1241results about How to "Reduce air resistance" patented technology

An improved gas deposition chamber includes a hollow gas deposition volume formed with a volume expanding top portion and a substantially constant volume cylindrical middle portion. The hollow gas deposition volume may include a volume reducing lower portion. An aerodynamically shaped substrate support chuck is disposed inside gas deposition chamber with a substrate support surface positioned in the constant volume cylindrical middle portion. The volume expanding top portion reduces gas flow velocity between gas input ports and the substrate support surface. The aerodynamic shape of the substrate support chuck reduces drag and helps to promote laminar flow over the substrate support surface. The volume reducing lower portion helps to increase gas flow velocity after the gas has past the substrate support surface. The improved gas deposition chamber is configurable to 200 mm diameter semiconductor wafers using ALD and or PALD coating cycles. An improved coating method includes expanding process gases inside the deposition chamber prior to the process gas reaching surfaces of a substrate being coated. The method further includes compressing the process gases inside the deposition chamber after the process gas has flowed past surfaces of the substrate being coated.

A method and system for a plurality of airplanes in flight to receive from and send to a plurality of ground stations broadcast and communication signals through a single or a plurality of geostationary satellites, wherein at least the mobile link between said airplanes and said satellite, uplink or downlink, uses the high frequency radio waves at 17 GHz or higher, such as Ka-band. The fixed link between said satellite and said ground stations may use any radio frequencies below the frequencies used to communicate between the satellite and the aircraft. The lower frequencies tend to be less susceptible to rain attenuation and hence suitable for closing the fixed broadcast and communication link. Frequencies such as C-band or Ku-band, or even Ka-band, are applied between satellite and ground such that the available link margin is sufficient to overcome rain attenuation at said ground stations. Said satellite carries a plurality of transponders that may include a plurality of frequency converters to enable the conversion between different frequencies. Said satellite generates a plurality of spot beams, shaped or unshaped, which collectively cover the flight routes of said airplanes, preferably the geodesic path between two highly populated regions.

Disclosed therein is an external monitoring system, which includes cameras mounted at both sides of the front and rear of a vehicle and on side view mirrors, display devices for outputting images in a driver's front sight direction through the cameras, and controller for controlling the display devices. The display devices are mounted on a dash board of the upper portion of an instrument cluster or on the dash board of the upper portion of a steering wheel and are adjustable in their location laterally to allow the driver to gaze the front to the maximum. The external monitoring system includes: front and rear view cameras disposed at both side ends of the front and rear of the vehicle; side view cameras mounted on both side view mirrors of the vehicle in such a way as to be directed to the rear of the vehicle; at least two display devices for receiving and outputting signals inputted through the front and rear view cameras and the side view cameras; a holding device mounted on the dash board of the upper portion of the instrument cluster for moving the display devices laterally and fixing them; and a controller for converting the image output from the front and rear view cameras and the side view cameras and controlling brightness of a screen and zoom-in and zoom-out of the cameras.

A nacelle (55) for a gas turbine engine (10), the engine (10) comprising accessories (34) mounted to a fan casing (28) and a core engine (9), the nacelle (55) substantially surrounds the engine (10) and comprises an intake (12) and a thrust reverser unit (31). The thrust reverser unit (31) is formed by two generally C-shaped portions (31a, 31b). The thrust reverser unit (31) is openable to provide access to the accessories (34) and the core engine (9). The nacelle (55) further comprises a fan containment casing (33) that is integral with the intake (12).

A combination of vehicle fairing structures forming a fairing system having a front end structure, a rear end structure, and first and second side structures, for optimizing the aerodynamic profile of vehicles, especially tractor-trailer combinations.

A resilient skirt assembly is provided, the assembly comprising a skirt panel adapted to connect to a trailer to direct at least a portion of the amount of air on the side of the trailer; and a skirt support adapted to connect the skirt to a trailer, the skirt support having a resilient strut providing lateral support to the skirt panel, the resilient strut allowing substantial lateral pivotal movement of the skirt panel between a skirt panel unloaded position and a skirt panel loaded position. A method of assembling a skirt assembly and a skirt kit are also provided.

The present invention is directed to the manufacture of and the use of an aerodynamic flow control device having a compact array of a plurality of fluidic actuators in planar, curved, circular and annular configurations. The compact array of fluidic actuators of the invention may be designed to produce oscillating or pulsed jets at the exit ports with frequencies in the range of 1-22 kHz. They may be integrally manufactured along with the wing sections, flaps, tail and rudder of airplane, the inlet or exit geometries of a jet engine. When supplied with a source of fluid such as air, these arrays of actuators produce a set of fluid jets of random phase of high velocity and influence the main stream of air over the subject surface. The beneficial effects of modifying flow using the present invention include increased lift, reduced drag, improved performance and noise reduction in jet engines.

A bicycle carrier for a vehicle including a frame, a crossbar assembly, a wheel tray, and a swing arm pivotally secured to the crossbar assembly. The wheels of the bicycle are positioned in the tray and secured by a tray coupling to restrain lateral movement. Two trays may be secured to the crossbar assembly to each receive a wheel of the bicycle. The swing arm pivots on the crossbar assembly and includes a shoe which engages the bicycle wheel. A shoe coupling secures the bicycle wheel to the swing arm. Two swing arms could be pivotally secured to the crossbar assembly each to engage a bicycle wheel. The frame may include a drawbar for insertion into the receiver of a trailer hitch. Additional crossbar assemblies could be secured to the frame to accommodate multiple bicycles.

The invention relates to a driving auxiliary device and a driving auxiliary method. The driving auxiliary device comprises image acquisition devices, a display, an image processing device and an alarm. Information of images around a vehicle is acquired, analyzed and processed by using a plurality of the image acquisition devices which are arranged in an optimized manner and the image processing device. On the one hand, traditional physical imaging rearview mirrors of an automobile are removed, visual blind areas of a driver are eliminated, and air resistance of the automobile is reduced; on the other hand, the acquired images are processed by the image processing device, information of risks under different driving conditions is identified, to fulfill the auxiliary functions of active safety driving, such as lane change and early warning for side impact in turning, early warning for safe interval, early warning for recognition of road signs, early warning for lane departure, early warning for pedestrian detection and collision avoidance.

A wing, in particular a airfoil of an aircraft, with a variable profile shape, which wing comprises a first skin and a second skin and a supporting structure, arranged between the first and the second skin, which supporting structure in the direction of the wing depth extends between a first end and a second end, wherein the form of said supporting structure, for the purpose of varying the profile shape by means of a drive device comprising drive elements, is variable. The supporting structure comprises ribs, arranged one behind the other in the direction of the wing depth, which ribs at connection positions are interconnected so as to be articulated, wherein said ribs at first connection positions are connected to the first skin, and at second connection positions are connected to the second skin. For the purpose of setting the variable profile the mutual spacing of the second connection positions can be varied by means of the drive elements.

A structure for sheltering and optimizing highway systems includes an arcuate structure extending over a highway and a cover over the structure to create an enclosure. The enclosure protects the highway and users of the highway from rain, snow and sun while the surrounding scenery remains visible to drivers. A number of different additions optimize use of the highway. For example, a plurality of solar panels are layered on the cover and wind turbines are used to create usable energy, an air current generation system reduces wind resistance on vehicles to increase gas mileage, and an elevated rail system transports many persons great distances along the highway.