluid spring assembly and a mechanical spring assembly, where the fluid spring assembly and the mechanical spring assembly are arranged in series. The mechanical spring assembly includes a first spring and a second spring arranged so that compression of the mechanical spring assembly simultaneously directly compresses the first spring and indirectly compresses the second spring via an intermediate actuator, such that the first and second spring are compressed in parallel.

Provided is a damper that exerts a damping force with a simple structure using elastically deformable granular bodies.

The damper includes a cylinder, a piston, a rod, a rod guide, and a plurality of granular bodies. The piston is housed in the cylinder and reciprocates in the central axis direction of the cylinder. The rod is connected to the piston. The rod extends in the central axis direction of the cylinder and protrudes to an outside from an open end side of the cylinder. The rod guide is fixed to the open end of the cylinder. The rod guide has a through hole which penetrates in the central axis direction of the cylinder and through which the rod is reciprocably inserted. The granular bodies are elastic bodies each having a spherical shape. The granular bodies are filled in the cylinder.

A method for servicing a dual-stage, separated gas/fluid shock strut may comprise measuring a servicing temperature, charging a secondary gas chamber with compressed gas, wherein a secondary chamber pressure corresponds to the servicing temperature, pumping oil into the shock strut, and charging a primary gas chamber with compressed gas.

A damping stopper is interposed between two members axially displaced relative to each other and is provided with an elastic body which, when the interval between the two members decreases, is axially compressed by the two members and expands radially outward. In the elastic body, a second member suppressing the expansion is located in one axial region and attached to the outer periphery. When axially compressed by the two members, the elastic body expands while receiving resistance by the second member. The expanding elastic body contacts the side wall of one of the two members.

A dual-stage, separated gas/fluid shock strut arrangement includes a dual-stage, separated gas/fluid shock strut, a pressure/temperature sensor mounted to the primary gas chamber, a stroke sensor, and a monitoring system, comprising a recorder configured to receive a plurality of sensor readings from at least one of the pressure/temperature sensor and the stroke sensor, a landing detector configured to detect a landing event based upon a stroke sensor reading received from the stroke sensor, and a health monitor configured to determine a volume of oil in the oil chamber, a volume of gas in the primary gas chamber, and a volume of gas in the secondary gas chamber.