Patents
Literature
Hiro is an intelligent assistant for R&D personnel, combined with Patent DNA, to facilitate innovative research.
Hiro

98 results about "Spiral trajectory" patented technology

Methods for processing holes by moving precisely timed laser pulses in circular and spiral trajectories

High speed removal of material from a specimen employs a beam positioner for directing a laser beam axis along various circular and spiral laser tool patterns. A preferred method of material removal entails causing relative movement between the axis of the beam and the specimen, directing the beam axis at an entry segment acceleration and along an entry trajectory to an entry position within the specimen at which laser beam pulse emissions are initiated, moving the beam axis at a circular perimeter acceleration within the specimen to remove material along a circular segment of the specimen, and setting the entry segment acceleration to less than twice the circular perimeter acceleration.
Owner:ELECTRO SCI IND INC

Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse

The method serves to place a space vehicle, such as a satellite, on a target orbit such as the orbit adapted to normal operation of the space vehicle and starting from an elliptical initial orbit that is significantly different from, and in particular more eccentric than the target orbit. The space vehicle is caused to describe a spiral trajectory made up of a plurality of intermediate orbits while a set of high specific impulse thrusters mounted on the space vehicle are fired continuously and without interruption, thereby causing the spiral trajectory to vary so that on each successive revolution, at least during a first stage of the maneuver, perigee altitude increases, apogee altitude varies in a desired direction, and any difference in inclination between the intermediate orbit and the target orbit is decreased, after which, at least during a second stage of the maneuver, changes in perigee altitude and in apogee altitude are controlled individually in predetermined constant directions, while any difference in inclination between the intermediate orbit and the target orbit continues to be reduced until the apogee altitude, the perigee altitude, and the orbital inclination of an intermediate orbit of the space vehicle have substantially the values of the target orbit.
Owner:SN DETUDE & DE CONSTR DE MOTEURS DAVIATION S N E C M A

Model-based synthesis of band moire images for authentication purposes

The present invention relies on a band moiré image layout model capable of predicting the band moiré image layer layout produced when superposing a base band grating layer of a given layout and revealing line grating layer of a given layout. Both the base band grating layer and the revealing line grating layer may have a rectilinear or a curvilinear layout. The resulting band moiré image layout may also be rectilinear or curvilinear. Thanks to the band moiré image layout model, one can choose the layout of two layers selected from the set of base band grating layer, revealing line grating layer and band moiré image layer and obtain the layout of the third layer by computation, i.e. automatically. In the case of a concentric band moiré image, base band grating layer and revealing line grating layer layouts may be produced according to geometric transformations, which yield, upon relative displacement of the position sampled by the revealing layer on the base layer, a band moiré image whose patterns move either radially, circularly or according to a spiral trajectory, depending on the orientation of the base band replication vector in the original non-transformed base layer space. In addition, it is possible to conceive a revealing line grating layer which when translated on top of the base band grating layer, generates a band moiré image which is subject to a periodic deformation. Furthermore, thanks also to the availability of a large number of geometric transformations and transformation variants (i.e. different values for the transformation constants), one may create documents having their own individualized document protection. The base band layer and the revealing layer may be separated by a small gap and form a fixed composed layer, where, thanks to the well-known parallax effect, by tilting the composed layer in respect to an observer, different positions of the base layer are sampled and a dynamically moving moiré image is generated. A computing system may automatically generate upon request an individualized protected security document having specific base band grating and revealing line grating layouts. The computing system may then upon request generate and issue a security document incorporating the base band grating layer, a base band grating layer or a revealing line grating layer allowing to authenticate a previously issued security document. The presented methods may be used for creating an individualized protection for various categories of documents (banknotes, identity documents, checks, diploma, travel documents, tickets) and valuable products (optical disks, CDs, DVDs, CD-ROMs, packages for medical drugs, products with affixed labels, watches).
Owner:ECOLE POLYTECHNIQUE FEDERALE DE LAUSANNE (EPFL)

Method and a system for putting a space vehicle into orbit, using thrusters of high specific impulse

The method serves to place a space vehicle, such as a satellite, on a target orbit such as the orbit adapted to normal operation of the space vehicle and starting from an elliptical initial orbit that is significantly different from, and in particular more eccentric than the target orbit. The space vehicle is caused to describe a spiral trajectory made up of a plurality of intermediate orbits while a set of high specific impulse thrusters mounted on the space vehicle are fired continuously and without interruption, thereby causing the spiral trajectory to vary so that on each successive revolution, at least during a first stage of the maneuver, perigee altitude increases, apogee altitude varies in a desired direction, and any difference in inclination between the intermediate orbit and the target orbit is decreased, after which, at least during a second stage of the maneuver, changes in perigee altitude and in apogee altitude are controlled individually in predetermined constant directions, while any difference in inclination between the intermediate orbit and the target orbit continues to be reduced until the apogee altitude, the perigee altitude, and the orbital inclination of an intermediate orbit of the space vehicle have substantially the values of the target orbit.
Owner:SN DETUDE & DE CONSTR DE MOTEURS DAVIATION S N E C M A

Synthesis of superposition images for watches, valuable articles and publicity

InactiveUS7295717B2Improve visual attractiveness and aestheticVisual indicationOther printing matterGratingDisplay device
The present invention aims at synthesizing superposition images formed either by band moire shapes or by shape level lines for making the information forwarded by valuable articles or by time pieces such as watches and clocks more dynamic, as well as for improving their attractiveness and aesthetics. A further application is publicity. For synthesizing band moiré images, the present invention relies on a band moiré image layout model allowing to obtain the layout of the base the band grating, given the layouts of the band moire image and of the revealing line grating. Base and revealing layer layouts may be conceived to create band moiré image shapes whose patterns move e.g. radially, circularly, or according to a spiral trajectory. Shape level lines occur in a superposition image when e.g. a base layer comprising modified sets of lines is superposed with a revealing layer comprising a line grating. Such a base layer embeds a shape elevation profile generated from an initial motif shape image (e.g. typographic characters, words of text, symbols, logo, ornament). By moving the revealing layer in superposition with the base layer, shape level lines move dynamically between the initial motif shape boundaries and shape foreground centers, respectively shape background centers, thereby growing and shrinking. The movement of the shape level lines creates visually attractive pulsing motif shapes, e.g. a pulsing heart or pulsing text. Categories of embodiments comprise (1) visually attractive articles having moving parts (watches, clocks, vehicles, publicity display devices, fashion clothes), (2) articles such as cosmetics, drugs, perfumes and wines, where one part is moved in respect to a second part, e.g. bottles having a lid or labels composed of two layers, (3) articles where the base layer and the revealing line grating are separated by a gap and form a fixed composed layer, and (4) articles where at least one of the layers is an electronic display.
Owner:ECOLE POLYTECHNIQUE FEDERALE DE LAUSANNE (EPFL)

Flounder-type underwater glider

InactiveCN103287558AChange direction of taxiingSolve the large radius of gyrationUnderwater vesselsUnderwater equipmentLow noiseResist
The invention discloses a flounder-type underwater glider. An electronic cabin comprises a pressure-resisting cabin, a gravity and gravity center adjustment mechanism, a control system and a lithium battery unit. The inside of the pressure-resist cabin is partitioned into a central area, a middle circular area and an outer circular area. The lithium battery unit is arranged in the middle circular area. The control system includes an overwater control system and an underwater control system which are connected in a wireless manner. The underwater control system and the electronic part of surveying equipment are arranged in the middle circular area uniformly. The gravity and gravity center adjustment mechanism comprises four water bag pump units in same structure, and the four water bag pump units are distributed in the outer circular area symmetrically. The flounder-type underwater glider has the advantages of low cost, low noise, high endurance and high flexibility; the gravity and posture of the glider can be adjusted to realize zigzag or spiral trajectory through controlling the four water bag pump units distributed symmetrically. The flounder-type underwater glider can carry a plurality of underwater scientific-investigation and survey devices simultaneously, continuous data collection in extensive sea areas can be completed automatically, and the data can be transmitted back in real time.
Owner:SHANGHAI JIAO TONG UNIV

Cooling apparatus for electronic device

The present invention relates to a cooling apparatus for an electronic device. In the present invention, a coolant passing through a condenser 10 is introduced into and s filled in a compensator 15. The coolant passing through the compensator 15 is introduced into a vaporizer 20 and vaporized through heat exchange with an auxiliary heat source H2 provided outside of the vaporizer. In addition, a vaporizing unit 22 made of a porous material is provided in the vaporizer 20. The coolant passing through the vaporizer 20 and a liquid coolant supplied from the condenser 10 are mixed in a vortex generating unit 30 to form a coolant spray, and the coolant spray moves along a spiral trajectory to be formed into a vortex. Meanwhile, the coolant spray of a vortex is injected to be in close contact with the inner wall of an evaporator 50 to be heat-exchanged with a main heat source H1 positioned outside of the evaporator, thereby cooling the main heat source H1. According to the present invention as mentioned above, the main heat source adjacent to the evaporator is heat-exchanged with the coolant more actively to thereby improve the cooling performance of the electronic device. Also, a pressure loss of the coolant spouted from the venturi tube is further reduced.
Owner:LG ELECTRONICS INC +1

Construction method of time-varying dynamic model for high-feed turning of external thread members

ActiveCN107368665AAids in analytical researchAdjust and optimize processing parametersGeometric CADSpecial data processing applicationsVirtual workStrain energy
The invention relates to a construction method of a time-varying dynamic model for high-feed turning of external thread members; the method comprises the steps of I, using, based on the Rayleigh beam vibration theory, a nose track spiral line equation as an integration object to solve a workpiece strain energy and kinetic energy equation for a tool that performs cutting along the nose spiral track; II, considering, based on an established tool instant cutting force model, the impact of 'quasi-regeneration effect' upon instant cutting force for turning a large-pitch thread member so as to correct the existing instant cutting force model and perform numerical solution; III, describing boundary conditions of thread member turning through a vibration mode function, and performing solving; IV, establishing and solving a workpiece vibration model according to the virtual work principle and the method of separation of variables. The large-pitch external thread member vibration equation established herein is capable of predicting a sharply varying position of a workpiece upon vibration and displacement, and can assist in adjusting and optimizing parameters of a machining process for large-pitch thread members.
Owner:HARBIN UNIV OF SCI & TECH

High-availability data collection method based on multiple AUVs in underwater sensor network

The invention discloses a high-availability data collection method based on multiple AUVs in an underwater sensor network. The method comprises the following steps: constructing an underwater sensor network model, patrolling, by a plurality of autonomous underwater vehicles AUVs, in the network according to a predefined spiral trajectory for data collection, and periodically adjusting the patrol trajectory; and calculating, by a node, whether itself is within the collection area of one or more autonomous underwater vehicles AUVs according to own location and the trajectories of the autonomousunderwater vehicles AUVs. The node within the collection area performs communication after the autonomous underwater vehicle AUV arriving at the vicinity of the node to upload data; and the node beyond the collection area forwards the data to the node within the collection area through multiple hops. When the autonomous underwater vehicle AUV is faulty, a gateway node discovering the fault broadcasts a control packet and performs fault processing. By adoption of the high-availability data collection method, the energy consumption and the communication overhead of the node are reduced, and thehigh availability of the network is guaranteed.
Owner:HOHAI UNIV CHANGZHOU

Method and magnetic resonance system for distortion correction in magnetic resonance imaging

The invention relates to a method for distortion correction in spiral magnetic resonance imaging, radial magnetic resonance imaging and echo planar imaging. In a method for distortion correction in spiral magnetic resonance imaging, a first MR data set is acquired by scanning raw data space along a spiral trajectory beginning at a first point. A first complex MR image is determined from the first MR data set, which includes first phase information for image points of the first MR image. A second MR data set is acquired by scanning raw data space along the spiral trajectory beginning at a second point that differs from the first point. A second complex MR image is determined from the second MR data set, which includes second phase information for image points of the second MR image. A geometric distortion for image points of the first or second MR image is determined from the first and second phase information, for example with a PLACE method.
Owner:SIEMENS AG

In-place precision measurement method for three-dimensional shape error of aspheric grinding circular arc diamond grinding wheel

The invention provides an in-place precision measurement method for a three-dimensional shape error of an aspheric grinding circular arc diamond grinding wheel. The in-place precision measurement method comprises the steps that (1) height data of all points on the surface of the grinding wheel are spirally and continuously scanned and measured; (2) the data are subjected to interpolation fitting treatment according to a spiral trajectory model, a three-dimensional geometrical morphology matrix on the surface of the grinding wheel is obtained, and least square circular arc fitting is conducted, so that the circular arc radius, the circular arc center coordinate and the circular arc center deviation of the grinding wheel are obtained; (3) an average three-dimensional geometrical morphology matrix on the surface of the grinding wheel is established and subtracted from the morphology matrix, and a three-dimensional error distribution matrix, a circular arc degree error and a radial run-out error are obtained; and (4) outer circumference height data of the grinding wheel are measured, and the basic part radius of the grinding wheel is obtained through least square circular arc fitting. According to the in-place precision measurement method for the three-dimensional shape error of the aspheric grinding circular arc diamond grinding wheel, efficient precision non-contact measurement of all the important geometrical parameters of the circular arc diamond grinding wheel is achieved, and the measurement results can be directly used for precise interpolation calculation of aspheric optical element ultra-precision grinding machining grinding wheel movement control point coordinates.
Owner:LASER FUSION RES CENT CHINA ACAD OF ENG PHYSICS
Who we serve
  • R&D Engineer
  • R&D Manager
  • IP Professional
Why Eureka
  • Industry Leading Data Capabilities
  • Powerful AI technology
  • Patent DNA Extraction
Social media
Try Eureka
PatSnap group products