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    • 1. 发明授权
    • Method of manufacturing an advanced composite duct having integral ribs
    • 制造具有整体肋骨的先进复合管道的方法
    • US5225016A
    • 1993-07-06
    • US739403
    • 1991-08-02
    • Branko Sarh
    • Branko Sarh
    • B29C53/30B29C70/46B29D99/00
    • B29D99/0014B29C53/30B29C70/46B29C70/462B29K2105/06B29L2023/003
    • A method of making ducts having outwardly extending ribs formed integrally with the duct structure. Two tubes are formed from fiber reinforced resin materials, a uniform inner tube and a ribbed outer tube, then the inner tube is bonded with in the outer tube to form a high strength ribbed duct. An outer tube is formed by placing resin impregnated fibers over a cylindrical mandrel having an inflatable bladder on its surface, placing a plurality of spaced rings tightly against the outer surface, pressurizing the bladder to expand the tube into the spaces between rings to form low ribs, then gradually moving the rings toward each other to press the ribs therebetween and form thin upstanding ribs. The inner tube is formed by placing resin impregnated fibers on a slightly thinner mandrel that also has a surface bladder. When both tubes are formed, the mandrel is removed from the outer tube and the inner tube and mandrel are inserted therein and the inner tube bladder is inflated. The assembly is vacuum bagged and cured in an autoclave at a suitable temperature. The rings and mandrel are then removed and an integrally ribbed duct results. The thermosetting or thermoplastic resin impregnated fiber material may be placed on the mandrels by any suitable means such as filament winding, hand lay-up, or other deposition techniques.
    • 一种制造具有与管道结构一体形成的向外延伸肋的管道的方法。 两根管由纤维增强树脂材料,均匀的内管和带肋的外管形成,然后将内管与外管接合,形成高强度的肋管。 通过将树脂浸渍的纤维放置在其表面上具有可膨胀囊的圆柱形心轴上而形成外管,将多个间隔开的环紧紧地放置在外表面上,对囊进行加压以将管扩展成环之间的空间,以形成低肋 然后逐渐地将环彼此移动以将肋压在其间并形成薄的直立肋。 内管通过将树脂浸渍的纤维放置在也具有表面膀胱的稍薄的心轴上而形成。 当两个管都形成时,心轴从外管中取出,内管和心轴插入其中,内管囊充气。 将组件真空包装并在适当温度下在高压釜中固化。 然后取出环和芯棒,并形成一体的带肋的导管。 热固性或热塑性树脂浸渍的纤维材料可以通过任何合适的方式放置在心轴上,例如细丝缠绕,手糊或其它沉积技术。
    • 2. 发明授权
    • Pivoting door thrust reverser
    • 旋转门推力反向器
    • US5117630A
    • 1992-06-02
    • US683587
    • 1991-04-11
    • Roy E. CariolaThadeus N. Grace
    • Roy E. CariolaThadeus N. Grace
    • B64D33/04F02K1/70
    • F02K1/70B64D33/04Y02T50/671
    • A pivot door type aircraft turbine engine thrust reverser which includes a pair of pivoting panels on the inner side of the door. The panels are positioned alongside the door actuation mechanism. The panels form a flush surface along the fan duct flow path when stowed during normal engine operation in flight. When the door is deployed in thrust reversing mode, one end of the door moves to at least partially block airflow through the duct and divert it out along the door through an opening uncovered by door deployment. During door deployment, a linkage moves the panels toward the outer surface of the door, exposing a door deflector plate to the airflow. Air flows along the door, then along the panel, out through the opening, then impacts the deflector plate which deflects the airflow in the reverse direction.
    • 枢轴门式飞机涡轮发动机推力反向器,其包括在门的内侧上的一对枢转面板。 面板沿着门致动机构定位。 当飞行中正常的发动机运转期间,这些板在沿着风扇管道流动路径形成平齐的表面。 当门以推力反向模式部署时,门的一端移动至少部分地阻挡通过管道的气流,并通过未被门部署覆盖的开口沿着门转移出门。 在门部署期间,连杆将面板移向门的外表面,将门偏转板暴露于气流中。 空气沿着门流动,然后沿着面板流过开口,然后撞击偏转板,该反向板使气流沿相反方向偏转。
    • 3. 发明授权
    • Integrated corner for ducted fan engine shrouds
    • 风扇发动机罩的集成角
    • US5101621A
    • 1992-04-07
    • US411991
    • 1989-09-25
    • Henry Mutch
    • Henry Mutch
    • B29D24/00B64D29/00
    • B29D24/005B64D29/00Y10T428/24149
    • An engine shroud with integral honeycomb panel corners for use in the thrust reverser region of ducted fan gas turbine engines. The integral shroud is useful in a turbine engine having a core engine surrounded by an engine casing and nacelle, with a fan at the inlet directing air flow into the bypass duct between core engine and engine nacelle. The shroud basically consists of right and left ducts each having an approximately semicircular cross-section with radial flanges extending from the duct edges. The flanges permit the halves to be fastened together to produce a tubular shroud adapted to surround a gas turbine engine and form the inner wall of a bypass duct. The disclosed shroud eliminates the prior complex corner fittings connecting the semicircular center portion of the shroud to the extending flanges and provides simple, integral corners.
    • 具有整体蜂窝板角的发动机罩,用于管道式风机燃气轮机的推力反向器区域。 整体护罩可用于具有由发动机壳体和机舱包围的核心发动机的涡轮发动机,入口处的风扇将空气流引导到核心发动机和发动机机舱之间的旁路管道。 护罩基本上由右和左管道组成,每个管道具有大致半圆形的横截面,其中径向凸缘从管道边缘延伸。 凸缘允许半部紧固在一起以产生适于围绕燃气涡轮发动机并形成旁通管道的内壁的管状护罩。 所公开的护罩消除了将罩的半圆形中心部分与延伸法兰连接的现有复杂的角配件,并且提供了简单的整体角。
    • 5. 发明授权
    • Method and apparatus for hot die draw forming metal sheets
    • 热冲模成型金属板的方法和装置
    • US5035133A
    • 1991-07-30
    • US477452
    • 1990-02-09
    • Robert T. WhiteThomas J. LiebigJeffrey K. Switzer
    • Robert T. WhiteThomas J. LiebigJeffrey K. Switzer
    • B21D25/02
    • B21D25/02
    • A method and apparatus for draw forming a metal sheet over a male form to produce a three-dimensional shape. A sheet of metal is clamped between upper and lower draw plates positioned above the male form. The upper plate has an edge conforming to the male form shape. The plates and sheet are moved downwardly over the form with the edge of the upper plate firmly pressing the sheet against the form. The clamping pressure between the draw plates allows suitable slippage as drawing proceeds to produce a drawn shape of intended thickness. The drawn shape has a configuration conforming to the outer surface of the male form and has an outer surface of improved uniformity and appearance due to the wiping action of the upper plate edge.
    • 用于在阳模形成金属片以产生三维形状的方法和装置。 一块金属被夹在位于阳形式上方的上和下拉板之间。 上板具有符合阳模形状的边缘。 板和片材向下移动到形式上,其中上板的边缘牢固地将纸张压靠在纸上。 当绘图继续进行以产生预期厚度的拉伸形状时,拉伸板之间的夹紧压力允许适当的滑动。 拉伸形状具有符合阳型外表面的构造,并且具有由于上板边缘的擦拭作用而具有改善的均匀性和外观的外表面。
    • 6. 发明授权
    • Reticulated core to perforate sheet bonding and galvanic barrier
    • 网状核心穿孔片材接合和电流屏障
    • US4990391A
    • 1991-02-05
    • US305515
    • 1989-02-03
    • Ross E. VetaErnest C. Millard
    • Ross E. VetaErnest C. Millard
    • B32B3/12E04C2/36G10K11/172
    • E04C2/365B32B3/12G10K11/172Y10T428/24149Y10T428/24331
    • The invention is directed a laminate structure using a reticulated adhesive material positioned between the honeycomb core and a perforate sheet and a precured reticulated adhesive between the perforated sheet and an outer layer of wire screen or other porous fibrous materials with similar pore openings therethrough through which the cells of the honeycomb core can communicate the atmosphere adjacent to the opposite side of the outer layer of porous material and a method of manufacturing same. During the manufacturing process of honeycomb noise attenuation structures which includes an imperforate sheet, an open cell honeycomb core, a perforated sheet and a layer of porous material stacked in that order a thin sheet of a reticulative adhesive material is positioned between the honeycomb core and perforated sheet and between the perforated sheet and the outer porous layer. During reticulation the reticulative material by its physical makeup shrinks to the edges of the perforations of the perforated sheet thereby leaving the perforations of both sheets of material open to the cells providing a bonding agent between the honeycomb core and perforated sheet and a similar precured layer providing galvanic isolation between the porous sheet and the perforated sheet.
    • 本发明涉及一种使用位于蜂窝芯和穿孔片之间的网状粘合剂材料的层压结构,以及穿孔板和丝网外层之间的预固化网状粘合剂或具有类似孔隙的其它多孔纤维材料, 蜂窝芯的电池可以与邻近多孔材料外层的相对侧的气氛和其制造方法相连通。 在蜂窝噪音衰减结构的制造过程中,包括无孔板,开孔蜂窝芯,穿孔板和多层材料层按顺序堆叠,薄片的网状粘合材料位于蜂窝芯和穿孔之间 并且在穿孔片材和外部多孔层之间。 在网状化期间,通过其物理成分的网状物料收缩到穿孔片材的穿孔的边缘,从而留下两片材料的穿孔向细胞开放,从而在蜂窝芯和穿孔片材之间提供粘结剂,并提供类似的预固化层, 多孔片和多孔片之间的电隔离。
    • 7. 发明授权
    • Superplastic drape forming
    • 超塑性悬垂成形
    • US4984348A
    • 1991-01-15
    • US492314
    • 1990-03-06
    • Gilbert C. Cadwell
    • Gilbert C. Cadwell
    • B21D26/055
    • B21D26/055Y10T29/4981
    • An improved method of superplastic forming comprises the steps of selecting a relatively larger driver sheet and a relatively smaller part blank, both being made of Titanium, Titanium alloy or other metal capable of exhibiting superplasticity. A ceramic die is placed on a bottom wall of an upwardly opening ceramic forming chamber having sidewalls with upper edges. The ceramic chamber has an outer supporting steel jacket. The part blank is positioned over the die. The driver sheet is positioned over the part blank so that the peripheral edges of the driver sheet rest on the upper edges of the sidewalls of the forming chamber. A cover is provided for closing the chamber. It has a peripheral seal extending from an underside thereof. The cover and the chamber are clamped together in order to impinge the seal into a periphery of the driver sheet. The driver sheet and part blank are then heated to a predetermined temperature at which they exhibit superplasticity. Next a pressurized inert gas is introduced into an interior formed by the closed cover and chamber and thereafter released so that the driver sheet presses and forms the part blank around the die. The peripheral edges of the part blank are free to draw in during the forming to thereby avoid any undesired necking or thinning. The cover is lifted from the chamber and the formed driver sheet and part blank are removed.
    • 改进的超塑性成形方法包括以下步骤:选择相对较大的驱动片和相对较小的部分坯料,它们均由钛,钛合金或能显示超塑性的其它金属制成。 将陶瓷模具放置在具有具有上边缘的侧壁的向上开口的陶瓷成形室的底壁上。 陶瓷室具有外部支撑钢外套。 零件坯料定位在模具上。 驱动片位于零件坯件上方,使得驱动片的周边部分位于成形室的侧壁的上边缘上。 提供用于封闭腔室的盖子。 它具有从其下侧延伸的外围密封件。 盖和腔被夹在一起以便将密封件撞击到驱动片的周边。 然后将驱动片和零件坯料加热至预定的温度,在此温度下它们表现出超塑性。 接下来,将加压的惰性气体引入由封闭的盖和腔室形成的内部中,然后释放,使得驱动片材压制并在模具周围形成零件坯料。 零件坯料的周边边缘在成形期间自由地拉入,从而避免任何不希望的颈缩或变薄。 将盖从室中提起并且形成的驱动片和部件坯件被移除。
    • 8. 发明授权
    • Oxidation resistant refractory coated carbon-carbon composites
    • 耐氧化耐火涂层碳 - 碳复合材料
    • US4894286A
    • 1990-01-16
    • US268015
    • 1988-11-07
    • Paul E. Gray
    • Paul E. Gray
    • C04B35/65C04B35/80C04B35/83C04B41/50C04B41/85C04B41/87
    • C04B41/009C04B35/65C04B35/806C04B35/83C04B41/5053C04B41/5096C04B41/85C04B41/87Y10S428/902Y10T428/2916Y10T428/2918Y10T428/30
    • An oxygen resistant high temperature composite structure comprises a carbonous matrix and reinforcing high temperature fibers disposed within said matrix, an outer refractory coating covering said matrix, boron, in elemental form and/or as a moiety of a compound dispersed throughout said structure, silicon, in elemental form and/or as a moiety of a compound dispersed throughout said structure, and titanium, in elemental form and/or as a moiety of a compound dispersed throughout said structure, said silicon and said boron oxidizing when exposed to a high temperature, oxidizing environment to form silicon oxide and boron oxide, and said titanium forming titanium oxide which stabilizes the molten phase of the boron oxide. Microcracks which form in the refractory coating are sealed by a molten glass which forms from oxidation of the boron, silicon and titanium, thereby preventing oxidation degradation of the underlying matrix.
    • 耐氧高温复合结构包括碳基质和设置在所述基质内的增强高温纤维,覆盖所述基质的外部耐火涂层,元素形式的硼和/或分散在所述结构中的化合物的部分,硅, 元素形式和/或分散在整个结构中的化合物的部分,以及分散在整个结构中的化合物的元素和/或部分的钛,暴露于高温时所述硅和所述硼氧化, 氧化环境形成氧化硅和氧化硼,以及形成氧化钛的钛形成氧化钛,其稳定氧化硼的熔融相。 在耐火涂层中形成的微裂纹由从硼,硅和钛的氧化形成的熔融玻璃密封,从而防止下面的基质的氧化降解。
    • 9. 发明授权
    • Filament winding process
    • 丝卷绕过程
    • US4869761A
    • 1989-09-26
    • US97696
    • 1987-09-17
    • Oscar WeingartGerald A. LundeClark D. Taylor
    • Oscar WeingartGerald A. LundeClark D. Taylor
    • B29C53/56B29C53/80
    • B29C53/566B29C53/8016
    • A filament winding payoff unit and process for applying strands of adhesive impregnated filament material arranged into a gap-free band to a rotating mandrel. A plurality of side-by-side slightly overlapped impregnated filament strands are passed over bars between tines of combs for positioning when leaving the payoff head. The payoff head is positionable toward and away from the rotating mandrel to allow for mandrel longitudinal dimension changes while maintaining the payoff head roller in contact with the mandrel at a predetermined pressure thereagainst. The payoff head is also freely pivotable horizontally to maintain a proper angle of filament application to any changing mandrel longitudinal configuration.
    • 长丝缠绕支付单元和用于将布置在无间隙带中的粘合剂浸渍的长丝材料线施加到旋转心轴的方法。 多个并排的稍微重叠的浸渍的细丝股线在梳齿之间的条上通过,用于当离开收益头时进行定位。 发射头可朝向和离开旋转心轴定位,以允许心轴纵向尺寸变化,同时保持发射头辊在心轴处以预定压力接触。 发射头也可以水平自由地枢转,以保持灯丝施加到任何变化的心轴纵向配置的适当角度。
    • 10. 发明授权
    • Cutting abrasive feeder, demand type
    • 切割磨料进料器,需求型
    • US4829724A
    • 1989-05-16
    • US142445
    • 1988-01-11
    • Fred W. Miller, Jr.Forrest W. SweatDale L. Jennings
    • Fred W. Miller, Jr.Forrest W. SweatDale L. Jennings
    • B24C7/00
    • B24C7/0053B24C7/0076Y10T137/4891
    • The invention is directed to an improved hopper for feeding abrasive material of very small grit size to a cutting head. The device comprises an open hopper vertically disposed with a transverse positioned pick-up tube located in the lower portion of the hopper. The pick-up tube has a tubular center with a necked down diameter intermediate of its's ends. An opening extends from the bottom of the tube into the tubular center at a location centered in the necked down portion thereof. One end of the tube is vented to atmosphere through an adjustable orifice and the other end is connected to a source of low pressure created within the mixing chamber of the nozzle body assembly by high pressure water passing across the open end of the tube. This effect causes abrasive grit to be drawn through the opening in the bottom of the tube out the low pressure end of the tube to the cutting head. The flow of abrasive is regulated by controlling inlet/outlet air stream mass air flow or in combination with varying abrasive inlet sizes. The device is a passive, demand system, eliminating the need for mechanically controlled abrasive flow.
    • 本发明涉及一种用于将非常小的砂粒尺寸的研磨材料供给切割头的改进的料斗。 该装置包括垂直设置有位于料斗下部的横向放置的拾取管的开放料斗。 拾取管具有管状中心,其中心具有缩小的直径。 开口从管的底部延伸到管状中心的中心在其颈缩部分的位置处。 管的一端通过可调节的孔排放到大气中,另一端通过穿过管的开口端的高压水连接到在喷嘴体组件的混合室内产生的低压源。 这种效应使得磨料砂粒通过管的底部的开口从管的低压端拉出到切割头。 研磨剂的流动通过控制入口/出口空气流质量空气流量或与不同的研磨入口尺寸组合来调节。 该设备是一种无源的需求系统,无需机械控制的磨料流。