Abstract: Fixtures for releasably holding a sensor having a first sensor portion and a second sensor portion, methods for making such fixtures, and methods for installing a sensor harness, are provided. In one example, a fixture includes a clip portion that is configured to hold a first sensor portion of a sensor. A support portion is coupled to and extends away from the clip portion. An arm portion is coupled to and extends away from the support portion. The arm portion is configured to hold a second sensor portion of the sensor. The fixture has a frangible seam formed therein that ruptures in response to an applied force for removing the fixture from the sensor.

Abstract: Fixtures for releasably holding a sensor having a first sensor portion and a second sensor portion, methods for making such fixtures, and methods for installing a sensor harness, are provided. In one example, a fixture includes a clip portion that is configured to hold a first sensor portion of a sensor. A support portion is coupled to and extends away from the clip portion. An arm portion is coupled to and extends away from the support portion. The arm portion is configured to hold a second sensor portion of the sensor. The fixture has a frangible seam formed therein that ruptures in response to an applied force for removing the fixture from the sensor.

Abstract: An arrangement for supplying heated air to a wing anti-icing system on an aircraft propelled by a jet engine includes, but is not limited to, an ejector that is configured for coupling to a wing anti-icing system. The ejector is further configured to receive a first flow of air, to entrain a second flow of air with the first flow of air, the second flow of air having a lower temperature than the first flow of air, to mix the first flow of air with the second flow of air to form a combined flow having a temperature and a volume suitable for use by the wing anti-icing system, and to exhaust the combined flow into the wing anti-icing system.

Abstract: An arrangement for supplying heated air to a wing anti-icing system on an aircraft propelled by a jet engine includes, but is not limited to, an ejector that is configured for coupling to a wing anti-icing system. The ejector is further configured to receive a first flow of air, to entrain a second flow of air with the first flow of air, the second flow of air having a lower temperature than the first flow of air, to mix the first flow of air with the second flow of air to form a combined flow having a temperature and a volume suitable for use by the wing anti-icing system, and to exhaust the combined flow into the wing anti-icing system.