Abstract: An apparatus is disclosed for monitoring the temperature of the propulsion gas at the inlet to a turbine wheel in a turbine in which a compressor fuels air into a chamber where it is heated and the heated products exiting the chamber form the propulsion gas. The temperature of the heated products exiting the chamber is a function of the inlet static and total pressure, the total inlet temperature, the static pressure of the heated products and the static pressure drop across the chamber.

Abstract: A measuring system has a pair of sensors with the response time of one sensor lagging the response time of the other. The output of each sensor is sampled periodically and the outputs for two successive samples are compared to calculate the actual value of the parameters based upon the change in the two outputs.

Abstract: The damper system for controlling the flow of a gaseous fluid in a duct member is disclosed in which the combination of parallel and opposed flow characteristics is utilized to produce a composite rate of flow which varies substantially linearly with the angle of rotation of the damper blades over the full opening range. A plurality of damper blades pivotally mounted in substantially louvered fashion is utilized in one embodiment in which alternate pairs of blades are rotated in opposite directions to produce alternate parallel and opposed passage flow characteristics. In addition to being linear, the alternate parallel and opposed flow characteristics of the adjacent blade systems of the damper provide an additive advantage in mixing flow from different streams each being provided with one of the dampers. This can be produced by combining the alternate swirling and sheet flow of the damper openings in a manner which produces intermeshing of the flow and complete mixing of the two streams.