Unitized high temperature probes
AssigneeThe United States of America as represented by the Secretary of the Air Force
InventorsFrederick J. Komanetsky, John A. Selstad
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Abstract
A unitized static sensor probe 20 for a gas turbine engine 10, machined from a single piece of raw material. The probe preferably has integral kiel cups 26 that form a part of the probe airfoil. The probe is manufactured by electrical discharge machining, and is shaped with an airfoil (53, 70) that minimizes disruption of the engine airstream. Integral air seal platforms 56, 58 and a mounting plate 54 are also provided.
Claims12
An instrumentation probe for holding and shielding static sensors in a flow stream, the instrumentation probe comprising:
- (a) a probe body, aerodynamically shaped to be non-disruptive of the flow stream and manufactured from a single piece of metal;
- (b) multiple kiel heads protruding into the flow stream in order to shield static sensors, the kiel heads formed as an integral part of said probe body and having smooth transitioning outer surfaces connecting said kiel heads to said probe body;
- (c) an instrumentation cavity formed within said probe body,
- (d) static sensors positioned within said instrumentation cavity and said kiel heads;
- (e) a mounting flange forming a part of said probe body for mounting said instrumentation in the flow stream;
- and
- (f) an exit area for sensor leads to facilitate connection of said sensors to data recording means.
An instrumentation probe comprising a single piece metallic probe body which comprises an aerodynamically shaped probe airfoil and at least two kiel cups protruding into a flow stream for shielding static instrumentation and wherein the kiel cups are formed integral with said probe airfoil, wherein said probe body comprises a multibranched internal instrumentation cavity and is formed by electrical discharge machining of a single piece of raw material.
Dependencies are inferred from the claim text.