| abstract |
An air suspension system comprising a manifold defining first and second ports each defining a receiving area at a second end, the first and second ports being arranged in a common plane, a a channel intersecting the first and second ports, a cavity intersecting each port and a pressure sensor port between the first and second ports, wherein the pressure sensor port defines a sensor insertion perpendicular to the common plane shaft, the pressure sensor interface is spaced by a thickness from the first interface, the second interface and the channel; a first and second solenoid valve, each solenoid valve is arranged in the cavity coaxially with the first and second interfaces , each solenoid valve includes a connector; a pressure sensor arranged in the pressure sensor interface, the pressure sensor includes a connector; and an electronic module arranged in parallel with the common plane, the electronic module is arranged to be connected with the connector electrical connection. |