Abstract: A deflector assembly in a cooking appliance door includes a fin with a directing flange and a projection. The projection extends toward the central panel and is configured to concentrate cool air flow within the channels of the cooking appliance door. The directing flange cooperates with a tab to define a single opening through which the cool air is concentrated and directed toward an upper portion of the cooking appliance door.

Abstract: A vent assembly for use with an oven. The vent assembly includes polymeric end caps that are ultrasonically molded to a metal bracket. The metal bracket is coupled to a lower fin and an upper fin. The polymeric end caps include support surfaces for holding sections of the lower fin, the upper fin, and the metal bracket.

Abstract: A ventilation system for an oven is provided. The system includes a rear duct assembly. The rear duct assembly includes vertical walls defining a vertical air flow path along a rear of the oven, and a separator plate dividing the vertical air flow path into a first air flow configured to receive air from oven electronics and a second air flow configured to receive air from an oven cavity. The separator plate extends vertically downward between the vertical walls from the top of the vertical air flow path a portion of the height of the oven until a mixing zone at the rear of the oven into which the first and second air flows combine into a combined air flow.

Abstract: A cooking appliance is provided that includes a casing defining a cooking cavity. The casing includes a top wall defining an aperture. A supporting member has an inner surface and defines an air channel and a sealed chamber with a first opening and a second opening. The second opening is aligned with the aperture of the top wall of the casing. A fan is coupled to the casing and is configured to selectively supply airflow along the inner surface. An imaging device assembly is positioned within the air channel of the supporting member and is aligned with the first opening of the chamber to view the cavity. The imaging device assembly is configured to seal the first opening. A transparent member is positioned proximate the second opening and is configured to seal the second opening.

Abstract: Coupling for inducing high temperature drops on parts of an aircraft includes an edge portion (2) subjected to high temperature and a bearing structure (3) having limited capacity to resist against high temperatures. The coupling includes at least one hinge (4) having low heat conductivity.