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997 results about "Surface element" patented technology

Surface element may refer to. An infinitesimal portion of a 2D surface, as used in a surface integral in a 3D space.

Stent delivery system with nested stabilizer and method of loading and using same

InactiveUS7867267B2Easy to useEasily collapsed longitudinallyStentsEar treatmentInterior spaceInsertion stent
A stent delivery system deploys a stent having an inner periphery that defines an interior space extending lengthwise along at least a part of the stent and comprising at least one segment having relatively low column strength. The stent delivery system comprises a stabilizer which is disposed within the stent interior space and has a surface element adapted to engage the stent inner periphery in a region containing the low-column-strength segment. The surface element may comprise a sleeve or a coating having a high friction surface adapted to transmit adequate shear force to the stent to move the stent relative to the outer sheath upon deployment. Alternatively, or in addition, the surface element can include at least one radial protuberance. The protuberances may comprise rings of various cross-sections, axial lengths, or space sizes therebetween, or may be in the form of discrete barbs, bumps, or inflatable knobs arranged in a ringed configuration or helical pattern about the stabilizer. The stabilizer may also comprise an inner core and a heat-moldable compression sleeve surrounding the inner core, the heat-moldable compression sleeve having an outer surface comprising a plurality of protuberances defined by a thermal imprint of the stent inner periphery on the compression sleeve outer surface. A method for delivering a stent using a stent delivery system as described herein is also disclosed, as is a method for loading a stent and stabilizer having a heat-moldable compression sleeve into a stent delivery system.
Owner:LIFESHIELD SCI

Laser radar road reconstruction and expansion exploratory survey design method

The invention discloses a laser radar road reconstruction and expansion exploratory survey design method. The method comprises the steps of A designing a result coordinate benchmark, measuring basic control and measuring pavement control points; B determining parameters including the data density, acquisition route and the like, and acquiring vehicle laser radar data along a main road and a ramp; C determining parameters including the data density, flight design and the like, and acquiring airborne laser radar data according to a designed flight strip; D realizing laser radar data fusion by refining laser point cloud plane coordinates and elevation coordinates and refining track line data; E acquiring characteristics of road traffic lane lines by using point cloud intensity information, and realizing extraction of characteristic lines of road pavements, protection and the like by adopting a method of projecting three-dimensional point clouds to a two-dimensional plane; F recovering planar elements and longitudinal surface elements of an existing road; G producing a DEM (digital elevation model), a DOM (digital orthophoto map) and a DLG (digital line graphic); H collaboratively designing laser radar measurement and road reconstruction and expansion CAD (computer-aided design), designing flat, longitudinal and transverse cross sections of a road, comparing and selecting schemes, and outputting final design drawings and charts.
Owner:CCCC SECOND HIGHWAY CONSULTANTS CO LTD

Multifunctional super-surface structure based on polarization, super-surface element and encryption method

The invention discloses a multifunctional super-surface structure based on polarization, a super-surface element and an encryption method, wherein the multifunctional super-surface structure comprisesa transparent substrate and a metal nano-brick array; the metal nano-brick array comprises a plurality of nano-bricks distributed on the substrate in an array mode; the surface of each nano-brick, away from the substrate, is a working surface; the substrate is divided into a plurality of square substrate units by the nano-bricks; the nano-bricks and the corresponding substrate units form nano-brick units; the geometric parameters of the nano-brick units comprise the lengths and widths of the nano-bricks and the side lengths of the substrate units; and the geometric parameters of the nano-brick units are configured as follows: when two first linearly polarized beams with polarization directions perpendicular to each other are incident on the working surface in a perpendicular mode, the reflection rate of one of the first linearly polarized beams is the highest, the transmissivity of the other first linearly polarized beam is the highest. The structure can simultaneously and independently control the phase of transmitted light and the light intensity of reflected light.
Owner:WUHAN POST & TELECOMM RES INST CO LTD

Helicopter aerodynamic layout optimization method capable of reducing adverse effect of aerodynamic interference

The present invention discloses a helicopter aerodynamic layout optimization method capable of reducing the adverse effect of aerodynamic interference. According to the method, aiming at the defects of a wind tunnel test and a CFD method and based on a discrete vortex method and a surface element method, a coupled aerodynamic interference high-precision analysis model for a helicopter is set up, so that the influence of aerodynamic interference on the helicopter can be considered only by simulating calculation without carrying out the wind tunnel test; compared with the CFD method, the method has the advantages of greatly reducing the requirements of a simulation model for computing resources and shortening computing time. In order to further reduce calculated amount and a optimization region, a helicopter fuselage shape parameter model is set up by a parametric method and a combined optimization method based on an agent model is adopted, so that the optimal helicopter aerodynamic outline and layout are obtained and the purpose of reducing aerodynamic interference to improve the flight characteristics of the helicopter is achieved. The helicopter aerodynamic layout optimization method can be applied to the conceptual design phase of the helicopter so as to improve the flight characteristics, the balancing characteristic, stability and manoeuvrability of the helicopter.
Owner:NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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