Insertion device for deformable intraocular lens

    公开(公告)号:US07037312B2

    公开(公告)日:2006-05-02

    申请号:US10222419

    申请日:2002-08-16

    IPC分类号: A61B17/00

    CPC分类号: A61F2/1678 A61F2/167

    摘要: An intraocular-lens insertion device is adapted to deform a deformable intraocular lens into a smaller size and insert the intraocular lens into an eye via an insertion tube. An intraocular-lens guide is provided on the inner surface of the insertion tube. The guide may be a rail-shaped projection or a groove, which extends parallel to a direction along which the intraocular lens is pushed out. A stress release structure is provided on the insertion tube in order to release stress of the intraocular lens produced due to deformation thereof. Moreover, a frictional-resistance increasing structure is provided on the inner surface of the insertion tube to be located in the vicinity of the stress release structure. The frictional-resistance increasing structure increases frictional resistance between the inner surface of the insertion tube and the intraocular lens. The frictional-resistance increasing structure may be a roughened surface which completely or partially covers the inner surface of the insertion tube.

    Composition for toothbrushing
    5.
    发明申请
    Composition for toothbrushing 审中-公开
    刷牙用组合物

    公开(公告)号:US20070166243A1

    公开(公告)日:2007-07-19

    申请号:US10589396

    申请日:2005-03-22

    IPC分类号: A61K8/73

    CPC分类号: A61Q11/00 A61K8/731

    摘要: Provided is a dentifrice composition excellent in plaque and stain removing effect and feeling upon use. The dentifrice composition has the following components (A), (B) and (C): (A) from 0.2 to 3 weight % of powder cellulose; (B) a surfactant; and (C) from 10 to 30 weight % of an abrasive.

    摘要翻译: 本发明提供了一种洁牙剂组合物,其在斑块和除斑效果以及使用感上均优异。 洁齿剂组合物具有以下组分(A),(B)和(C):(A)0.2至3重量%的粉末纤维素; (B)表面活性剂; 和(C)10至30重量%的研磨剂。

    Aircraft engine run-up hangar
    6.
    发明授权

    公开(公告)号:US06637168B2

    公开(公告)日:2003-10-28

    申请号:US10114155

    申请日:2002-04-03

    IPC分类号: E04F1708

    CPC分类号: E04H6/44 B64F1/26 Y10S454/906

    摘要: An aircraft engine run-up hangar comprises a building defining a test chamber capable of receiving an aircraft therein, an air inlet structure, and an exhaust structure. The air inlet structure is formed in a front end part of a roof structure corresponding to a front end part of the building, the exhaust structure is connected to a rear end part of the building and defines an exhaust passage extending obliquely upward from the back end of the building, and one or a plurality of current deflecting members are disposed near a lower end of the air inlet structure to deflect air currents flowing through the air inlet structure into the building toward an aircraft housed in the building. A current-straightening structure is incorporated into the air inlet structure. A current-straightening space is defined under the air inlet structure. A first current-straightening member, a second current-straightening member, a third current-straightening member and a fourth current-straightening member are disposed in a region in and around the current-straightening space.