Abstract: A subassembly of a gas turbine engine includes a heat shield and carrier subassembly for a turbine section are disclosed. The carrier includes support features to couple to an engine casing. The upstream end of the carrier includes a radially inward arm extending toward to an engine axis. The outer end of the radially floating heat shield is coupled to the radially inward arm via a pin-and-slot joint configured to allow movement of the heat shield relative to the radially inward arm of the carrier. In response to thermal expansion and contraction of the vane, the heat shield is configured to move radially outward and inward, respectively, relative to the radially inward arm to maintain contact with the outer platform of the vane.

Abstract: A catalyst for the hydroformylation of at least one olefin, having a ligand fo the general formula (1)—R1, R2, R3 selected from the group including substituted and non-substituted alkyl, substituted and non-substituted aryl, substituted and non-substituted alkenyl, substituted and non-substituted alkinyl, substituted and non-substituted cycloalkyl, and substituted and non-substituted heterocycles, wherein R1, R2 and R3 can each be the same or different, L is selected from a group having a sandwich complex, an oxygen group, substituted and non-substituted alkylene or heterocycles, and substituted aryl or heteroaryl; and aryl and heteroaryl is each substituted with groups which contain at least two heteroatoms and are coupled to the Si via the at least two heteroatoms of the substituents, ?n=1-10, preferably 1-5, particularly preferably 1, 2, or 3; and the ligand is coupled to the metal M from the group VIIIb of the periodic table of elements via the Si group.

Abstract: Systems and methods for reducing heat exposure of a turbine casing in a gas turbine engine may be provided. The system may include a blade track coupled with a turbine casing with a clip. The system may further include a nozzle guide vane coupled to the turbine casing. A cavity may be formed by an end of the blade track, the clip, and a portion of the nozzle guide vane. A heat shield may be positioned between the clip and the end of the blade track in the cavity such that an edge of the heat shield and the portion of the nozzle guide vane form a gap. The heat shield and the nozzle guide vane may be positioned such that the gap closes in response to the heat shield and the nozzle guide vane thermally expanding.

Abstract: A subassembly of a gas turbine engine includes a heat shield and carrier subassembly for a turbine section are disclosed. The carrier includes support features to couple to an engine casing. The upstream end of the carrier includes a radially inward arm extending toward to an engine axis. The outer end of the radially floating heat shield is coupled to the radially inward arm via a pin-and-slot joint configured to allow movement of the heat shield relative to the radially inward arm of the carrier. In response to thermal expansion and contraction of the vane, the heat shield is configured to move radially outward and inward, respectively, relative to the radially inward arm to maintain contact with the outer platform of the vane.

Abstract: A motor vehicle front end crash-load carrying structure has at least one side rail on each side of the vehicle extending in the vehicle longitudinal direction, an A-pillar extending upward from the side rail, and a reinforcement extending between the A-pillar and the side rail. The reinforcement is made up of a longitudinally-extending rear element fixed to the A-pillar and extending forward therefrom outboard of the side rail, and a transversely-extending forward element fixed to and extending inboard from a forward end of the rear element, an inboard end of the forward element abutting an outboard surface of the side rail. The rear element extends substantially parallel with a vehicle longitudinal axis and defines a concave-downward wheel arch. The rear element may include an engineered bending site adjacent to a joint between the rear element and the forward element. The reinforcement may be supported on a suspension mount.

Abstract: A motor vehicle front end crash-load carrying structure has at least one side rail on each side of the vehicle extending in the vehicle longitudinal direction, an A-pillar extending upward from the side rail, and a reinforcement extending between the A-pillar and the side rail. The reinforcement is made up of a longitudinally-extending rear element fixed to the A-pillar and extending forward therefrom outboard of the side rail, and a transversely-extending forward element fixed to and extending inboard from a forward end of the rear element, an inboard end of the forward element abutting an outboard surface of the side rail. The rear element extends substantially parallel with a vehicle longitudinal axis and defines a concave-downward wheel arch. The rear element may include an engineered bending site adjacent to a joint between the rear element and the forward element. The reinforcement may be supported on a suspension mount.

Abstract: A fuel element storage and cooling configuration includes a fuel element storage pool and a cooling system having at least one first heat exchanger disposed in the fuel element storage pool and at least one second heat exchanger disposed in a heat sink and located at a distance therefrom, above a highest point of the first heat exchanger. The two heat exchangers are connected, using a pipe system, to form a closed circuit, which is at least partially filled with a flowable coolant. If the temperature of the first heat exchanger is increased with respect to the second heat exchanger, natural circulation of the coolant, and thus heat transport from the fuel element storage pool to the heat sink, is ensured without a pump apparatus.

Abstract: A transport securing device of an aircraft gas turbine includes a securing element, which at its two end areas is each provided with a first and a second connecting element, with the first connecting element being designed to be suitable for fastening to a front suspension device and the second connecting element being designed to be suitable for fastening to a rear suspension device of an aircraft gas turbine.

Abstract: The present invention relates to a transport securing device of an aircraft gas turbine with a securing element, which at its two end areas is each provided with a first and a second connecting element, with the first connecting element being designed to be suitable for fastening to a front suspension device and the second connecting element being designed to be suitable for fastening to a rear suspension device of an aircraft gas turbine.

Abstract: A package including a stack of tissue paper sheets, wherein the package includes at least one line of weakness that has an unbroken configuration and a broken configuration and wherein the package is configured to be able to be flexed to pull apart the line of weakness when the line of weakness is in the broken configuration to open the package to allow a tissue paper sheet in the stack to be withdrawn through the open package.

Abstract: A system including a dry absorbent tissue paper sheet dispenser having a dispensing opening through which dry tissue paper sheets can be withdrawn and a moist sheet dispenser having a dispensing opening through which moist sheets can be withdrawn, wherein one of the dry tissue paper dispenser and the moist sheet dispenser is configured to sit atop the other so that the dispensing openings face in opposing directions in a combined configuration, and wherein the dry and moist sheet dispensers have cooperating interfacing surfaces when they are in the combined configuration that resist movement of the moist sheet dispenser with respect to the dry tissue paper dispenser in a first direction perpendicular to a sheet withdrawal direction of the dry tissue paper dispenser and the moist dispenser.

Abstract: A moist dispenser, the moist sheet dispenser including a receptacle housing for receiving a stack of moist sheets, the receptacle housing including a dispensing opening through which a sheet can be withdrawn from the stack, the dispenser including a lid that has an open position to provide access to the dispensing opening so that a sheet can be withdrawn from the stack through the dispensing opening and a closed position covering the dispensing opening, wherein the lid defines a periphery and the receptacle housing defines a periphery and the peripheries of the lid and the receptacle housing meet when the lid is in the closed position.

Abstract: A stack of interfolded tissue paper sheets, wherein the interfolding pattern is such that each sheet is folded at least once to provide leading and trailing panels with respect to a sheet withdrawal direction, to define a stack comprising an overlapping region where adjacent sheets in the stack overlap and non-overlapping regions of the stack on opposed sides of the overlapping region wherein adjacent sheets of the stack do not overlap.

Abstract: A container for containing a stack of interfolded tissue paper sheets, wherein the container includes a dispensing opening and lips so that a sheet passes through the dispensing opening when being withdrawn from the stack and dispensed from the sheet, wherein the lips are in an overlapping state in a direction of withdrawal of the sheets, wherein the lips are configured to be opened into a less overlapping or non-overlapping state by the sheet as the sheet moves therethrough and are configured to return to the overlapping state after withdrawal of the sheet.

Abstract: A fuel element storage and cooling configuration includes a fuel element storage pool and a cooling system having at least one first heat exchanger disposed in the fuel element storage pool and at least one second heat exchanger disposed in a heat sink and located at a distance therefrom, above a highest point of the first heat exchanger. The two heat exchangers are connected, using a pipe system, to form a closed circuit, which is at least partially filled with a flowable coolant. If the temperature of the first heat exchanger is increased with respect to the second heat exchanger, natural circulation of the coolant, and thus heat transport from the fuel element storage pool to the heat sink, is ensured without a pump apparatus.