Sampling system for moving fluid
AssigneeThe United States of America as represented by the Secretary of the Navy
InventorGeorge A. Andrews, Jr.
Life of this patent
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Abstract
A system for sampling a moving fluid utilizes a housing in the shape of an airfoil having a leading edge adapted to be disposed in the moving fluid such that the moving fluid will initially encounter the leading edge. A fluid flow pathway extends through the airfoil. One or more sampling ports are formed in the airfoil on the airfoil's high pressure side. Each sampling port is in fluid communication with the fluid flow pathway. The system can also have one or more control ports formed on the low pressure side of the airfoil. Each control port is in fluid communication with the fluid flow pathway. The housing can be mounted to experience two rotational degrees of freedom, and can have an aerodynamic tail assembly coupled thereto.
Claims12
A system for sampling a moving fluid, comprising:
- a housing in the shape of an airfoil having a leading edge adapted to be disposed in a moving fluid such that the moving fluid will initially encounter the leading edge of the airfoil wherein a high pressure side and a low pressure side of the airfoil are established such that a pressure differential develops therebetween, the housing further having a fluid flow pathway defined therein that extends through the airfoil;
- and
- at least one sampling port formed in the airfoil on the high pressure side, each sampling port in fluid communication with the fluid flow pathway, wherein each sampling port comprises an adjustable-sized opening in the housing.
A system for sampling a moving fluid, comprising:
- a housing in the shape of an airfoil having a leading edge adapted to be disposed in a moving fluid such that the moving fluid will initially encounter the leading edge of the airfoil wherein a high pressure side and a low pressure side of the airfoil are established such that a pressure differential develops therebetween, the housing further having a fluid flow pathway defined therein that extends trough the airfoil to a collection zone;
- at least one sampling port formed in the airfoil on the high pressure side, each sampling port in fluid communication with the fluid flow pathway;
- at least one control port formed in the airfoil on the low pressure side and aft of the sampling port, each control port in fluid communication with the fluid flow pathway;
- and
- mounting means coupled to the housing for permitting the housing to experience two rotational degrees of freedom thereabout, wherein a portion of the moving fluid is drawn into each sampling port and travels through the fluid flow pathway to the collection zone.
A system for sampling a moving fluid, comprising:
- a housing in the shape of an airfoil having a leading edge adapted to be disposed in a moving fluid such that the moving fluid will initially encounter the leading edge of the airfoil wherein a high pressure side and a low pressure side of the airfoil are established such that a pressure differential develops therebetween, the housing further having a fluid flow pathway defined therein that extends through the airfoil to a collection zone;
- at least one adjustable-sized sampling port formed in the airfoil on the high pressure side, each sampling port in fluid communication with the fluid flow pathway;
- at least one adjustable-sized control port formed in the airfoil on the low pressure side and aft of the sampling port, each control port in fluid communication with the fluid flow pathway;
- mounting means coupled to the housing for permitting the housing to experience two rotational degrees of freedom thereabout, wherein a portion of the moving fluid is drawn into each sampling port and travels through the fluid flow pathway to the collection zone;
- and
- an aerodynamic tail assembly coupled to the housing and adapted to be disposed in the moving fluid, the aerodynamic tail assembly interacting with the moving fluid to thereby cause the housing to rotate about the mounting means wherein the leading edge of the airfoil is positioned to initially encounter the moving fluid.
Dependencies are inferred from the claim text.