Pattern factor control valve
AssigneeJansen's Aircraft Systems Control., Inc.
InventorHarvey Jansen
Life of this patent
Estimating the term…
Abstract
A fuel valve for use in regulating the pattern factor of a gas turbine has a highly accurate pressure balanced clevis valve assembly. The clevis valve is pivotally mounted inside the valve housing by a flexure pivot, and has a pair of legs at each side of a valve body that control flow through pairs of flow orifices. An armature mounts to the clevis valve, and when energized, an electromagnet inside the valve housing generates magnetic flux that moves the armature to pivot the clevis valve to open or closed the orifices. The clevis valve is inherently balanced and can meter fuel through multiple orifices simultaneously.
Claims20
A fuel valve for a turbine, the valve comprising:
- a valve housing having an inlet port and an outlet port;
- a valve body disposed within the valve housing and defining a passageway and a pair of orifices in communication with the inlet and outlet ports;
- a clevis valve member having at least two spaced apart prongs located adjacent to the valve body to interrupt flow through the orifices when the clevis valve member is in a closed position so as to prevent flow from the inlet port to the outlet port;
- a flexure pivot having a first end mounted to the housing and having a second end movable relative to the first end and coupled to the clevis valve member to permit the clevis valve member to pivot between the closed position and an open position in which the prongs open the orifices to permit flow from the inlet port to the outlet port;
- and
- a drive assembly for effecting movement of the clevis valve member between the open and closed positions.
A fuel valve for a turbine, the valve comprising:
- a valve housing defining a fuel flow path between an inlet port and an outlet port;
- a valve body disposed within the valve housing in the fuel flow path and defining a passageway and a pair of orifices in communication with the fluid flow path;
- a clevis valve member having at least two spaced apart prongs located adjacent to the valve body to interrupt flow through the orifices when the clevis valve member is in a closed position so as to prevent flow from the inlet port to the outlet port;
- a flexure pivot having a first end mounted to the housing and having a second end movable relative to the first end and coupled to the clevis valve member to permit the clevis valve member to pivot between the closed position and an open position in which the prongs open the orifices to permit flow from the inlet port to the outlet port;
- and
- a magnetic drive assembly having an electromagnet and an armature coupled to one of the flexure pivot second end and the clevis valve member to effect pivoting of the clevis valve member between the open and closed positions, wherein the drive assembly is disposed within the valve housing in the fuel flow path.
A fuel valve for a turbine, the valve comprising:
- a valve housing having an inlet port and an outlet port;
- a valve body disposed within the valve housing defining a passageway and having two opposite sides with orifices in communication with the inlet and outlet ports;
- and
- a clevis valve member having at least two spaced apart prongs that straddle the valve body so that at least one prong is located at each of the two opposite sides of the valve body so that the clevis valve member is pressure balanced about the valve body, the clevis valve member being pivotally mounted within the valve housing so as to pivot relative to the valve body between an open position in which the prongs are at least partially clear of the orifices and a closed position in which the prongs essentially close off flow through the orifices so as to prevent flow from the inlet port to the outlet port.
Dependencies are inferred from the claim text.