Abstract: Routing technologies are disclosed. A described technology includes routing packets through a network based on backpressure scheduling; when a number of packets in a transmitter queue satisfies a first threshold, retaining copies of at least a portion of the packets; and once the number of packets in the transmitter queue satisfies a second threshold, transmitting the retained copies of the packets to perform the routing. Retaining the copies can include copying a packet from the transmitter queue into a duplicate buffer when the number of packets in the transmitter queue is below the first threshold.

Abstract: A blower assembly includes a motor cover having (1) a body portion defining a motor cavity, (2) an air flow guide surface connected to an end of the body portion, the guide surface extending radially outwardly from the body portion, and (3) a cooling duct integrally formed with the body portion and having an inlet and an outlet, the inlet being located at the end of the body portion and the outlet being defined in a sidewall of the body portion. The blower assembly further includes a motor positionable in the motor cavity, the motor having a motor shaft having a central axis. In addition, the blower assembly includes a fan housing is connected to the motor cover, wherein (1) the fan housing defines a scroll cut-off line, and (2) a plane passes through the scroll cut-off line and the central axis, and (3) the cooling duct is positioned adjacent to the plane.

Abstract: A vehicle fan assembly for circulating air to cool an engine. The fan assembly has a central hub; an outer, circumferential ring with an inner surface disposed around the hub; a plurality of blades, each blade having a root connected to the hub, a tip connected to the inner surface of the ring, and a span between the root and the tip, the blades extending generally radially outward from the hub to the ring; and at least one bladelet having a base connected to the inner surface of the ring, a free end, and a span between the base and the free end. Preferably, a plurality of bladelets are disposed alternately with the blades on the inner surface of the ring around the circumference of the ring. The span of each bladelet is about 40% to 50% of the span of the blades. The tips of the blades and the bases of the bladelets are connected to the ring over the full width of the blades and the bladelets, respectively. Finally, each bladelet has a planform with an elliptical profile.

Abstract: A blade for a vehicle engine-cooling fan assembly. The blade combines a particular distribution of four, key, blade-design parameters--planform sweep, airfoil chord, maximum airfoil camber, and airfoil pitch angle--to achieve a fan assembly having high pumping, high efficiency, and low noise. Specifically, the blade has a planform with a forward sweep angle continuously increasing in absolute value along the span from the root to a maximum absolute value not exceeding about 15 degrees at the tip. The airfoil of the blade has a chord that continuously increases from the root to the tip, a maximum camber that continuously decreases from a value not greater than about 12% of chord at the root to a value not less than about 5% of chord at the tip, and a solidity not greater than about 1.1 at the root and not less than about 0.5 at the tip.

Abstract: A blower assembly includes a motor cover having (1) a body portion defining a motor cavity, (2) an air flow guide surface connected to an end of the body portion, the guide surface extending radially outwardly from the body portion, and (3) a cooling duct integrally formed with the body portion and having an inlet and an outlet, the inlet being located at the end of the body portion and the outlet being defined in a sidewall of the body portion. The blower assembly further includes a motor positionable in the motor cavity, the motor having a motor shaft having a central axis. In addition, the blower assembly includes a fan housing is connected to the motor cover, wherein (1) the fan housing defines a scroll cut-off line, and (2) a plane passes through the scroll cut-off line and the central axis, and (3) the cooling duct is positioned adjacent to the plane.

Abstract: A vehicle engine-cooling fan assembly for circulating air to cool an engine. The fan assembly has a central hub with a plurality of blades extending radially outward from the central hub. Each blade has a root joined to the central hub, a tip, and a span formed between the root and the tip. The blades are spaced circumferentially from each other, by unequal spacing angles, around the central hub. The unequal spacing angles minimize noise produced by the fan assembly. The blades are positioned at a radial location along a blade span by unequal setting angles which increase the efficiency of the fan assembly. The blades can have either a straight or a curved planform. Mechanical energy is imparted to the fan assembly from an electric motor, a hydraulic motor, or some other source. Also disclosed is a process for designing a vehicle fan assembly combining unequal fan blade spacing angles and unequal fan blade setting angles.

Abstract: A blade for a vehicle engine-cooling fan assembly having a curved planform and a high-lift airfoil. The planform has a first region adjacent the root of the blade with forward curvature, a second region adjacent the tip of the blade with backward curvature, and an intermediate region disposed between the first region and the second region with substantially straight curvature. The airfoil has a leading edge; a rounded, bulbous nose section adjacent the leading edge; a trailing edge; a curved pressure surface extending smoothly and without discontinuity from the nose section to the trailing edge; a curved suction surface extending smoothly and without discontinuity from the nose section to the trailing edge; and a thin, highly cambered aft section formed adjacent the trailing edge and between the pressure surface and the suction surface.

Abstract: An airfoil defining the shape of the blades of a vehicle engine-cooling fan assembly. The airfoil has a leading edge; a rounded, bulbous nose section adjacent the leading edge; a trailing edge; a curved pressure surface extending smoothly and without discontinuity from the nose section to the trailing edge; a curved suction surface extending smoothly and without discontinuity from the nose section to the trailing edge; and a thin aft section formed adjacent the trailing edge and between the pressure surface and the suction surface. The aft section has a camber at its location of maximum camber of between 5 and 12% of the chord of the airfoil.