Fluid module

A fluid module configured to be connected to an aircraft, comprising:

• a manifold configured to direct fluid flow from a first inlet to an outlet, the outlet configured to be connected to a hydraulic system of the aircraft and the first inlet configured to be connected to a ground fluid source, wherein the ground fluid source is a ground cart, the manifold comprising:
• a filter port adapted to receive a filter unit;
• the first inlet in fluid communication with the filter port;
• and
• the outlet in fluid communication with the filter port.

A fluid module configured to be connected to an aircraft, comprising:

• a manifold configured to direct fluid flow from a first inlet to an outlet, the outlet configured to be connected to a hydraulic system of the aircraft and the first inlet configured to be connected to a ground fluid source, the manifold comprising:
• a filter port adapted to receive a filter unit;
• the first inlet in fluid communication with the filter port;
• the outlet in fluid communication with the filter port;
• a first coupling at the first inlet;
• a fluid connection interface at the outlet;
• a second inlet connected to a second coupling, the first inlet configured to be connected to a first fluid source and the second inlet configured to be connected to a second fluid source, the first fluid source and the second fluid source having different pressures;
• and
• a flange extending from a main body of the manifold, the flange comprising a third coupling configured to be connected to the ground fluid source to provide return fluid from the aircraft to the ground fluid source.

A fluid module configured to be connected to an aircraft, comprising:

• a manifold including:
• a filter port adapted for mounting a filter unit to the manifold;
• a first inlet in fluid communication with the filter port;
• a second inlet;
• and
• an outlet in fluid communication with the filter port;
• wherein the manifold has a cylindrical body, the first inlet and the outlet located on the cylindrical body of the manifold;
• a first coupling connected to the first inlet;
• a second coupling connected to the second inlet;
• a third coupling;
• wherein the manifold includes a flange and the third coupling is connected to the flange;
• a fluid interface connected to the outlet;
• and
• a second fluid interface;
• wherein the fluid interface and the second fluid interface are disposed at a first side of the manifold;
• and
• the first coupling, the second coupling, and the third coupling are disposed at a second side of the manifold,
• wherein the flange is planar and extends axially from an axial end of the manifold.

A fluid module configured to be connected to an aircraft, comprising:

• a manifold including:
• a filter port adapted for mounting a filter unit to the manifold;
• a first inlet in fluid communication with the filter port;
• a second inlet;
• and
• an outlet in fluid communication with the filter port;
• a first coupling connected to the first inlet;
• a second coupling connected to the second inlet;
• wherein the first coupling and the second coupling extend from a body of the manifold at an angle relative to each other;
• a third coupling;
• wherein the manifold includes a flange and the third coupling is connected to the flange;
• a fluid interface connected to the outlet;
• and
• a second fluid interface;
• wherein the fluid interface and the second fluid interface are disposed at a first side of the manifold;
• and
• the first coupling, the second coupling, and the third coupling are disposed at a second side of the manifold.