子分类：
| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 361 | COMPOSITE TUBE ASSEMBLIES AND METHODS | US14267720 | 2014-05-01 | US20150316206A1 | 2015-11-05 | Rony Giovanni Ganis; Peter F. Giddings |
| Composite tubes comprising a compression sleeve coupled to an inner surface of a composite tube, a carbon extrusion member disposed within the composite tube, and an end fitting comprising a locking feature, wherein the end fitting is coupled to an inner surface of the compression sleeve and the locking feature is configured to engage the carbon extrusion member are disclosed. Methods comprising coupling a compression sleeve to an inner surface of a distal end of a composite tube, placing a carbon extrusion member inside the compression sleeve and the composite tube, and disposing an end fitting on the distal end of the composite tube, wherein the end fitting comprises a locking feature configured to interact with the carbon extrusion member are also disclosed. | ||||||
| 362 | METHOD FOR CONNECTING HOLLOW PROFILES | US14672480 | 2015-03-30 | US20150283756A1 | 2015-10-08 | Markus Flaig; Philipp Scheiner |
| A method is provided for connecting hollow profiles (1-4) in a joint (10) to produce a load-bearing structure (5). The method includes placing ends of hollow profiles (1-4) in a mold and pressing the ends together with at least one semi-finished product to connect the ends of the hollow profiles to the semi-finished product. | ||||||
| 363 | Slit tube locking longeron | US13331941 | 2011-12-20 | US08863369B2 | 2014-10-21 | Robert Taylor; Dana Turse; Larry G. Adams; Mark Reavis; Doug Richardson |
| According to the invention, an extendable member is disclosed. The extendable member may include a structure having a first state and a second state. The structure may be deformable between the first state and the second state. In the first state the structure may include a compact form. In the second state the structure may include a hollow longeron having a slit along the entire length of the hollow longeron. One or both longitudinal edges along the slit of the hollow longeron may have lateral protrusions. The lateral protrusions of a longitudinal edge may act in such a way with the other edge, and possibly its protrusions, to at least partially inhibit relative motion of the edges. | ||||||
| 364 | FITTING BODY | US14011876 | 2013-08-28 | US20140064845A1 | 2014-03-06 | Kurt MUELLER; Alfons STACHEL; Jurgen BAUMANN |
| A fitting body having at least one fitting unit is produced, at least to a large part, from a material having a density of less than 7000 kg/m3. | ||||||
| 365 | FLOW-CONTROL DEVICE, COMPONENT HAVING A FLOW-CONTROL DEVICE, AND METHOD OF PRODUCING A FLOW-CONTROL DEVICE | US13690438 | 2012-11-30 | US20130255796A1 | 2013-10-03 | Paul Stephen DIMASCIO; Rebecca Evelyn HEFNER |
| A flow-control device, a component, and method of producing a flow-control device are disclosed. The flow-control device includes thermally-adjustable features positioned along a surface of the flow-control device configured to be adjacent to a flow, and a heating member in direct or indirect contact with the thermally-adjustable features. The thermally-adjustable features deploy from or retract toward the surface in response to a predetermined temperature change provided by the heating member. The deploying from or the retracting toward of the thermally-adjustable features increases or decreases turbulation of the flow along the surface. The component includes the flow-control device. The method includes forming the thermally-adjustable features along the surface of the flow-control device, in direct or indirect contact with a heating member. The thermally-adjustable features deploy from or retract toward the surface in response to a predetermined temperature change provided by the heating member. | ||||||
| 366 | Systems and methods for value bearing indicia balance reservation | US11970933 | 2008-01-08 | US08027935B1 | 2011-09-27 | Geoffrey Charles Begen |
| Systems and methods which operate to reserve an amount of value associated with a value bearing indicia (VBI) request or requests are shown. Embodiments facilitate completion of a multiple VBI session without failing due to insufficient value balance once the session has begun. Additionally or alternatively, embodiments facilitate later or subsequent (e.g., scheduled) completion of a VBI session, whether a session for a single VBI or multiple VBI, without failing due to insufficient value balance. Value reservations may be made automatically and/or manually. Embodiments provide various reservation priority levels, such as to individual users, user groups, user systems, sessions, types of sessions, jobs, etc., in order to facilitate completion of various desired operations without failure due to insufficient value. Value reservation techniques according to embodiments do not introduce additional transactions into a normal VBI session flow. | ||||||
| 367 | Mounting element | US09529772 | 2000-06-02 | US06398448B1 | 2002-06-04 | Albrecht Benz; Joerg Walther; Torsten Buenning; Frank Rahnfeld; Olaf Kelmd |
| A mounting element (12, 12a, 12b) for securing components, in particular profile bars, and a cap (14, 14a, 14b) for covering the mounting element (12, 12a, 12b) are provided. Indentations (31, 39) are provided in lateral ribs (22, 36) of the mounting element (12, 12a, 12b) and/or of the cap (14, 14a, 14b). This makes the grip better and/or facilitates aligning the mounting element (12, 12a, 12b) and/or the cap (14, 14a, 14b). | ||||||
| 368 | Stress steering structure | US338408 | 1994-11-14 | US5615528A | 1997-04-01 | Charles R. Owens |
| A load bearing structure having a set of uniform voids functions to resolve the forces imposed by developing compression in the material having the voids and minimizing the amount of tension developed in the material. For the voids to have this function, they must be deployed in a particular fashion. The voids are deployed to encompass a particular set of points. The set of points are such that each point in the matrix is spaced an equal distance from twelve and only twelve adjacent points of the matrix. The distance between the points does not matter as long as all are uniformly distanced in accordance with that rule. If the structure is considered to be composed of a closely packed set of hypothetical rhombic dodecahedra (RD) and the four edge vertices of each of those hypothetical RDs is truncated, the result will be a set of cubic voids. The center of each of those cubic voids will define the matrix referred to above and the cubic voids will serve to provide the optimum resolution of stress which minimizes the development of tension in the material. One in four of the hypothetical or mathematical RDs can be eliminated achieving the same force resolution result in a structure that contains less material. The shape and size, but not the position, of the voids can be varied with only slight loss in optimum stress resolution. Some voids can be omitted with only slight loss of optimum stress resolution. | ||||||
| 369 | Design and construction module | US466106 | 1995-06-06 | US5575120A | 1996-11-19 | Frederick G. Handley |
| A design and construction module comprised of nine cells each having substantially equal lengths, widths and heights and longitudinally opposed ends. Two of the cells form the base of the module and are located side-by-side with their ends terminating adjacent and flush with one another. Three of the cells form an intermediate level of cells located above the base cells. Two of these intermediate cells correspond with the two base cells and are located immediately thereabove, but longitudinally offset. In this way these two intermediate cells extend a predetermined distance beyond the one end of the base cells in an overhang. Opposite the overhang, the third cell of the intermediate cells extends transversely with respect to the two other intermediate cells and the base cells. A portion of the third intermediate cell therefore laterally extends beyond the side of the base cells. Three additional cells define a common top surface of the module. The three top cells are each positioned directly above one of the intermediate cells. A final cell extends perpendicular to the base, intermediate and top cells. With the above construction, the module of this invention is adapted for interlocking engagement with one or more additional modules to aid in the designing and construction of various structures including terrestrial, marine and aeronautical structures. | ||||||
| 370 | Method of constructing flat building block modules from the union of two frustums by their congruent bases and slot connectors complement for a variety of constructive or amusing applications | US436665 | 1989-11-15 | US5168677A | 1992-12-08 | Antonio C. Pronsato; Ernesto D. Gyurec |
| A method to guide the creation of flat modular building block units to be interconnected with others of like shape by means of fasteners and magnetically, the modules are created by the union of any two frustums by a congruent larger base, a series of holes truncations and roundings made them fit in a variety of constructive and amusing applications, also complementing the invention is a built-in slot connector for connecting two flat members. | ||||||
| 371 | Modular universal construction units employing flexible web with interlockable heads | US432461 | 1989-11-06 | US5016417A | 1991-05-21 | Robert Mentken |
| A prefabricated adaptable lightweight hollow core construction system comprising at least a unit (30) which may be extruded of plastic and which comprises a plurality of compression-resistant, flexibly connected, elongated, hollow element pairs (40). Each pair comprises a triangular base element protruding from one side of a flat flexible sheet and an octagonal head element flexibly connected to the uppermost angle of the base element. Element pairs have undersized spaces (42) between them adapted to receive elements in interlocking engagement. Adjacent head elements (36) may be manually swung apart on flexible connections (38) and forced into adjacent undersized negative spaces (42) to subsequently form rigid right-angle corners at incremental points (34a) or other shapes formed (41, 32a, 34c, 34d, 34e) along the unit. Elements of a second unit (30a) may be alternately and sequentially interlocked with those remaining elements of the first unit that are not engaged in corner formation. This rigidly extends the straight sides of right-angle corners. Forced interlocking produces high compression/tension values with concomitant rigidity within and throughout assembled constructions. Force to produce high compression/tension values is generated by leverage action of partially interlocked elements (36), one upon another between the manually driven element and the element with the highest values. Units may have an additional integral fastener (52) and/or auxiliary fasteners (54, 55, 56, 57, 58) to secure end elements (48), and rigid connectors (60, 66), or flexible connectors (61) for attachment of additional units and accessories (62, 64, 68); a cutting guide for accurate removal of unit portions (44). The unit requires no skill to assemble and can be reused. Unused portions may be used in future constructions and existing constructions may be disassembled and its units readapted into new constructions. | ||||||
| 372 | Assemblable structures | US139452 | 1980-04-11 | US4343117A | 1982-08-10 | Norman S. Shemitz |
| Structures including buildings, furniture items or room partitions are formed by assembling panels and releasably connecting the panels together with a support system comprising collars on the corners of the panels and elastic members interconnecting these collars so as to hold the structure together into a predetermined form by virtue of the tension of the stretched elastic members. Structures formed by this system include building structures such as small outdoor shelters, furniture items such as display cases, bookshelves, tables and containers and room partitions of virtually any arrangement, and toys. | ||||||
| 373 | Corrugated plate having variable material thickness and method for making same | US962365 | 1978-11-20 | US4241146A | 1980-12-23 | Eugene W. Sivachenko; Firoze H. Broacha |
| A corrugated plate is disclosed which has trapezoidal corrugations defined by alternating, side by side, relatively thick corrugation peaks and corrugation troughs and relatively thin, inclined corrugation sides which interconnect edges of adjoining peaks and troughs. A method is also disclosed for corrugating the corrugated plate from flat sheet by providing a flat sheet with spaced apart, longitudinally extending, relatively thick sections which thereafter define the corrugation peaks and corrugation troughs or for forming the thick sections by providing a relatively thin sheet and folding over portions of the thin sheet in the areas which ultimately form the corrugation peaks and corrugation troughs so that the latter are defined by a plurality of staked sheet layers. | ||||||
| 374 | Light weight tension-compression equilibrium structures | US595853 | 1975-07-14 | US4156997A | 1979-06-05 | Bert J. Decker, deceased; Jean S. Decker, executrix |
| Light weight tension-compression equilibrium structures include structural units which contain a plurality of compression members in contact with each other in an interior portion of the unit and a plurality of tension members in contact with them and exerting balanced tensions on them to hold them in position with respect to each other, and to produce compressive forces in the compression members which are directed toward the point(s) of contact of the compression members in the interior of the unit, thereby strengthening the compression members and the structural units. The tension members are positioned apart such distances along the compression members less than lengths at which the compression members alone would buckle under applied compressive forces. The various structural units may be essentially planar, useful for forming walls or relatively thin supporting structures, or they may be made three-dimensional so as to be capable of serving as major load-bearing units. Various types of tension-compression equilibrium structures are illustrated, including parallelepipedal units wherein the compression members are interlocking twin tetrahedrons or such tetrahedrons internally braced by compression members or "planes" connecting the intersections of diagonals of the parallelepiped sides, or parallelepipeds made from a plurality of essentially planar tension-compression units and such structural units and pluralities of them joined together, preferably with additional tension parallelepipeds between them and exerting tension thereon, may be employed as load-bearing components of buildings, bridges, tunnels, subways towers, stanchions, dams, roadways and various other structures. | ||||||
| 375 | Prismatic interlocking structural module | US826112 | 1977-08-19 | US4095386A | 1978-06-20 | Joseph Daniel Johnson |
| A structural module is provided having at least three triangular prismatic elements arranged such that a similar quadrangular sidewall of each prismatic element forms a common quadrangular wall of the entire module. | ||||||
| 376 | Cuboidal structures | US20008171 | 1971-11-18 | US3813841A | 1974-06-04 | TSURUMI S |
| The present invention relates to the assembling matters such as blocks which are solid and stout and have excellent fittability or joinability to one another, such matters being capable of forming face plates of perfectly same configuration adapted to constitute the respective sides or faces of a six-sided cubic structure which can be easily assembled or disassembled and which can be utilized for a variety of purposes such as for building, construction, many types of utensiles, structures, toys and so forth.
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| 377 | Modular louver structure | US39629864 | 1964-09-14 | US3291978A | 1966-12-13 | IRVING GREENBERG; MARCHHART FRANK J |
| 378 | Acceleration belt and stocking for aviators | US41067241 | 1941-09-13 | US2397710A | 1946-04-02 | VERSOY IRVING R; LOEFFEL LESTER H |
| 379 | BASE PLATE UNIT | US15536355 | 2015-11-20 | US20180327180A1 | 2018-11-15 | Shuang HE; Fuyou WANG; Wen PENG |
| Provided is a base plate unit, which is of an integrated structure made of fiber reinforced polymer-matrix composite and comprises a base plate unit body and foot plates. The base plate unit body comprises at least one bearing part, each bearing part comprising a panel, a plurality of web plates extending downwards from the bottom of the panel, and bottom supports disposed at the lower end of the web plates. The web plates comprise two side-web plates on the two sides of the panel and a middle web plate in the middle. The foot plates are disposed on the two outer sides of the bottom of the base plate unit body, and are formed by the bottoms of the two side-web plates on the outmost side of the base plate unit body respectively extending outwards horizontally. Also provided is a base plate unit provided with a cavity filling member. | ||||||
| 380 | GRID FLAP | US15963749 | 2018-04-26 | US20180310772A1 | 2018-11-01 | Andreas Peters; Felix Profe |
| The present application deals with a grid flap, comprising a multiplicity of vertical and horizontal grid struts, a frame which surrounds the grid struts, wherein a vertical and a horizontal grid strut respectively overlap in a crossing point, characterized in that the crossing points of the grid struts are made of one piece. As the grid is self-supporting because of its topology (made of one piece) and the overlapping of two grid struts can be avoided, double areas or cavities can be avoided, which contributes to a hygienic design of the grid flap. | ||||||
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