Abstract: A temperature control device (e.g., a thermostat) may be configured to control an internal heat-generating electrical load so as to accurately measure a present temperature in a space around the temperature control device. The temperature control device may comprise a temperature sensing circuit configured to generate a temperature control signal indicating the present temperature in the space, and a control circuit configured to receive the temperature control signal and to control the internal electrical load. The control circuit may be configured to energize the internal electrical load in an awake state and to cause the internal electrical load to consume less power in an idle state. The control circuit may be configured to control the internal electrical load to a first energy level (e.g., a first intensity) during the awake state and to a second energy level (e.g., second intensity) that is less than the first during the idle state.

Abstract: A helicopter windshield defogger and/or deicer system is discussed which is connectable with a high pressure, high temperature air supply from the compression stage of a helicopter turbine engine. The system utilizes a coanda ejector type nozzle to mix and distribute high temperature bleed air and aspirated cabin air to a dispersal shroud fixed adjacent to the helicopter windshield.