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1. 发明授权

US6138568A Planographic printing member and process for its manufacture 失效
标题翻译：普通印刷机构及其制造工艺
公开(公告)号：US6138568A
公开(公告)日：2000-10-31
申请号：US366489
申请日：1999-08-03
申请人： Christopher D. McCullough , Kevin B. Ray , Michael S. Yates , Colin J. Griffiths , Mark J. Spowage , Peter A. R. Bennett , Harjit S. Bhambra
发明人： Christopher D. McCullough , Kevin B. Ray , Michael S. Yates , Colin J. Griffiths , Mark J. Spowage , Peter A. R. Bennett , Harjit S. Bhambra
IPC分类号： B41C1/10 , B41N1/14 , B41N3/03
CPC分类号： B41C1/1033 , B41N1/14 , B41N3/038
摘要： A planographic printing member comprising a substrate, an oleophilic layer, an infra-red sensitive/ablatable layer, and a hydrophilic layer. The hydrophilic layer is derived from a silicate solution, optionally containing particulate materials such as alumina and/or titania. The printing member may be exposed to radiation from a laser which ablates the infra-red sensitive/ablatable layer to reveal areas of the oleophilic layer. An exposed printing member may be used in wet lithographic printing.
摘要翻译：平版印刷构件，包括基底，亲油层，红外线敏感/可消融层和亲水层。亲水层衍生自硅酸盐溶液，任选地含有颗粒材料如氧化铝和/或二氧化钛。印刷构件可能暴露于来自消融红外线敏感/可消融层的激光器的辐射，以露出亲油层的面积。暴露的印刷构件可以用于湿式平版印刷。

2. 发明授权

US4344141A Gas-turbine engine control 失效
标题翻译：燃气轮机发动机控制
公开(公告)号：US4344141A
公开(公告)日：1982-08-10
申请号：US162545
申请日：1980-06-24
申请人： Michael S. Yates
发明人： Michael S. Yates
IPC分类号： F02C9/28 , F02C9/08
CPC分类号： F02C9/28 , F05D2270/04
摘要： A control system for an aircraft gas-turbine engine has positive and negative acceleration control units. Each control unit has a memory storing values of the maximum or minimum desired rate of change of fuel flow at different speeds beyond which surge or extinction will occur. The control units produce output signals, in accordance with the engine speed and acceleration, for controlling fuel flow so that it follows closely within the surge or extinction curves. The system also has amplitude gates that pass one or the other of these output signals to the engine if the speed of engine demanded by the pilot is such as to cause surge or extinction.
摘要翻译：用于飞机燃气涡轮发动机的控制系统具有正和负加速度控制单元。每个控制单元具有存储在不同速度下燃料流量的最大或最小期望变化率的值的存储器，超过该速度将发生浪涌或消光。控制单元根据发动机转速和加速度产生输出信号，用于控制燃油流量，使其紧密地在喘振或消光曲线内。如果飞行员要求的发动机的速度是引起浪涌或熄灭，该系统还具有将这些输出信号中的一个或另一个传递给发动机的振幅门。

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