Abstract: An apparatus for thermal treatment of coatings on substrates includes a microwave applicator cavity; a microwave power supply to deliver power to the cavity; a thermally insulated microwave-transparent compartment within the cavity, large enough to contain the coated substrate while occupying no more than 50% of the total volume of the cavity; a means of supporting the coated substrate within the compartment; an adjustable IR heating source in the compartment and facing the substrate so that a selected amount of IR heating may be applied to the substrate; and, a non-contacting temperature measurement device to measure the temperature of the coating. Related methods for using the apparatus to process different kinds of films are also disclosed.

Abstract: An apparatus for thermal treatment of coatings on substrates includes a microwave applicator cavity; a microwave power supply to deliver power to the cavity; a thermally insulated microwave-transparent compartment within the cavity, large enough to contain the coated substrate while occupying no more than 50% of the total volume of the cavity; a means of supporting the coated substrate within the compartment; an adjustable IR heating source in the compartment and facing the substrate so that a selected amount of IR heating may be applied to the substrate; and, a non-contacting temperature measurement device to measure the temperature of the coating. Related methods for using the apparatus to process different kinds of films are also disclosed.

Abstract: A method and control system for modulating a starter turbine (14) speed to a predetermined reference speed to prevent crash engagement with a turbine engine (16) during restart. The turbine engine (16) is coupled to the starter turbine (14) by a ratchet and pawl clutch (17), and crash engagement is prevented by modulating the starter turbine (14) speed to the predetermined reference speed, which is below a minimum pawl engagement speed, until the pawls have locked-in. A control system (10) in accordance with the present invention includes an electronic control (18) section and a mechanical pneumatic actuation means (20) which operate to limit the speed of the starter turbine (14) to the predetermined reference speed which is below the minimum speed at which crash engagements occur. The electronic control (18) provides an adjustment signal (26) corresponding to the difference between a sensed starter turbine speed signal (24) and a reference speed signal (49).