458 results about "High elevation" patented technology

A method and apparatus for mitigating communications interference between satellite communications systems in different orbits is disclosed. The method comprises the steps of evaluating a geometrical relationship between a second ground station and the satellites in the second satellite constellation, and directing communications between the second ground station and the second satellite according to the evaluated geometrical relationship. In one embodiment communications are handed over from a first satellite to another satellite when the first satellite is no longer at the highest elevation angle of visible satellites. In another embodiment, handover occurs when the first satellite drops below a minimum elevation angle.

A hands-free personal hydration delivery system has a tubing assembly that has one end that detachably connects to a feed tube for a container of fluid worn on the back or torso of a user. The other end of the tubing assembly is coupled to a bite valve which is opened when manipulated by the user's mouth to allow fluid to be drawn by suction applied by the user, and is closed when not being manipulated so as to cut off fluid flow in an air-tight condition. An intermediate portion of the tubing assembly is mounted on the user's head or to the user's headgear at a position of higher elevation than the user's mouth. This allows fluid to be drawn to the elevated position and flow downward from there to the user's mouth by gravity feed. The fluid flow can then continue with little suction effort due to the gravity feed and siphoning effect of fluid from the container. The tubing can be mounted using retainer loops or other type of fasteners attached to a helmet, sports cap, head band bracket, headphone bracket, headband, or an earpiece worn by the user. The hydration delivery system is especially useful for bicycling, canoeing, mountain biking, kayaking, canoe paddling, and rowing environments.

A fluid catalytic cracking process includes feeding hydrocarbon into a riser in the presence of a catalyst, cracking the hydrocarbon in the riser in the presence of the catalyst to form a cracked stream, and separating the catalyst from the cracked stream. When in a gasoline mode, the hydrocarbon is fed through a first distributor into the riser, and when in a light olefin mode, the hydrocarbon is fed through a second distributor into the riser. The second distributor is positioned at a higher elevation than the first distributor.

A disposable cup lid for placement onto a drinking cup is provided, having a tear tab which is generally aligned with the orientation of the extruded plastic sheet material from which the cup lid is made. There is a first, generally centrally located region in the lid, which has a higher elevation than the cup rim receiving recess at the periphery of the lid; and there is an indentation formed in the central region which is provided so as to accommodate the tear tab when it is folded back around a U-shaped hinge to create a drink-through opening in the cup lid. The indentation has a pair of detents located at its edges so as to hold and retain the tear tab in place when the foldback flap is folded back about the U-shaped hinge and the tear tab is inserted into the indentation. The tear tab is retained below the plane of the central region of the cup lid.

A flight information display for the flight deck of an aircraft showing a pictorial side view of the flight path or the area directly in front of the aircraft area having a selected distance of at least 0.5 nautical miles, comprising (a) a pictorial representation to scale of the profile of the highest elevations of a swath of terrain along said path or area, (b) an icon positioned on the left or right side of the display representing the aircraft, the altitude of which is to scale with the height of the terrain, and (c) an altitude reference scale; wherein the width of the swath is at least 0.1 nautical miles and no greater than the distance of the minimum accuracy of the means for determining the aircraft's location.

Apparatus for biomass torrefaction which includes a serpentine elongated housing, the housing having three generally U-shaped axial portions having first and second axial extremities and an intermediate section, the first and second axial extremities are disposed in normal use at a higher elevation than the first and second axial extremities, the intermediate section being configured for holding a liquid. Other forms of the invention include the method for biomass torrefaction which includes providing a quantity of biomass, providing a liquid heat transfer fluid, providing at least a first housing for holding the heat transfer liquid, elevating the temperature of the liquid heat transfer liquid, heat treating the biomass by passing it through the heat transfer liquid in the first housing at a temperature and duration sufficient to accomplish torrefaction of the wood. In some forms of the method, the process further includes the step of pelletizing the biomass prior to performing the treating step.

The invention relates generally to processes for producing electrically conductive noble metal thin films on a substrate by atomic layer deposition. According to one embodiment of the invention a substrate with a surface is provided in a reaction chamber and a vaporised precursor of a noble metal is pulsed into the reaction chamber. By contacting the vaporised precursor with the surface of the substrate, no more than about a molecular layer of the metal precursor is formed on the substrate. In a next step, a pulse of molecular oxygen-containing gas is provided in the reaction chamber, where the oxygen reacts with the precursor on the substrate. Thus, high-quality metal thin films can be deposited by utilising reactions between the metal precursor and oxygen. In one embodiment, electrically conductive layers are deposited in structures that have high aspect ratio vias and trenches, local high elevation areas or other similar surface structures that make the surface rough.

A structural tower having a space frame construction for high elevation and heavy load applications is disclosed, with particular application directed to wind turbines. The structural tower includes damping or non-damping struts in the longitudinal, diagonal or horizontal members of the space frame. One or more damping struts in the structural tower damp resonant vibrations or vibrations generated by non-periodic wind gusts or sustained high wind speeds. The various longitudinal and diagonal members of the structural tower may be secured by pins, bolts, flanges or welds at corresponding longitudinal or diagonal joints of the space frame.

A gasification reactor comprising a vessel (1), provided at its upper end with a downwardly directed burner (2), and provided with supply conduits for an oxidizer gas (3), a carbonaceous feed (4) and a moderator gas (5), a combustion chamber (6) in the upper half of the vessel provided with a product gas outlet (7) at its bottom end and an opening for the outlet of the burner (2) at its top end, wherein between the wall of the combustion chamber (6) and the wall of the vessel (1) an annular space (9) is provided, and wherein the wall of the combustion chamber (6) comprises an arrangement of interconnected parallel arranged tubes (10) resulting in a substantially gas-tight wall running from a common lower arranged distributor (12) to a higher arranged common header (11), said distributor (12) provided with a cooling water supply conduit (14) and said header (11) provided with a steam discharge conduit (13) and wherein the steam discharge conduit (13) and the water supply conduit (14) are fluidly connected to a steam drum (29) and wherein the steam drum (29) is provided with a supply conduit (32) for fresh water and wherein the steam drum (29) is positioned at a higher elevation than the common header (11).

A method of communicating satellite tracking information among a network of global navigation satellite system receivers is described. The method includes determining at a first GNSS receiver which satellites in a constellation of satellites have been continuously tracked over a preceding selected time period, and for each such satellite determining its elevation with respect to the zenith. Only the elevation value for the lowest satellite in the set of satellites for which all satellites of higher elevation values have been continuously tracked over the selected time period is then transmitted to the second GNSS receiver. That receiver can then reconstruct the set of satellites which have been continuously tracked.

A flight information display for the flight deck of an aircraft showing a pictorial side view of the flight path or the area directly in front of the aircraft area having a selected distance of at least 0.5 nautical miles, comprising (a) a pictorial representation to scale of the profile of the highest elevations of a swath of terrain along said path or area, (b) an icon positioned on the left or right side of the display representing the aircraft, the altitude of which is to scale with the height of the terrain, and (c) an altitude reference scale; wherein the width of the swath is at least 0.1 nautical miles and no greater than the distance of the minimum accuracy of the means for determining the aircraft's location.

A wind power plant for producing electrical energy on a large scale, comprising a base, a housing, rotatable on said base around vertical axis. A wind tail, attached to the housing, rotate the housing toward direction of the wind, utilizing the power of the wind, and produces additional tunnel suction to the flow of the wind from front side to back side of the housing. A plurality of turbines, equipped with rotors with wide blades, is mounted inside the housing one above another. Deflectors cover from the wind the front side of the rotors above their axis of rotation while computer controlled governors are covering the remaining front side of the rotors below their axis of rotation, keeping steady the speed of rotation of the rotors. Working surfaces of turbines are covered from heavy snow and during the storm and protected from birds. Power plant saves the area of occupied land, utilizing higher speed of wind on higher elevations. It has an attractive aesthetic view and can be a landmark for the location where it is built.

A hybrid water pressure energy accumulating, tower assembly used to directly propel water pumps to raise water from low elevation reservoir(s) to high elevation reservoir(s) where it is used as a potential energy. The tower is electrically connected and positioned next to or close to a wind turbine or a wind or solar power plant. The tower includes in-tower storage reservoirs configured for storing water. The in-tower storage reservoirs could be defined by lower and upper water storage containers attached to the inner or outer surface of the tower that might be connected to other neighboring reservoir(s). The lifted water is used to generate electricity utilizing a hydropower generator.

This invention is a system of transparent or translucent panel units that permit selective transmission of light and solar radiation or glare across the system and can be adjusted and controlled according to a user's varying needs using light-controlling members mounted for rotation about their longitudinal axes. The system can illuminate the interior space by reflected sunlight, conducting both light from the brightest part of the sky and low-angle sunlight efficiently into the interior space, and also shading or deflecting the intense light found when the sun is at high elevation. Alternatively, the amount of a selected portion of the radiation spectrum passed through the system can be set at will, and can be amplified to allow increased light passage and transmission.

The invention discloses a rapid satellite selection method for a global navigation satellite system. The rapid satellite selection method carries out the satellite selection on the basis of meeting the navigation positioning requirements, so as to achieve the purposes of reducing the calculation amount of satellite selection and reducing the calculation amount of navigation positioning. Firstly, visible satellites are divided into three regions of high elevation angle, middle elevation angle and low elevation angle according to the size of the elevation angle, the satellite with the largest elevation angle is selected, and then the satellite selection is carried out in the high elevation angle satellites according to the size of the elevation angle of the satellite with the biggest elevation angle. Then an appropriate number of positioning satellites are selected from the middle and the low regions according to the equalization principle of the satellites in constellations. Finally, the satellite selection result is verified according to geometric dilution of precision, and the satellite selection result is amended according to the verification result, thereby leading the satellite selection result to meet the positioning requirements. The method can effectively solves the problem of great calculation amount of the traditional satellite selection method and can realize the simple and rapid satellite selection and is applicable to real-time satellite selection demands under static and dynamic conditions.

A mobile receiver is programmed with available channels by initially searching for all potentially available channels and autoprogramming the receiver with channels that are detected by the receiver. Subsequently, only potentially available channels that have not been programmed into the receiver are searched for to reduce autoprogramming time when, e.g., the mobile receiver is carried to a higher elevation.

A method for inversion of the ground feature high elevation and the number of land subsidence through high resolution InSAR timing sequence analysis includes the first step of high resolution SAR data selection, the second step of initial elevation phase estimation, the third step of selection of InSAR timing sequences, analysis of an interference image pair data set and extraction of coherent target candidate points, the fourth step of elevation phase correction and linear deformation component estimation, and the fifth step of deformation sequence estimation of coherent targets. According to the method, the defect that no high resolution DEM is available for removal of high-rise building additional phases in urban area high resolution InSAR deformation monitoring data processing can be overcome, the additional phases and deformation phases of urban high-rise buildings in the high resolution InSAR are effectively separated, and therefore monitoring precision of the high resolution InSAR in urban area land subsidence is greatly improved.

A stretch head for facilitating the wrapping of palletized loads within packaging or wrapping film comprises a vertical downright, and a carriage assembly vertically movable along the vertical downright. A base plate is mounted upon the carriage assembly and is inclined with respect to a horizontal plane so as to have a first end thereof disposed at a higher elevation than a second opposite end thereof. A supply roll of wrapping or packaging film is rotatably mounted upon the first higher end of the base plate, and a pair of tension rollers are mounted upon a substantially central portion of the base plate. A strain gauge roller is also mounted upon the base plate for receiving the wrapping film exiting from the tension rollers, a first idler roller is mounted upon the base plate for receiving the wrapping film from the strain gauge roller, and a second idler roller is mounted upon the second opposite end of the base plate for receiving the wrapping film from the first idler roller. Since the second idler roller is mounted upon the lowest end portion of the base plate, in view of the inclined disposition thereof, the second idler roller is capable of positioning the wrapping film at the lowest elevation whereby the wrapping film can be wrapped around the lowermost regions of the palletized load. The second idler roller also comprises a rubberized sleeve member for preventing movement of the wrapping film in an axial direction along the external periphery of the second idler roller so as to ensure proper positioning and orientation of the wrapping film with respect to the palletized load.

An input chamber receives runoff water to be cleaned. Part of the way up the chamber wall is a restricted outlet which feeds a system for cleaning the water. At a still higher elevation another opening allows runoff water to flow to an extended detention chamber. Near the top of the chamber is an outlet pipe. A vertical baffle in front of the outlet cleans water that flows under the baffle on its way to the outlet. When the incoming flow rate is very high, water passes over the baffle to the outlet.

A loader boom arm for a material handling vehicle used in the agricultural or construction industries includes a post attachable to the vehicle, a lower arm pivotally connected to the post, an upper arm pivotally connected to the lower arm, a pivoting mechanism coupled to the post and the lower arm, and a link arm pivotally connected to the post and to the upper arm. The boom arm is raised and lowered in an angular direction of rotation by pivoting the lower arm about the post using the pivoting mechanism. As the lower arm is pivoted, the link arm causes the upper arm to pivot relative to the lower arm such that the upper arm pivots further in the direction of angular rotation than the lower arm, thus changing the angle between the lower arm and upper arm. The subject loader boom arm allows an operator to move material in a bucket attached to the boom arm to locations of higher elevation and further reach than typically available with conventional boom arms.

The invention discloses an atmospheric turbulence detection simulator used for an self-adaptive optical system, which comprises a beam contracting module, a first atmospheric turbulence simulation unit, a second atmospheric turbulence simulation unit, a first splitter, a third atmospheric turbulence simulation unit, a second splitter, a lens, a Rayleigh beacon, a natrium beacon, and a target; thefirst atmospheric turbulence simulation unit, the second atmospheric turbulence simulation unit, and the third atmospheric turbulence simulation unit respectively represent the atmospheric turbulencedistribution from lower elevation to higher elevation according to order from left to right in sequence; the Rayleigh beacon is arranged behind the first atmospheric turbulence simulation unit, the second atmospheric turbulence simulation unit, and the first splitter, before the third atmospheric turbulence simulation unit; the natrium beacon is arranged behind the third atmospheric turbulence simulation unit and the second splitter; and the target is arranged behind the second splitter and the lens, and represents an infinity target.

A conveyor assembly is provided for accumulating and discharging a column of evenly spaced items. The conveyor assembly includes a receiving conveyor, a discharge conveyor and a belt guiding carriage. The receiving and discharge conveyors each include a plurality of round belts that are interlaced with the receiving belts being at a slightly higher elevation on the receiving end of the system and the discharge belts being at a slightly higher elevation on the discharge end. Both sets of belts pass through a movable carriage that guides the receiving belts from the upper elevation to the lower elevation and the discharge belts from the lower elevation to the upper elevation so that the receiving belts are at a higher elevation on the receiving end of the carriage and the discharge belts are at a higher elevation on the discharge end of the carriage.

An apparatus for loading bikes and motorcycles from the ground to a higher elevation such as into a transport vehicle without lifting. The apparatus permits the user to walk the bike or motorcycle into up a vehicle on a foldable, for easy storage, arcuate ramp. The user holds onto the bike or motorcycle and walks up the ramp from behind the cycle in a first embodiment; or adjacent to the vehicle into the van or truck in a second embodiment. The second embodiment includes a series of spaced steps or U-rungs on one or both sides of the ramp. Both versions fold for easy storage and portability and both embodiments can be separated into two parts for easy linear storage if needed.

A loader boom arm for a material handling vehicle used in the agricultural or construction industries includes a post attachable to the vehicle, a lower arm pivotally connected to the post, an upper arm pivotally connected to the lower arm, a pivoting mechanism coupled to the post and the lower arm, and a link arm pivotally connected to the post and to the upper arm. The boom arm is raised and lowered in an angular direction of rotation by pivoting the lower arm about the post using the pivoting mechanism. As the lower arm is pivoted, the link arm causes the upper arm to pivot relative to the lower arm such that the upper arm pivots further in the direction of angular rotation than the lower arm, thus changing the angle between the lower arm and upper arm. The boom arm also preferably includes a low profile self leveling linkage assembly for maintaining the levelness of a bucket during raising and lowering of the boom arm, having a control arm pivotally connected to the lower arm, a rotator link pivotally connected to the upper arm at a leveling fulcrum, and an output arm pivotally connected to the rotator link and pivotally connectable to a work implement. The subject loader boom arm allows an operator to move material in a bucket attached to the boom arm to locations of higher elevation and further reach than typically available with conventional boom arms.

Provided is a method of correcting an ionosphere error, a system of a precise orbit determination using the same and a method thereof. The method includes the steps of: a) determining a time of a highest elevation angle of a GPS satellite per one pass of each GPS satellite received at a LEO satellite or a receiver on a ground; b) determining a minimum total electron content found from an ionosphere model of the determined time per one pass of each GPS satellite; c) determining a total electron content directly calculated from the LEO satellite or a single frequency GPS data; d) determining an ionosphere error value of a single frequency GPS data by combining the minimum total electron content and the directly calculated total electron content; and e) correcting pseudorange data or carrier phase data based on the determined ionosphere error value.