Military vehicle
A military vehicle includes a brake positioned to facilitate braking a tractive element, a brake housing defining an inner volume, a piston separating the inner volume into a first chamber and a second chamber, a rod extending through an end of the brake housing and coupled to the piston where the rod is positioned to selectively engage with the brake to inhibit movement of the tractive element, a resilient member positioned within the inner volume and configured to generate a biasing force against the piston such that the rod is biased into engagement with the brake, and an air-to-hydraulic intensifier coupled to the brake housing. The air-to-hydraulic intensifier is configured to receive a supply of air and provide a hydraulic fluid to the brake housing based on the supply of air to overcome the biasing force to disengage the rod from the brake to permit movement of the tractive element.
1. A military vehicle comprising:
a chassis;
an axle coupled to the chassis
a tractive element coupled to the axle;
a brake positioned to facilitate braking the tractive element;
a brake housing defining an inner volume;
a piston separating the inner volume into a first chamber and a second chamber;
a rod extending through an end of the brake housing and coupled to the piston, the rod positioned to selectively engage with the brake to inhibit movement of the tractive element;
a resilient member positioned within the inner volume and configured to generate a brake biasing force against the piston such that the rod is biased into engagement with the brake;
an air-to-hydraulic intensifier coupled to the brake housing, the air-to-hydraulic intensifier configured to receive a supply of air and provide a hydraulic fluid to the brake housing based on the supply of air to overcome the brake biasing force to disengage the rod from the brake to permit movement of the tractive element;
a valve positioned between the air-to-hydraulic intensifier and the brake housing; and
a hydraulic reservoir fluidly coupled to the valve and the air-to-hydraulic intensifier;
wherein the valve includes a first port fluidly coupled to the air-to-hydraulic intensifier, a second port fluidly coupled to the hydraulic reservoir, a third port fluidly coupled to the brake housing, and a valve gate that is repositionable between a first position and a second position, the first position coupling the first port to the third port to fluidly couple the air-to-hydraulic intensifier to the brake housing, the second position coupling the second port to the third port to fluidly couple the hydraulic reservoir to the brake housing.
2. The military vehicle of claim 1 , wherein the air-to-hydraulic intensifier includes a hydraulic pump.
3. The military vehicle of claim 1 , wherein the valve includes:
an air pilot positioned at a first end of the valve gate; and
a biasing element positioned at an opposing second end of the valve gate, the biasing element configured to provide a valve biasing force to the valve gate to bias the valve gate into the second position.
4. The military vehicle of claim 3 , wherein the brake biasing force of the resilient member is configured to bias the piston to force the hydraulic fluid out of the brake housing, through the valve, and into the hydraulic reservoir in response to the valve being in the second position.
5. The military vehicle of claim 3 , further comprising an air supply line coupled to the air-to-hydraulic intensifier and the air pilot, the air supply line configured to provide the supply of air to the air-to-hydraulic intensifier and the air pilot.
6. The military vehicle of claim 5 , wherein the supply of air provided to the air pilot overcomes the valve biasing force to reposition the valve gate into the first position to place the air-to-hydraulic intensifier into fluid communication with the brake housing to facilitate disengaging the brake.
7. A brake system comprising:
a brake configured to facilitate braking a tractive element;
a brake housing defining an inner volume;
a piston separating the inner volume into a first chamber and a second chamber;
a rod extending through an end of the brake housing and coupled to the piston, the rod positioned to selectively engage with the brake to inhibit movement of the tractive element;
a resilient member positioned within the inner volume and configured to generate a brake biasing force against the piston such that the rod is biased into engagement with the brake;
an air-to-hydraulic intensifier coupled to the brake housing, the air-to-hydraulic intensifier configured to receive a supply of air and provide a hydraulic fluid to the brake housing based on the supply of air to overcome the brake biasing force to disengage the rod from the brake to permit movement of the tractive element;
a valve positioned between the air-to-hydraulic intensifier and the brake housing; and
a hydraulic reservoir fluidly coupled to the valve and the air-to-hydraulic intensifier;
wherein the valve includes a first port fluidly coupled to the air-to-hydraulic intensifier, a second port fluidly coupled to the hydraulic reservoir, a third port fluidly coupled to the brake housing, and a valve gate that is repositionable between a first position and a second position, the first position coupling the first port to the third port to fluidly couple the air-to-hydraulic intensifier to the brake housing, the second position coupling the second port to the third port to fluidly couple the hydraulic reservoir to the brake housing.
8. The brake system of claim 7 , wherein the air-to-hydraulic intensifier includes a hydraulic pump.
9. The brake system of claim 7 , wherein the valve includes:
an air pilot positioned at a first end of the valve gate; and
a biasing element positioned at an opposing second end of the valve gate, the biasing element configured to provide a valve biasing force to the valve gate to bias the valve gate into the second position.
10. The brake system of claim 9 , wherein the brake biasing force of the resilient member is configured to bias the piston to force the hydraulic fluid out of the brake housing, through the valve, and into the hydraulic reservoir in response to the valve being in the second position.
11. The brake system of claim 9 , further comprising an air supply line coupled to the air-to-hydraulic intensifier and the air pilot, the air supply line configured to provide the supply of air to the air-to-hydraulic intensifier and the air pilot.
12. The brake system of claim 11 , wherein the supply of air provided to the air pilot overcomes the valve biasing force to reposition the valve gate into the first position to place the air-to-hydraulic intensifier into fluid communication with the brake housing to facilitate disengaging the brake.
13. A military vehicle comprising:
a brake configured to facilitate braking a tractive element;
a brake housing defining an inner volume;
a piston separating the inner volume into a first chamber and a second chamber;
a rod extending through an end of the brake housing and coupled to the piston, the rod positioned to selectively engage with the brake to inhibit movement of the tractive element;
a resilient member positioned within the inner volume and configured to generate a brake biasing force against the piston to bias the rod into engagement with the brake;
a hydraulic reservoir;
an air-to-hydraulic intensifier coupled to the brake housing, the air-to-hydraulic intensifier configured to receive a supply of air and provide a hydraulic fluid to the brake housing based on the supply of air to overcome the brake biasing force to disengage the rod from the brake to permit movement of the tractive element;
a valve including:
a first port fluidly coupled to the air-to-hydraulic intensifier;
a second port fluidly coupled to the hydraulic reservoir;
a third port fluidly coupled to the brake housing;
a valve gate that is repositionable between a first position and a second position, the first position coupling the first port to the third port to fluidly couple the air-to-hydraulic intensifier to the brake housing, the second position coupling the second port to the third port to fluidly couple the hydraulic reservoir to the brake housing;
an air pilot; and
a biasing element configured to provide a valve biasing force to the valve gate to bias the valve gate into the second position; and
an air supply line configured to provide the supply of air to the air-to-hydraulic intensifier and the air pilot;
wherein the brake biasing force of the resilient member is configured to bias the piston to force the hydraulic fluid out of the brake housing, through the valve, and into the hydraulic reservoir in response to the valve being in the second position.
14. The military vehicle of claim 13 , wherein the supply of air provided to the air pilot overcomes the valve biasing force to reposition the valve gate into the first position to place the air-to-hydraulic intensifier into fluid communication with the brake housing to facilitate disengaging the brake.