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1. 发明授权

US4267030A Apparatus for checking gas analysis devices 失效
标题翻译：用于检查气体分析装置的装置
公开(公告)号：US4267030A
公开(公告)日：1981-05-12
申请号：US970100
申请日：1978-12-15
申请人： Wolfram Breuer , Wolf-Jurgen Becker , Jacques Deprez , Eckard Drope , Karl-Heinz Kaufmann , Kurt Schreckling
发明人： Wolfram Breuer , Wolf-Jurgen Becker , Jacques Deprez , Eckard Drope , Karl-Heinz Kaufmann , Kurt Schreckling
IPC分类号： G01N27/04 , G01N1/00 , G01N27/26 , G01N33/00 , C25B1/00 , C25B1/26 , C25C1/22
CPC分类号： G01N33/0006
摘要： An apparatus for checking gas analysis devices in respect of their sensitivity and their response and regeneration behaviour with respect to time, wherein a reproducible quantity of the measurement component is produced at a predetermined production rate, for a period of time which is guided entirely or at a constant proportion as a concentration pulse to the measurement element of the gas analysis device. For the production of the measurement component a chemical or electro-chemical reaction or even a thermal reaction is used. The time interval can then be conveniently controlled. A decisive advantage with toxic measurement components is that the gas production takes place in all cases for only a short time during the test procedure.
摘要翻译：一种用于检查气体分析装置的灵敏度及其相对于时间的响应和再生行为的装置，其中以预定的生产速率产生测量部件的可重复量，该时间段完全或在作为气体分析装置的测量元件的浓度脉冲的恒定比例。对于测量部件的生产，使用化学或电化学反应或甚至使用热反应。然后可以方便地控制时间间隔。具有有毒测量组件的决定性优点是，在所有情况下，在测试过程中仅在短时间内进行天然气生产。

2. 发明授权

US4151739A Method for checking gas analysis devices 失效
标题翻译：检查气体分析装置的方法
公开(公告)号：US4151739A
公开(公告)日：1979-05-01
申请号：US791125
申请日：1977-04-25
申请人： Wolfram Breuer , Wolf-Jurgen Becker , Jacques Deprez , Eckard Drope , Karl-Heinz Kaufmann , Kurt Schreckling
发明人： Wolfram Breuer , Wolf-Jurgen Becker , Jacques Deprez , Eckard Drope , Karl-Heinz Kaufmann , Kurt Schreckling
IPC分类号： G01N27/04 , G01N1/00 , G01N27/26 , G01N33/00 , G01N7/00 , G01N27/46
CPC分类号： G01N33/0006
摘要： A method for checking gas analysis devices in respect of their sensitivity and their response and regeneration behaviour with respect to time, wherein a reproducible quantity of the measurement component is produced at a predetermined production rate, for a period of time which is guided entirely or at a constant proportion as a concentration pulse to the measurement element of the gas analysis device. For the production of the measurement component a chemical or electro-chemical reaction or even a thermal reaction is used. The time interval can then be conveniently controlled. A decisive advantage with toxic measurement components is that the gas production takes place in all cases for only a short time during the test procedure.
摘要翻译：一种用于检查气体分析装置的灵敏度及其相对于时间的响应和再生行为的方法，其中以预定的生产速率产生测量部件的可重复量，该时间段完全或在作为气体分析装置的测量元件的浓度脉冲的恒定比例。对于测量部件的生产，使用化学或电化学反应或甚至使用热反应。然后可以方便地控制时间间隔。具有有毒测量组件的决定性优点是，在所有情况下，在测试过程中仅在短时间内进行天然气生产。

3. 发明授权

US4023929A Process for determining traces of mercury in liquids 失效
标题翻译：测定液体中汞痕量的方法
公开(公告)号：US4023929A
公开(公告)日：1977-05-17
申请号：US608311
申请日：1975-08-27
申请人： Wolf-Jurgen Becker , Kurt Schreckling
发明人： Wolf-Jurgen Becker , Kurt Schreckling
IPC分类号： G01N31/00 , G01N33/00 , G01N33/18 , G01N31/12 , G01N31/06
CPC分类号： G01N31/005 , G01N33/1813 , G01N33/0045 , Y10T436/255
摘要： In a process for determining the total mercury content in samples of effluent water, the sample is collected on a sample collector where it is evaporated at 1000.degree. C before it is decomposed in a pyrolysis zone at 1000.degree. to 1200.degree. C. The mercury in the liquid sample is thereby expelled as vapor and together with carrier gas it is conducted over a metal sheet which absorbs the mercury and concentrates it. The concentrated mercury is then expelled by heating the metal and transferred by the carrier gas into a mercury absorption photometer where it is determined quantitatively.
摘要翻译：在确定出水水样中总汞含量的过程中，将样品收集在样品收集器上，在1000℃蒸发，然后在1000〜1200℃的热解区分解。液体样品因此被排出蒸气并与载气一起在吸收汞并将其浓缩的金属片上进行。然后通过加热金属并将载气转移到汞吸收光度计中来定量浓缩的汞，其中定量地确定浓汞。

4. 发明授权

US5528903A Small gas turbine 失效
标题翻译：小型燃气轮机
公开(公告)号：US5528903A
公开(公告)日：1996-06-25
申请号：US307717
申请日：1994-09-20
申请人： Kurt Schreckling
发明人： Kurt Schreckling
IPC分类号： A63H27/26 , F01B17/02 , F02C3/08 , F02C6/20 , F23R3/06 , F23R3/32 , F23R3/50 , F23R3/60 , F02C7/224
CPC分类号： F23R3/32 , A63H27/06 , F01B17/02 , F02C3/08 , F02C6/20 , F23R3/06 , F23R3/50 , F23R3/60 , Y02T50/675
摘要： A small gas turbine, in particular for powering airplane models, provided with a casing (3), a compressor rotor (1, 2), a combustion chamber (15-17) and a turbine rotor (5), the turbine rotor (5) driving the compressor rotor(1, 2) by a shaft positioned in a shaft tunnel extending through the combustion chamber (15-17) and surrounded by a helical fuel feed and vaporizing tube (22, 23), the combustion chamber (15-17) being defined by a cylindrical outer wall (15) and a frusto-conical inner wall (16) provided with combustion air intake orifices (19-21)the outlet side of the inner wall (16) of the combustion chamber extending into a cylindrical flow element (6, 7) forming an annular gap therewith, which in turn extends into the center opening of the turbine side guide vane ring (4) and is supported by the end (9) of the shaft tunnel (8), and the other end of the shaft tunnel (8) being secured to the casing (3) between the compressor rotor (1, 2) and the front wall (17) of the combustion chamber.
摘要翻译： PCT No.PCT / EP93 / 00684第 371日期1994年9月20日 102（e）1994年9月20日PCT 1993年3月22日PCT公布。第WO93 / 18832号公报日期：1993年9月30日。一种小型燃气轮机，特别是为飞机型号供电，设有壳体（3），压缩机转子（1,2），燃烧室（15-17）和涡轮转子），涡轮转子（5）通过位于延伸穿过燃烧室（15-17）的轴通道中的轴驱动压缩机转子（1,2），并被螺旋燃料供给和蒸发管（22,23）包围，，所述燃烧室（15-17）由圆柱形外壁（15）和截头圆锥形内壁（16）限定，所述圆锥形内壁（16）设置有所述内壁（16）的出口侧的燃烧空气进气口（19-21）所述燃烧室延伸到与其形成环形间隙的圆柱形流动元件（6,7）中，所述圆柱形流动元件又延伸到所述涡轮机侧导叶环（4）的中心开口中并由所述涡轮机侧导叶环（4）的端部（9）支撑，轴通道（8），轴通道（8）的另一端固定在压缩机转子（1,2）和前壁（17）之间的壳体（3）上 f燃烧室。

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