Abstract: A skin treatment product and method includes steps of detoxifying cleansing, tightening, and moisturizing skin, by applying bentonite paste, followed by a skin moisturizer, to provide improved skin health and appearance. A single packaging contains bentonite paste and the skin moisturizer. The bentonite paste may be applied in a first step to extract oils, toxins, bacteria and other materials from the skin. After the bentonite paste dries and is removed, the moisturizer is applied to the skin, preferably a vitamin and/or mineral infused moisturizer. In one embodiment, the skin moisturizer is in the form of a skin mask. Following moisturizing the skin, a third step may be to nourish the skin. The skin treatment may be applied to facial skin, feet, hands, or any skin surface.

Abstract: A skin treatment product and method includes steps of detoxifying cleansing, tightening, and moisturizing skin, by applying bentonite paste, followed by a skin moisturizer, to provide improved skin health and appearance. A single packaging contains bentonite paste and the skin moisturizer. The bentonite paste may be applied in a first step to extract oils, toxins, bacteria and other materials from the skin. After the bentonite paste dries and is removed, the moisturizer is applied to the skin, preferably a vitamin and/or mineral infused moisturizer. In one embodiment, the skin moisturizer is in the form of a skin mask. Following moisturizing the skin, a third step may be to nourish the skin. The skin treatment may be applied to facial skin, feet, hands, or any skin surface.

Abstract: An engine nacelle comprised of a top portion with hinges and a composite fan cowl pivotally connected to the top portion by the hinges. The composite fan cowl comprises a core with a hinge zone having a first thickness and a body zone having a second thickness. The hinge zone includes the hinges. The body zone is distal from the hinge zone, and the first thickness is less than the second thickness.

Abstract: An engine nacelle comprised of a top portion with hinges and a composite fan cowl pivotally connected to the top portion by the hinges. The composite fan cowl comprises a core with a hinge zone having a first thickness and a body zone having a second thickness. The hinge zone includes the hinges. The body zone is distal from the hinge zone, and the first thickness is less than the second thickness.

Abstract: A disk for a turbine engine is disclosed herein. The disk includes a rotatable body extending along a longitudinal axis between a forward side and an aft side. The disk also includes a plurality of slots disposed about a periphery of the body. Each of the slots extends between the forward and aft sides along a respective slot axis. The sides of each of the slots are asymmetrical relative to one another in a cross-section normal to the slot axis.

Abstract: A disk for a turbine engine is disclosed herein. The disk includes a rotatable body extending along a longitudinal axis between a forward side and an aft side. The disk also includes a plurality of slots disposed about a periphery of the body. Each of the slots extends between the forward and aft sides along a respective slot axis. The sides of each of the slots are asymmetrical relative to one another in a cross-section normal to the slot axis.

Abstract: A system and method for supplying cooling air to the turbine section of a gas turbine. The system may include a compressed air supply, an ambient air supply, and an ejector for entraining the ambient air supply with the compressed air supply to form a cooling air supply. In a gas turbine including a compressor section and a turbine section, the method may include extracting compressed air from the compressor section, entraining ambient air with the compressed air to form cooling air, and directing the cooling air to the turbine section.