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211 results about "Relative thickness" patented technology

Suspended containers

A disposable package for consumable contents includes a container having a surrounding wall of upstanding, generally flexible material extending from a container bottom to a wide mouth defined by a rim formation of greater relative thickness than said surrounding wall, said mouth being of greater than two inch minimum horizontal dimension and being about as wide as the horizontal cross-section of a top of the container. The disposable package further includes a removable lid at least partially closing the mouth, the lid having a rim portion extending over and removably engaged with the rim formation to form at least part of an attachment of the lid to the container, the attachment being constructed to support the container and its contents when suspended by the lid, and a flexible suspending element extending from the lid and arranged to be engaged by a thin support element, the suspending element being sized and arranged, with a length less than about 5 inches, such that when engaged by said support element, the suspending element suspends the container by its lid in a position below the support, for at least one of display and transport. In some embodiments, a single suspending element extends from a rim region of the container, the element being located to suspend the package at a tilted orientation, such that the lid of the container, so suspended, extends at a greater angle to horizontal than does the lid of the container when rested upon said bottom. Also, a display rack is provided for displaying such disposable packages.
Owner:LID LASSO

Ultrathin metallic resistance composite multi-frequency wave-absorbing material

The invention relates to an ultrahigh metallic resistance composite multi-frequency wave-absorbing material and belongs to the technical field of wave-absorbing materials. The technical problems that in the prior art, a circuit simulation wave-absorbing structure is narrow in wave-absorbing bandwidth, single in wave-absorbing frequency band and large in relative thickness are solved. The wave-absorbing material comprises a frequency selecting surface, a medium layer and a metal bottom plate. The frequency selecting surface is composed of patch units arrayed periodically, and each patch unit comprises a square patch, a first square surrounding patch and a second square surrounding patch, wherein the square patch, the first square surrounding patch and the second square surround patch are sequentially arrayed from inside to outside according to the length of sides. The wave-absorbing material further comprises four L-shaped patches which are symmetrically arranged outside four right angles of the second square surrounding patch. The double-frequency or triple frequency wave-absorbing characteristic that the reflection coefficient, below -10dB, of the wave-absorbing material is adjusted within the 4 GHz-18 GHz range can be achieved, the reflection coefficient of about -20 dB can be achieved nearby a wave-absorbing harmonic peak, and therefore a higher wave-absorbing effect is achieved.
Owner:CHANGCHUN INST OF OPTICS FINE MECHANICS & PHYSICS CHINESE ACAD OF SCI

Large-thickness blunt-trailing-edge wind-power airfoil profiles and a design method thereof

The invention discloses a group of large-thickness blunt-trailing-edge wind-power airfoil profiles and a design method thereof. The airfoil profiles have high lift coefficients under operation angles of attack. The airfoil profile group includes four airfoil profiles with relative thicknesses of 45%, 50%, 55% and 60% in sequence and with trailing edge thicknesses of 7%, 9%, 12% and 16% in sequence. Variable working condition design is adopted by the airfoil profile group, design Reynolds numbers of the four airfoil profiles are 4.0*106, 3.5*106, 3.0*106 and 2.5*106 in sequence according to the relative thicknesses, and the design objective mainly aims to take stability, changed along with the Reynolds numbers, of the lift coefficients as main constraint according to change features of the lifting coefficients within the range of large angles of attack in vane root areas. Numerical prediction results indicate that when the four large-thickness blunt-trailing-edge airfoil profiles are in the range of large angles of attack, the lift coefficients ascend continuously and stably and are in a high level. By the airfoil profile group, vane structural strength and stiffness can be improved, and a wind turbine can have high-efficient and stable output.
Owner:INST OF ENGINEERING THERMOPHYSICS - CHINESE ACAD OF SCI

Degradable lamellar Zn-Mg composite material and preparation method thereof

The invention discloses a degradable lamellar Zn-Mg composite material and a preparation method thereof. The outer layer of a lamellar medical metal composite material is made of pure zinc or zinc alloy, and the core part of the lamellar medical metal composite material is made of pure magnesium or magnesium alloy; the ratio of zinc or zinc alloy and magnesium or magnesium alloy is calculated according to volume percentage, zinc or zinc alloy accounts for 20%-50% of the total volume of the material, and the balance is magnesium or magnesium alloy. The lamellar composite material is prepared bycombining layered casting with nested extruding. The degradable lamellar Zn-Mg composite material has the advantages that: the selected magnesium alloy and the selected zinc alloy have good biocompatibility and degradability; mechanical properties and a degradation rate of the integral composite material are controlled by controlling a relative thickness of a Zn layer to a Mg layer, so that the composite material adapts to a service environment, and therefore, a condition that single metal is too quick or too slow in degradation is solved. The material design and the preparation method are simple and convenient, and the cost is low, so that industrial production is facilitated.
Owner:TIANJIN UNIVERSITY OF TECHNOLOGY

Method for evaluating performance of wing profile special for horizontal axis wind turbine

The invention discloses a method for parameter testing the performance of a wing profile special for a horizontal axis wind turbine. The method comprises the following steps of: firstly, acquiring the wing profile and aerodynamic data thereof; secondly, analyzing the geometry parameter of the wing profile and dividing the wing profile into a thin type and a thick type according to different relative thicknesses; thirdly, obtaining a design point performance parameter item, a non-design point performance parameter item, a stalling characteristic parameter item and a stability parameter item of the wing profile; fourthly, comparing with the performance reference index of the wing profile to obtain a relative value and judging the performance level of the wing profile; and finally, endowing the wing profile with different weight coefficients according to different types of the wing profiles, and calculating an overall performance evaluation value of the wing profile based on the relative value to judge the performance level of the wing profile of the wind turbine. The invention can provide a judging basis and a method for selecting different wing profiles on different parts when wind turbine blades are designed or can be used for evaluating the performance of an intermediate wing profile during design and optimization of new wing profiles.
Owner:中科国风科技有限公司

Friction stir welding method for different metal plates

The invention provides a friction stir welding method for different metal plates. The friction stir welding method for different metal plates comprises the following steps that (1) the relative thicknesses of two metal plates are determined; (2) connector structures are machined at the welding end of the two metal plates, specifically, a rectangular groove is machined in the welding end of the low-melting point metal plate, and a rectangular boss is machined at the welding end of the high-melting point metal plate, and the height and thickness of the rectangular boss are matched with the depth and width of the rectangular groove correspondingly; (3) whether a transition layer capable of avoiding or reducing generated intermetallic compounds needs to be additionally arranged or nor is determined, specifically, the transition layer is arranged on the surface of the rectangular boss if the ductility of the intermetalic compounds between the two metal plates is not larger than 2%, otherwise, the next step is executed directly; (4) the two metal plates are fixed through clamps; (5) welding technological parameters are set; and (6) welding of the two metal plates is completed through a stirring head according to the set welding technological parameters. According to the friction stir welding method for different metal plates, the welding quality is high, and the stress condition of connectors can be improved.
Owner:725TH RES INST OF CHINA SHIPBUILDING INDAL CORP
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