A shock absorber assembly having a wheel assembly including first and second coupling points, and first and second shock absorber elements. Each shock absorber element includes a housing portion defining a bore, and a rod slidably coupled within the bore such that the shock absorber element has a variable length. Each rod is coupled to a respective coupling point of the wheel assembly. The shock absorber assembly is arranged to maintain the relative positions of the first and second housing portions such that the longitudinal axis of the first bore has a generally fixed relationship with respect to the longitudinal axis of the second bore.

A wheel suspension system for mounting a wheel on a vehicle body, such as a flying car, the system comprising: an upright assembly for mounting the wheel; a lower arm assembly comprising: a lower control arm; and a storage arm; a mounting structure connecting the lower arm assembly to the upright assembly; an upper control arm; and an adjustable suspension assembly pivotally connected to the upright assembly or lower control arm assembly and pivotally connected to the body; wherein one end of the lower control arm is pivotally connected to the body, and the other end of the lower control arm is connected to the mounting structure to be pivotable about a first axis; the mounting structure is connected to the upright assembly to be pivotable about a second axis that is substantially perpendicular to the first axis; the storage arm is pivotally connected to the lower control arm at one end, and is moveably connected to the body under control of an actuator at the other end; and the upper control arm having a pivot connection to an upper part of the upright assembly at one and, and a pivot connection to the body at the other end; and wherein the lateral position of the upright assembly with respect to the body is adjustable by movement of the actuator of the storage arm with respect to the body, and the vertical position of the upright assembly with respect to the body is adjustable by operation of the adjustable suspension assembly.

An aircraft landing gear assembly (112) including a shock absorber strut (114), a bogie (120), a link assembly (124), and a movement detector (132). The shock absorber strut includes an upper and a lower telescoping parts (118, 116), the upper part being connectable to the airframe of an aircraft and the lower part being connected to the bogie. The link assembly extends between the upper and lower telescoping parts. The movement detector detects movement of the link assembly relative to the bogie. The movement detector includes: a piston (138) arranged such that relative movement between the link assembly and the bogie causes relative movement of the piston within a cylinder (136); fluid which flows as a result of relative movement between the piston and the cylinder; and a flow sensor (184) arranged to sense a change in flow due to movement of the piston within the cylinder.

A shock absorber for a vehicle includes a cylinder and a piston, a portion of which slidably disposed with the cylinder. A magnetic target is fixedly positioned relative to the piston, and a sensor is fixedly positioned relative to the cylinder. The sensor generates a signal according to the position of the magnet target relative to the sensor.

An aerocar with a dual mode suspension system configured to operate in a roadable mode and a flight mode. The aerocar may include a front suspension assembly having a front axle, and a rear suspension assembly having a rear axle. A conduit system provides a hydraulic fluid in fluid communication between the front suspension assembly and the rear suspension assembly. An auxiliary hydraulic fluid reservoir is provided in fluid communication with the conduit system, and configured to selectively maintain or interrupt fluid communication between the front suspension assembly and the rear suspension assembly to adjust damping of the front suspension assembly. A controller may be provided, configured to direct the flow of hydraulic fluid from the rear suspension assembly to the front suspension assembly, for example, when a stroke of the rear suspension exceeds a predetermined value during landing.