Abstract: A method for managing a financing or lease of a product and/or service, the method executing on a computing device, the method including: receiving a price of the product to be financed or leased; receiving an amount of the price of the product to be financed; selecting a rate card; determining a current finance rate based upon the rate card that is selected; selecting a purchase option for the product and/or service; selecting a contract term of the financing or lease related to the purchase or lease the product and/or service; determining a payment amount for the product based on the inputted price of the product to be financed or leased, the amount of the price of the product to be financed, the current finance rate, the purchase option selected, and the term of the financing or lease selected; and displaying the payment amount that is determined.

Abstract: Nozzles and nozzle assemblies for gas turbine engines are provided. A nozzle includes an airfoil having an exterior surface defining a pressure side and a suction side extending between a leading edge and a trailing edge, an outer band disposed radially outward of the airfoil, the outer band including a radially outwardly-facing end surface, and an inner band disposed radially inward of the airfoil, the inner band including a radially inwardly-facing end surface. The nozzle further includes a flange extending radially from one of the radially outwardly-facing end surface or the radially inwardly-facing end surface. The flange is formed from a ceramic matrix composite material and includes a plurality of ceramic matrix composite plies stacked together and generally having an L-shape in a circumferential cross-sectional view.

Abstract: An airfoil assembly for a gas turbine engine and a method of transferring load from the ceramic matrix composite (CMC) airfoil assembly to a metallic vane assembly support member are provided. The airfoil assembly includes a forward end and an aft end with respect to an axial direction of the gas turbine engine. The airfoil assembly further includes a radially outer end component including a radially outwardly-facing end surface having a non-compression load-bearing feature extending radially outwardly from the outwardly-facing end surface and formed integrally with the outer end component, the feature configured to mate with a complementary feature formed in a radially inner surface of a first airfoil assembly support structure, the feature selectively positioned orthogonally to a force imparted into the airfoil assembly.

Abstract: A method for managing a financing or lease of a product and/or service, the method executing on a computing device, the method including: receiving a price of the product to be financed or leased; receiving an amount of the price of the product to be financed; selecting a rate card; determining a current finance rate based upon the rate card that is selected; selecting a purchase option for the product and/or service; selecting a contract term of the financing or lease related to the purchase or lease the product and/or service; determining a payment amount for the product based on the inputted price of the product to be financed or leased, the amount of the price of the product to be financed, the current finance rate, the purchase option selected, and the term of the financing or lease selected; and displaying the payment amount that is determined.