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1.发明申请VACUUM TOILET SYSTEM FOR WASTE WATER TRANSPORT AND WASTE WATER COLLECTION IN AN AIRCRAFT 审中-公开真空吸尘器系统，用于运输中的废水运输和废水收集公开(公告)号：US20100116935A1
公开(公告)日：2010-05-13
申请号：US12595849
申请日：2008-04-17
Applicant: Ulrich Rieger , Claus Hoffjann
Inventor： Ulrich Rieger , Claus Hoffjann
Abstract: The invention relates to a vacuum toilet system for transporting toilet waste water and for collecting the waste water in an aircraft. The vacuum toilet system comprises a waste water transport tank and a waste water collection tank that is always subjected to a cabin pressure. In this case, the vacuum toilet system is designed in such a way that the transport of the waste water through the waste water transport tank takes place in combination with a pressure difference between the toilet and an outboard ventilation. The waste water is collected in a waste water collection tank. In this case, the waste water collection tank may be realized in the form of a conform, unpressurized waste water collection tank.
Abstract translation: 本发明涉及一种用于运输马桶废水并用于收集飞机中的废水的真空马桶系统。 真空马桶系统包括总是受到舱室压力的废水输送箱和废水收集箱。 在这种情况下，真空马桶系统被设计成使得废水通过废水输送箱的运输与马桶和舷外通风之间的压差结合进行。 废水被收集在废水收集罐中。 在这种情况下，废水收集罐可以以符合，非加压的废水收集罐的形式实现。
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公开(公告)号：US06571762B2
公开(公告)日：2003-06-03
申请号：US10176937
申请日：2002-06-21
Applicant: Ulrich Rieger
Inventor： Ulrich Rieger
IPC: F02F142
Abstract: A cylinder head of an internal combustion engine includes at least one exhaust port, which is formed by a port liner of at least two layers cast into the cylinder head, provided with a heat-insulating layer and having a sheet metal port, the sheet metal port being surrounded by a helically wound sheet metal strip.
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公开(公告)号：US20100221642A1
公开(公告)日：2010-09-02
申请号：US12680023
申请日：2008-09-24
Applicant: Lars Frahm , Ulrich Rieger , Claus Hoffjann , Hansgeorg Schuldzig
Inventor： Lars Frahm , Ulrich Rieger , Claus Hoffjann , Hansgeorg Schuldzig
CPC classification number: B64D11/02 , B64D41/00 , B64D2041/005 , H01M8/04029 , H01M8/04126 , H01M8/04164 , H01M8/0662 , H01M2250/20 , Y02T50/44 , Y02T50/46 , Y02T90/32 , Y02T90/36
Abstract: A fuel cell system for an aircraft is stated, which fuel cell system comprises a fuel cell unit and a suction module. The suction module is used to draw oxygen through the fuel cell unit. No vacuum generators are used during cruising flight.
Abstract translation: 说明了一种用于飞行器的燃料电池系统，该燃料电池系统包括燃料电池单元和抽吸模块。 抽吸模块用于通过燃料电池单元吸入氧气。 巡航期间不使用真空发生器。
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公开(公告)号：US20050150477A1
公开(公告)日：2005-07-14
申请号：US11032302
申请日：2005-01-10
Applicant: Ulrich Rieger , Manfred Riester
Inventor： Ulrich Rieger , Manfred Riester
CPC classification number: F01N13/10 , F01N2450/24 , F02F1/24 , F02F11/002 , F02F2007/0041
Abstract: In a cylinder head of an internal combustion engine having an exhaust passage, a lower cylinder head part, an upper cylinder head part, and a bolt-on surface on the exhaust side with an exhaust manifold bolted thereto, a sealing surface is arranged in a recess extending along the exhaust passage into the cylinder head and the manifold has a tube which extends into the recess in sealing engagement with the sealing surface at the bottom of the recess and which is spaced from the surrounding wall of the cylinder head recess, through which the manifold tube extends in a curved fashion.
Abstract translation: 在具有排气通道，下气缸盖部分，上气缸头部分和排气侧的螺栓接合表面的内燃机的气缸盖中，具有螺栓连接到其上的排气歧管，密封表面设置在 凹槽沿着排气通道延伸到气缸盖中，并且歧管具有延伸到凹部中的密封件与密封表面密封接合的管，该密封表面在凹部的底部处，并且与气缸盖凹部的周围壁间隔开， 歧管以弯曲的方式延伸。
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公开(公告)号：US20050092282A1
公开(公告)日：2005-05-05
申请号：US10994736
申请日：2004-11-22
Applicant: Ulrich Rieger
Inventor： Ulrich Rieger
CPC classification number: F02F7/0043 , F02F7/0007
Abstract: In a cylinder-block for an internal combustion engine with a plurality of cylinders having longitudinal profiled sections in the form of lateral hollow reinforcement structures and vertical sections in the form of profiled reinforcement structures, in the region of a main bearing plane means are provided for supporting a lateral camshaft beneath the upper longitudinal profiled section, and, in the region of the bearing structure for the camshaft the vertical profiled section is divided in two.
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Patent Agency Ranking
公开(公告)号：US5703321A
公开(公告)日：1997-12-30
申请号：US546809
申请日：1995-10-23
Applicant: Johannes Feierlein , Ulrich Rieger
Inventor： Johannes Feierlein , Ulrich Rieger
Abstract: A device for locating artillery and sniper fire with a sensor and acoustically triggered marking means. An igniter is provided with the acoustic sensor and is adjustable in terms of frequency and/or pulse pattern. A remover preventer is provided and the components are provided in a shell-proof housing whereby removal triggers the marking means.
Abstract translation: 用传感器和声学触发标记装置定位火炮和狙击手的装置。 点火器设置有声学传感器，并且在频率和/或脉冲图案方面是可调节的。 提供了一种去除剂防护器，并且这些部件设置在防外壳中，由此移除触发标记装置。
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公开(公告)号：US5301614A
公开(公告)日：1994-04-12
申请号：US953266
申请日：1992-09-30
Applicant: Ulrich Rieger
Inventor： Ulrich Rieger
CPC classification number: F42C11/002 , F41G3/22 , F42B12/10
Abstract: Submunition is transported by a carrier to a target area and launched there, whereupon it covers a preset distance at a constant altitude at an angle to the flight axis of the carrier. The submunition has a target sensor and a payload, and is equipped with an altimeter as well as a circuit to evaluate the altimeter readings, and with at least one altitude/roll rudder controllable by this circuit.
Abstract translation: 子弹药由载体运输到目标区域并在那里发射，因此它以与载体飞行轴成一定角度的恒定高度覆盖预设距离。 子弹药具有目标传感器和有效载荷，并且配备有高度计以及用于评估高度计读数的电路，以及至少一个由该电路可控的高度/舵方向舵。
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公开(公告)号：US5206453A
公开(公告)日：1993-04-27
申请号：US766192
申请日：1991-09-27
Applicant: Ulrich Rieger
Inventor： Ulrich Rieger
IPC: F42B12/60
CPC classification number: F42B12/60
Abstract: An injection module for a subammunition container, of the type in which subammunitions, ejected transversely to the flight direction of the subammunition container, are situated in front of driving devices which are actuated by gas-generator-driven ejecting pistons. The ejecting pistons are arranged transversely with respect to the flight direction, and may extend along half the width or the full width of the ejecting module. The gas generator may be arranged transversely or longitudinally of the flight direction.
Abstract translation: 用于子弹药容器的注射模块，其中横向于子弹药容器的飞行方向弹出的子弹位于由气体发生器驱动的喷射活塞致动的驱动装置的前面。 喷射活塞相对于飞行方向横向地布置，并且可以沿喷射模块的宽度或全宽度的一半延伸。 气体发生器可以布置在飞行方向的横向或纵向上。
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9.发明申请Arrangement for handling the fuel supply in a common rail fuel injection system 失效用于处理共轨燃料喷射系统中的燃料供应的布置公开(公告)号：US20050150480A1
公开(公告)日：2005-07-14
申请号：US11035759
申请日：2005-01-14
Applicant: Michael Hoffmann , Magnus Korte , Ulrich Rieger
Inventor： Michael Hoffmann , Magnus Korte , Ulrich Rieger
CPC classification number: F02M37/22 , F01P2060/10 , F02M31/20 , F02M37/0052 , F02M37/20 , F02M53/00 , F02M63/0225 , Y02T10/126
Abstract: In an arrangement for handling the fuel in a common rail fuel injection system of an internal combustion engine, wherein fuel is supplied from a tank via a fuel delivery line including a first fuel filter, a low-pressure pump arranged upstream from the first fuel filter and a high pressure pump arranged downstream of the first fuel filter to a high pressure fuel rail from which the fuel is distributed to the cylinder of the engine, a bypass line extends from the high pressure fuel rail to the fuel delivery line and includes a second fuel filter and a heat exchanger which is operatively connected to a cooling circuit of an air conditioning system or to a cooling circuit of the internal combustion engine.
Abstract translation: 在用于处理内燃机的共轨燃料喷射系统中的燃料的装置中，其中通过包括第一燃料过滤器的燃料输送管线从燃料箱供给燃料，布置在第一燃料过滤器上游的低压泵 以及高压泵，其布置在所述第一燃料过滤器的下游到由所述燃料分配到所述发动机的气缸的高压燃料轨道，旁路管线从所述高压燃料轨延伸到所述燃料输送管线，并且包括第二 燃料过滤器和可操作地连接到空调系统的冷却回路或内燃机的冷却回路的热交换器。
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公开(公告)号：US5678788A
公开(公告)日：1997-10-21
申请号：US529109
申请日：1995-09-15
Applicant: Walter Hetzer , Ulrich Rieger
Inventor： Walter Hetzer , Ulrich Rieger
CPC classification number: B64D17/025 , B64D17/34
Abstract: A load glider has, between the parachute surface and the load, a device in which a reversible transfer of mechanical energy from the main lines to the steering lines takes place, so that essentially only frictional forces are to be overcome during the operation of the steering lines. The device includes two differential gears, which are arranged in parallel and are accommodated in housings in which a steering line is wound up on a roller with a larger diameter and a main line is wound up on the other roller with a small diameter. Gears, which can be driven by pinions driven by electric motors, are flanged onto the larger rollers.
Abstract translation: 负载滑翔机在降落伞表面和负载之间具有其中发生机械能从主线到转向线的可逆传递的装置，使得在转向操作期间基本上仅克服摩擦力 线条。 该装置包括两个平行布置的差速齿轮，并且容纳在壳体中，其中转向线卷绕在具有较大直径的辊上，并且主线以小直径卷绕在另一个辊上。 可由电动机驱动的小齿轮驱动的齿轮，被法兰连接到较大的滚子上。
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