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41results about How to "Reduced fretting wear" patented technology

Combined artificial hip joint cup

InactiveCN105030380AReduce stress concentrationReduces risk of fretting wear and liner breakageJoint implantsCoatingsIonCorrosion
The invention relates to a combined artificial hip joint cup in a concave semi-arc shape. The combined artificial hip joint cup comprises an outer layer and an inner layer; the outer layer is provided with screw holes; the outer layer is made of biocompatible material; the inner layer is made of polyetheretherketone or its derivative polymer material; the inner layer and the outer layer are integrally fixed; the screw holes are covered by the inner layer. The joint of the surface of the PEEK (polyetheretherketone) inner layer and the outer surface of a different cup liner may reduce stress concentration and reduce the risk of fretting wear and liner damage; or the inner surface of the PEEK inner layer and the outer surface of a femoral prosthesis directly form a friction pair, decreasing wear of the outer surface of the femoral prosthesis. The surface of the PEEK inner layer has the advantages of corrosion resistance and fretting wear resistance, and the release of existing metal ions and granules of metal prostheses, causing harm to the human body, is avoided.
Owner:JIANSU OKANI MEDICAL TECH CO LTD

Grid supporting piece

The invention discloses a grid supporting piece. The grid supporting piece comprises an annular frame and a grid assembly arranged in the annular frame, the grid assembly comprises a plurality of highsupporting strips and a plurality of low supporting strips, the high supporting strips are provided with a plurality of first inserting grooves formed at intervals, the high supporting strips comprise first high supporting strips and second high supporting strips, a plurality of second inserting grooves are formed between every two adjacent first inserting grooves in the high supporting strips, and the low supporting strips are inserted into the second inserting grooves of the first high supporting strips and the second high supporting strips in an embedded mode. According to the grid supporting piece, the first high supporting strips and the second high supporting strips are mutually inserted and embedded, the high supporting strips and the low supporting strips are mutually inserted andembedded, a self-locking stable supporting assembly is formed, the high supporting strips and the low supporting strips are in a strip shape, the structure formed by mutual embedding of the high supporting strips and the low supporting strips has certain flexibility, uneven thermal expansion of a heat exchange pipe can be compensated, the grid supporting piece has good performance of preventing the heat exchange pipe from vibrating, so that the possibility of micro-vibration abrasion is reduced, and the grid supporting piece is applied to the technical field of steam generators.
Owner:DONGFANG (GUANGZHOU) HEAVY MASCH CO LTD

Micro turbine for aero-engine

The invention discloses a micro turbine for an aero-engine. The micro turbine comprises a turbine disc, and turbine blades sequentially distributed on the turbine disc along the circumferential direction of the turbine disc, wherein the turbine disc further comprises locking pipes used for locking the turbine blades in corresponding mortises on the turbine disc; the locking pipe is arranged at theconnecting position of the small end of a tenon and the mortise of the turbine blade; and the locking pipe deforms under the action of external force punching and riveting so as to be squeezed in thetenon and the mortise at the same time to lock the turbine blade, and then the turbine blade is prevented from moving backwards towards the exhaust end of the turbine. According to the micro turbinefor the aero-engine, due to the fact that deformation of the locking pipes under the action of punching and riveting force is spatial multi-dimensional deformation, the positioning locking tightness of the locking pipes to the turbine blades is larger than the locking tightness of locking pieces, and therefore the turbine blade can be effectively prevented from moving backwards towards the exhaustend of the turbine, and then the breaking fault of the turbine blade occurring after the turbine blade scrapes a rear stator is reduced; and the turbine blades are high in positioning tightness, so that the fretting wear of the tenon contact surface is small, and the vibration stress of the tenon contact surface is small.
Owner:CHINA HANGFA SOUTH IND CO LTD
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