Abstract: Liquid fuel from a rotary fluid trap is atomized by a sharp edge on an inside surface of an aft cavity of a bladed rotor of a gas turbine engine and directed into each of a plurality of associated hollow blades through corresponding blade inlet ducts that are in fluid communication with corresponding aft hollow interior portions of each blade. A radially-extending central rib within each blade partitions the hollow interior thereof into aft and forward hollow interior portions that are in fluid communication through an associated opening in the central rib and through a radially-extending gap between the central rib and the interior surface of the blade. A blade outlet duct provides for fluid communication between the forward hollow interior portion and a forward cavity of the bladed rotor, and a rotor outlet duct provides for discharging the fuel from a radially-inboard portion of the forward cavity.

Abstract: Fuel (12) is supplied to a rotatable portion (118) of a gas turbine engine (10) comprising a rotor (24) and at least one blade (26, 26.1) operatively coupled thereto, so as to provide for cooling at least one of the rotor (24) or the at least one blade (26, 26.1) by transforming the fuel (12) to a vapor or gaseous state. The fuel (12) is discharged in a vapor or gaseous state from the rotatable portion (118) directly into a combustion chamber (16) of the gas turbine engine (10).

Abstract: Liquid fuel from a rotary fluid trap is atomized by a sharp edge on an inside surface of an aft cavity of a bladed rotor of a gas turbine engine and directed into each of a plurality of associated hollow blades through corresponding blade inlet ducts that are in fluid communication with corresponding aft hollow interior portions of each blade. A radially-extending central rib within each blade partitions the hollow interior thereof into aft and forward hollow interior portions that are in fluid communication through an associated opening in the central rib and through a radially-extending gap between the central rib and the interior surface of the blade. A blade outlet duct provides for fluid communication between the forward hollow interior portion and a forward cavity of the bladed rotor, and a rotor outlet duct provides for discharging the fuel from a radially-inboard portion of the forward cavity.

Abstract: Two vehicles are transported in tandem by a beam assembly connecting a lead vehicle to a trailing vehicle which is reversed end-for-end. The beam assembly includes an elongated beam which is connected to the rear and extends lengthwise of the trailing vehicle. The beam extends beyond the rear end of the trailing vehicle and is elevated and connected to the rear end of the lead vehicle at a height such that the rear wheels of the trailing vehicle are raised above ground. The connection of the beam to the lead vehicle permits the beam to swing both laterally and vertically.

Abstract: Two vehicles are transported in tandem by a beam assembly connecting a lead vehicle to a trailing vehicle which is reversed end-for-end. The beam assembly includes an elongated beam which is connected to the rear and extends lengthwise of the trailing vehicle. The beam extends beyond the rear end of the trailing vehicle and is elevated and connected to the rear end of the lead vehicle at a height such that the rear wheels of the trailing vehicle are raised above ground. The connection of the beam to the lead vehicle permits the beam to swing both laterally and vertically.