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

77results about How to "High mechanical load capacity" patented technology

Manufacturing method of multilayer shell-core composite structural part

The invention discloses a manufacturing method of a multilayer shell-core composite structural part, which comprises the following steps of: (1) respectively preparing feed for injection forming of a core layer, a transition layer and a shell layer, wherein powder in the feed of the core layer and the powder in the feed of the shell layer are selected from one or a mixture of some of metal powder, ceramic powder, or toughened ceramic powder and are different from each other, and the powder in the feed of the transition layer is gradient composite powder; (2) respectively manufacturing blanks of the multilayer shell-core composite structural part layer by layer with a powder injection forming method; (3) degreasing the blanks; and (4) sintering the blanks to obtain the multilayer shell-core composite structural part. The multilayer shell-core composite structural part is manufactured with the powder injection forming method, and has the advantages of high surface hardness, abrasion resistance, uniform thickness of the shell layer, stable and persistent performance, strong binding force between the shell layer and the core layer due to the transition layer, good integral bending strength and good impact toughness and is difficult to crack.
Owner:SUZHOU DINGAN ELECTRONICS TECH

Lightweight structure, particularly primary aircraft structure or subassembly, as well as method for the manufacture thereof

InactiveUS20130115404A1High mechanical load-bearing capacityLow weightLayered productsOrnamental structuresAirplaneSatellite
A lightweight structure at least sectionally composed of a plurality of connected mosaic elements and / or skin mosaic elements. The lightweight structure allows an essentially load-appropriate arrangement of the mosaic elements and / or the skin mosaic elements including the optional skin. The lightweight structure requires a significantly reduced number of connecting elements, such that the assembly effort can be reduced and an additional weight reduction can be achieved. Also, two variations of a method for manufacturing a lightweight structure are provided. Large-format lightweight structures such as, for example, an aircraft fuselage cell or partial shells thereof can also be manufactured in a reliable and dimensionally accurate fashion because only mosaic elements and skin mosaic elements, with relatively small dimensions, need to be handled. Other applications of the lightweight structure include launch vehicles, rocket stages, space stations, space station modules, satellites and masts or towers of wind power plants.
Owner:AIRBUS OPERATIONS GMBH

Floor panel for forming a loading area in a cargo hold of an aircraft

InactiveUS20080173755A1Minimal useBetter load distributionFuselage framesStrutsAirplaneEngineering
Disclosed is a floor panel, in particular for covering floors of cargo holds of aircraft. The floor panel is formed by a plurality of milled profiles, which are friction stir welded in each case along their longitudinal edges, with preference continuously to form longitudinal (butt) seams. The milled profiles each form a beam “of equal stress”, with an upper flange and a lower flange which are spaced apart from one another along their extent. The milled profiles have in each case a double-T-shaped cross-sectional profile, the upper flanges and the lower flanges being respectively connected by webs. With preference, the milled profiles are milled out in one piece from solid material of a sufficiently tough aluminium alloy. The joining together of the floor panel including a plurality of milled profiles that are arranged in parallel and friction stir welded allows a high mechanical load-bearing capacity of the floor panel in comparison with conventional sandwich floor panels along with a comparatively low weight.
Owner:AIRBUS OPERATIONS GMBH

Hollow chamber structural component and method for producing same

A hollow chamber structural component includes a shell component which extends along a main extension direction. A cover component is attached to the shell component, wherein a hollow chamber is disposed between the shell component and the cover component and extends in the main extension direction. A reinforcing structure is arranged in the hollow chamber and comprises: a synthetic support structure, which follows at least in some sections the main extension direction and rests with at least some sections against an inside of the shell component; and at least one reinforcing element that follows at least in some sections the main extension direction and is joined to the synthetic support structure with the aid of a layer of adhesive.
Owner:REHAU AG CO

Medical or dental hand-piece element

There is disclosed a medical or dental hand-piece element comprising a coupling mechanism for a detachable connection of the hand-piece element to a drive unit, a tool receptacle that is or can be connected to the hand-piece element, and a drive element for transmitting a driving movement from the drive unit to the tool receptacle so that the tool receptacle can be set into a working movement, wherein the drive element comprises at least one rotatable shaft, and a generator for converting mechanical energy into electric energy, wherein the generator can be driven by the at least one rotatable shaft of the drive element.
Owner:W&H DENTALWERK

Heat conduction and load bearing integrated light sandwiched panel with lattice structure and preparation method thereof

The invention relates to a heat conduction and load bearing integrated light sandwiched panel with a lattice structure and a preparation method of the heat conduction and bearing integrated light sandwiched panel, aiming at solving the problems that the existing sandwiched panel with the lattice structure has poor heat conducting property and single structure performance. The heat conduction and load bearing integrated light sandwiched panel is composed of an upper panel, a sandwiched layer with a lattice structure and a lower panel, and the sandwiched layer with the lattice structure is composed of an upper reinforcing mesh, multiple pyramid lattice structure unit cells, a lower reinforcing mesh and a carbon foam sandwiched panel. The preparation method comprises the following steps: I. preparing a cylindrical rod; II. preparing the foam sandwich panel; III. preparing the upper reinforcing mesh and the lower reinforcing mesh; IIIV. preparing the sandwiched layer with the lattice structure; and V. preparing the sandwiched panel with the lattice structure. The heat conduction and load bearing integrated light sandwiched panel with the lattice structure can be used for solving the problems that the existing sandwiched panel with the lattice structure has poor heat conducting property and single structure performance, and when the light multi-functional sandwiched panel is subjected to action of thermal loading, the panel with high heat conducting property and the carbon foams with high heat conducting property form a heat conducting passageway, so that the heat conducting property of the light multi-functional sandwiched structural panel is improved.
Owner:HARBIN INST OF TECH

Preparation method of special-shaped carbon fiber composite I-beam and special-shaped I-beam prepared through method

The invention provides a preparation method of a special-shaped carbon fiber composite I-beam and the special-shaped I-beam prepared through the method. The preparation method of the special-shaped carbon fiber composite I-beam comprises the steps that a setting agent is scattered on carbon fiber fabric according to the mass of 3-8 g / m<2>, heat setting is conducted, the fabric is cut into the required shape through a cutting machine after setting of the carbon fiber fabric is completed, the fabric cut into the specific shape is laid on a mold prepared in advance in an attached mode, so that a prefabricated body is obtained, and the prefabricated body is placed in a vacuum bag to be stored in an airtight mode after laying is completed; composite liquor is formed, so that a crude special-shaped carbon fiber composite I-beam is obtained; and the finished special-shaped carbon fiber composite I-beam is obtained by treating the crude special-shaped carbon fiber composite I-beam. The special-shaped carbon fiber composite I-beam is high in bearing capacity, good in rigidity, low in self weight and high in surface smoothness, the porosity of a product is low, and the outer surface dimension and the resin content can be controlled accurately.
Owner:HENGSHEN

Structural Health Monitoring System for a Material and Production Method

A structural health monitoring system includes a signal transmission element and a sensor unit. The sensor unit is designed to feed a first signal into the signal transmission element and to read out a second signal from the signal transmission element. The signal transmission element has carbon nanotubes.
Owner:AIRBUS DEFENCE & SPACE

Backflow preventer

The invention relates to a backflow preventer having a housing, which has an inlet opening, an outlet opening and at least one leakage opening disposed between these openings and accommodates first and second nonreturn valves disposed in series, the first nonreturn valve being held displaceably in order to open up and close a flow connection between an intermediate space of the housing and the leakage opening. To develop the backflow preventer in such a manner that an inadmissible increase in pressure in the region of the outlet opening can be avoided in a structurally simple way, according to the invention it is proposed that the housing comprises an inner housing and an outer housing, the outer housing having the at least one leakage opening and the inner housing accommodating the two nonreturn valves and being held such that it can be displaced to and fro in the direction of through-flow within the outer housing, and the inner housing having an outlet opening, via which the flow connection between the intermediate space and the leakage opening can be produced independently of the position of the inner housing, by displacement of the first nonreturn valve relative to the second nonreturn valve.
Owner:ALFRED KARCHER GMBH & CO KG

Fabric punched felt complex and preparation method thereof

The invention provides a fabric punched felt complex and a preparation method thereof. The preparation method comprises the following steps: compounding a continuous functional fiber fabric layer and a continuous functional fiber bulked yarn crude fabric layer together so as to obtain integrated fabric; then compounding a chopped functional fiber punched felt layer with the continuous functional fiber bulked yarn crude fabric layer of the integrated fabric through needling so as to obtain the fabric punched felt complex. The fabric punched felt complex has a light and high strength structure with stepped intensity changes. The weight of the fabric punched felt complex is 30% lighter than that of complete fabric with a same volume, while the mechanical performance of the fabric punched felt complex is equal to that of complete fabric with a same volume, and is better than that of complete chopped fiber punched felt. At the same time the fiber raw material is saved by 30% or more, moreover the preparation technology is simple, and the production period is short.
Owner:HUNAN JIUHUA CARBON HI TECH

Structural composite wave-absorbing material and preparation method thereof

PendingCN112312754AGood level interface compatibilityWide absorption bandwidthShielding materialsFrequency bandFibre reinforcement
The invention discloses a structural composite wave-absorbing material and a preparation method thereof, which belong to the technical field of materials. The structural composite wave-absorbing material is composed of a fiber-reinforced resin-based composite material, an absorbent and a metamaterial wave-absorbing structure. Different layers of fiber cloth are uniformly coated with resin and a mixture of resin and absorbent and are combined with the metamaterial wave-absorbing structure to form a laminated structure to obtain the wave-absorbing material. According to the composite wave-absorbing material with the structure, the bearing mechanical property of the composite material structure is maintained, meanwhile, the material absorption bandwidth is effectively widened, and strong absorption of key frequency bands is realized.
Owner:AEROSPACE INST OF ADVANCED MATERIALS & PROCESSING TECH

Half-chip assembly

The invention provides a half-chip assembly, comprising a plurality of solar cell strings and a junction box, wherein, a plurality of solar cell strings are arranged in parallel, and each solar cell string comprises a plurality of half-chip cells connected in series; The number of solar cell strings is an integer multiple of 4. The positive and negative electrodes of the solar cell strings in eachgroup are arranged in the same direction, and the positive and negative electrodes of the solar cell strings in the two adjacent groups are arranged in the opposite direction. The solar cell string in each group is connected in parallel to form a solar cell string group through a bus bar, and the adjacent solar cell string groups are connected in series to form a battery loop through the bus bar,and the positive and negative electrodes of the battery loop are located on the same side of the half-chip module. The junction box is arranged on the same side as the positive and negative electrodes of the battery circuit, and the bus bar on the same side as the positive and negative electrodes of the battery circuit is connected into the junction box, and the positive and negative electrodes of the half-piece assembly are led out from the junction box. The half-chip assembly provided by the invention has high reliability and high conversion efficiency.
Owner:CHINT NEW ENERGY TECH (HAINING) CO LTD

Plug-in combination of devices

The present invention relates to a plug-in apparatus combination with an apparatus base and a plug-in module, wherein, the plug-in module can be plugged into the apparatus base. The apparatus base has a base housing with a recess for receiving the plug-in module, a linkage terminal for a conductor of a power grid to be protected, and a plug-in contact linked with the linkage terminal. The plug-in module has a plug housing, a protective element arranged in the plug-in housing, and a linkage plug-in contact corresponding to the plug-in contact. In the apparaut combination, locking and replacement of the plug-in module are executed thereby, namely, a latching linkage portion acting between the apparatus base and the plug-in module has a latching arm with a latching mechanism and a groove, the latching linkage portion is arranged on the wall opposite to the latching arm, a latching hook of the latching arm is used for guding when the plug-in module is plugged into the apparatus base. The groove has a first region, a second region, and a third region, and the deepth of the groove is too small in the end of the third region so that the latching hook does not guide in the groove.
Owner:PHOENIX CONTACT GMBH & CO KG
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