Speed limiting turbine with momentum activated bypass valve
View Patent ↗A speed limiting mechanism for a turbine-driven fluid distribution apparatus usable with compressible fluid such as compressed air and incompressible fluid such as water. In one form, a flow restrictor is located in the turbine discharge flow path, with the turbine discharge port area selected in relation to the turbine inlet port area according to the desired turbine speed with compressed air. In another form, the incoming fluid flows downstream along the surface of the turbine stator, and is then diverted to enter the rotor chamber in the proper direction. A bleed area on the stator which permits a portion of a compressible fluid which has expanded as it flows along the stator surface to flow to bypass the turbine rotor. In another embodiment, a valve may be provided upstream from the turbine to selectively divert at least a portion of the pressurized fluid around the turbine when the pressurized fluid air or a combination of air and water.
1. A sprinkler, comprising:
a riser for receiving a pressurized fluid;
a nozzle;
a mounting device configured to mount the nozzle at an upper end of the riser for rotation about an axis;
a turbine mounted for rotation inside the riser and in fluid communication with the pressurized fluid;
a drive device connected between the turbine and the nozzle such that rotation of the turbine by the pressurized fluid will rotate the nozzle;
a first valve positioned upstream from the turbine and configured to selectively re-direct at least a portion of the pressurized fluid around the turbine when the pressurized fluid is air or a mixture of water and air the first valve including:
a valve seat positioned adjacent to the inlet of the turbine chamber;
a central opening formed in the valve seat in fluid communication with an area upstream of the turbine chamber;
a valve member movably mounted in the first valve and configured to move from a closed position in which it directs the pressurized fluid to bypass the turbine chamber and an open position in which it directs the pressurized fluid into the turbine chamber; and
a second valve positioned upstream from the first valve and configured to maintain a desired pressure differential across the turbine.
2. The sprinkler of claim 1 , wherein the turbine further comprises:
a stator positioned downstream of an inlet of a turbine chamber in which the turbine is mounted;
a rotor position downstream of the stator and rotatably mounted in the turbine chamber, wherein the pressurized fluid is directed by the stator to the rotor to rotate the rotor to turn the drive device.
3. The sprinkler of claim 1 , wherein the first valve further comprises a biasing element configured to bias the valve member in the closed position until sufficient force is applied to a bottom surface of the valve member by the pressurized fluid to overcome a bias force of the biasing element and to move the valve member into the open position to allow the pressurized fluid to flow into the turbine chamber.
4. A sprinkler comprising:
a turbine in fluid communication with a pressurized fluid, the turbine driven to rotate by the pressurized fluid; and
a valve positioned upstream from the turbine and configured to selectively re-direct at least a portion of the pressurized fluid around the turbine when the pressurized fluid is air or a mixture of water and air:
the valve including:
a first valve element biased into a first position to direct at least a portion of a flow of the pressurized fluid toward the turbine to provide a desired pressure, and
a second valve element positioned downstream from the first valve element and biased in a bypass position by a biasing element to direct the flow of pressurized fluid from the first valve element around the turbine, a biasing force of the biasing element set such that the second valve element moves into a second position to direct the flow of pressurized fluid toward the turbine when the pressurized fluid does not include air such that a force applied by the pressurized fluid on the second valve element is larger than the biasing force.