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US 9,822,709 B2Granted
Pneumatic control valve
AssigneePHD, Inc.
InventorNelson Broman
Life of this patent
Estimating the term…
Abstract
A control valve for a gas turbine engine air starter. The control valve includes a spherical or ball valve element rotatable between a closed position and an open position to connect an internal flow passage to the air starter. A series of camming elements interconnecting a piston and a valve stem for the spherical valve element convert linear displacement of the piston into rotational movement of the valve for rapid opening.
Claims14
A control valve for fluid flow, said control valve comprising:
- a valve body having an inlet passage and an aligned outlet passage, and an interconnecting chamber;
- a valve element positioned within said interconnecting chamber and having a through flow passage, said valve element being rotatable about a valve body axis between an open position in which the through flow passage aligns with and connects said inlet and outlet passages in said valve body and a closed position in which said valve element blocks flow between said inlet and outlet passages;
- a stem extending from said valve body coaxial with said valve body axis;
- a housing receiving said stem;
- and
- a piston displaceable within said housing in a direction parallel to an axis of said stem, said housing, said piston and said stem having inter-engaging camming elements for connecting the linear displacement of said piston along said valve body axis into rotation of said stem and said valve element between said open and closed positions, wherein said housing has at least one pin extending inward and said piston has a first slot receiving said at least one housing pin, and said stem has at least one stem pin extending outward from said stem and said piston has a second slot receiving said at least one stem pin for rotating said stem as said piston is displaced in said direction parallel to the axis of said stem, wherein said first and second slots each form a spiral configuration and converge at a common point.
3 more elements
A gas turbine power plant comprising:
- a gas turbine engine;
- a pneumatic starter mechanically connected to said gas turbine engine to drive said gas turbine engine into rotation;
- a source of pressurized fluid;
- and,
- a control valve for selectively connecting the pressurized fluid to said pneumatic starter, said control valve comprising a valve body having an inlet passage and aligned outlet passage and an interconnecting chamber, a valve element being positioned within the interconnecting chamber and having a through flow passage and rotatable about a valve body axis between an open position in which the through flow passage aligns with and connects the inlet and outlet passages in the valve body and a closed position in which the valve element blocks flow between the inlet and outlet passages, a rotatable stem extending from the valve body and coaxial with the valve body axis, said control valve including a housing receiving the rotatable stem and a piston displaceable within the housing in a direction parallel to an axis of the rotatable stem, the housing, the piston and the rotatable stem having inter-engaging camming elements for converting the linear displacement of the piston along said valve body axis into rotation of said rotatable stem and valve element between the closed and open positions, wherein said housing has at least one pin extending inward and said piston has a first slot receiving said at least one housing pin, and said rotatable stem has at least one pin extending outward and said piston has a second slot receiving said at least one stem pin for rotating said rotatable stem as said piston is displaced in said direction parallel to the axis of said rotatable stem, wherein said first and second slots each form a spiral configuration and converge at a common point.
2 more elements
Dependencies are inferred from the claim text.