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公开(公告)号：US20150345854A1
公开(公告)日：2015-12-03
申请号：US14705335
申请日：2015-05-06
发明人： Stefan BRENDELBERGER , Jan FELINKS
IPC分类号： F25D5/00
CPC分类号： F25D5/00 , B01J8/087 , B01J2208/00451 , C01B3/063 , C01B3/105 , F24S80/20 , F24S90/00 , F28D20/003 , Y02E10/40 , Y02E60/142 , Y02E60/36 , Y02E70/30
摘要： The present invention relates to a process for performing a chemical reaction consisting of at least two sequential reversible steps characterized by being performed in a cycle, and to a reactor for performing such process.
摘要翻译： 本发明涉及一种用于进行化学反应的方法，所述化学反应由至少两个顺序可逆步骤组成，其特征在于在循环中进行，并且涉及用于进行该方法的反应器。
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公开(公告)号：US20140312174A1
公开(公告)日：2014-10-23
申请号：US14252173
申请日：2014-04-14
发明人： Frank Theurich , Jan Himisch
IPC分类号： B64C23/06
CPC分类号： B64C23/069 , Y02T50/164
摘要： A wing for of aircraft has a wing tip shape that has a profile that extends in the direction of the span of the wing, and across the direction of the span of the wing extends from the wing leading edge to the wing trailing edge. The profile is delimited by a first skin and a second skin, with a winglet, arranged on the wing end. The winglet is substantially planar, and has a transition region arranged between the wing and the winglet, that extends from a connection on the wing to a connection on the winglet. The curvature of the local dihedral can increase in the transition region from a low level or a level of zero at or near the wing intersection in the outboard direction.
摘要翻译： 用于飞行器的机翼具有翼尖形状，其具有沿翼的跨度方向延伸的轮廓，并且跨越翼的跨度的方向从机翼前缘延伸到翼后缘。 轮廓由第一皮肤和第二皮肤划分，具有布置在翼端上的小翼。 小翼基本上是平面的，并且具有布置在翼和小翼之间的过渡区域，其从机翼上的连接延伸到小翼上的连接。 局部二面体的曲率可以在过渡区域从外侧方向上的翼交点处或附近的低水平或零水平增加。
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公开(公告)号：US20240344740A1
公开(公告)日：2024-10-17
申请号：US18701087
申请日：2022-10-21
发明人： Freerk KLASING , Veronika SÖTZ
摘要： The invention relates to a method for thermally stabilizing molten nitrate salt in thermal power plants, in particular solar power plants, having the steps of: a) providing molten nitrate salt, said nitrate salt being selected from alkali metal nitrates, alkaline earth metal nitrates, and mixtures of one or more alkali metal nitrates and alkaline earth metal nitrates, and transporting the molten nitrate salt in lines provided for this purpose and b) introducing a heat quantity ΔQpat into the molten salt at a defined position, wherein the heat quantity is provided in particular by means of solar energy. The invention is characterized in that prior to or after step b), a stabilization gas is supplied to the molten nitrate salt, said stabilization gas having oxygen, at least one nitric gas, and optionally nitrogen. The invention also relates to a device for carrying out the method.
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公开(公告)号：US12117247B2
公开(公告)日：2024-10-15
申请号：US17910009
申请日：2021-03-10
发明人： Werner Kraft , Peter Vetter , Veronika Stahl
CPC分类号： F28D20/021
摘要： A heat accumulator device is provided having a metal phase-change material as an accumulator material, the heat accumulator device including at least one a holding chamber having a holding space for the accumulator material, a housing for the holding space, at least one heat input apparatus for inputting heat into the at least one holding chamber, and at least one heat output apparatus for outputting heat from the at least one holding chamber. A coupling region of the heat input apparatus, provided for thermal coupling to the accumulator material, and/or a coupling region of the heat output apparatus, provided for thermal coupling to the accumulator material, is arranged, at least in part, at a distance from the accumulator material.
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公开(公告)号：US20240261964A1
公开(公告)日：2024-08-08
申请号：US18008760
申请日：2021-06-10
IPC分类号： B25J9/16
CPC分类号： B25J9/1643 , B25J9/1607
摘要： A method for controlling a kinematically redundant robot (100) in order to fulfill multiple tasks. At least one passivity-based first controller module (102) is used, at least one task target description and at least one associated task mapping are computed for the at least one first controller module (102), at least one weighting is computed for the tasks, and the at least one first controller module (102) is integrated into an overall controller (104), using the at least one weighting. Moreover, the invention relates to a computer program product that includes commands which, when the program is executed with the aid of at least one processor, prompt the processor to carry out such a method.
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公开(公告)号：US20240085528A1
公开(公告)日：2024-03-14
申请号：US18272395
申请日：2021-12-21
CPC分类号： G01S7/4811 , G01S7/4818 , G01S17/34 , G01S17/50 , G01S17/95
摘要： An optical device and systems for near and distance imaging includes an optical unit with a first optical lens and a second optical lens, the first optical lens and second optical lens being arranged along an optical axis, and a transceiver unit with a transceiver element, a light passage surface of the transceiver element being arranged in or intersecting a plane or curved surface. A first distance between the surface and the first optical lens is provided along the optical axis and set in such a way that, during intended normal operation, the transceiver element of the transceiver unit is imaged onto a distant imaging surface by the optical unit.
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公开(公告)号：USD1009111S1
公开(公告)日：2023-12-26
申请号：US29794123
申请日：2021-06-10
设计人： Roman Weitschat
摘要： FIG. 1 is a front elevation view of a gripper jaw showing my new design;
FIG. 2 is a rear elevation view thereof;
FIG. 3 is a top view thereof;
FIG. 4 is a bottom view thereof;
FIG. 5 is a right side elevation view thereof;
FIG. 6 is a left side elevation view thereof;
FIG. 7 is a front, bottom, left side perspective view thereof;
FIG. 8 is a rear, top, right side perspective view thereof; and,
FIG. 9 is a rear, left side perspective view and a front, right side perspective view showing the gripper jaw in its environment of a robotic device.
The broken line portion of the figure drawing is included to show environment and represents unclaimed subject matter only and forms no part of the claimed design.-
公开(公告)号：US20230396334A1
公开(公告)日：2023-12-07
申请号：US18031963
申请日：2021-10-18
IPC分类号： H04B10/114
CPC分类号： H04B10/1141 , H04B10/1149
摘要： A system for optical communication includes at least one light source for transmitting optical signals, at least one optical receiving unit for receiving the optical signals of the at least one light source, at least one mask unit, which is arranged between the optical receiving unit and the at least one light source, and which is designed to be switchable back-and-forth at least in areas between an at least partially optically non-forwarding and at least partially optically forwarding state. An image of at least one light-emitting area of the at least one light source can be imaged onto the at least one mask unit and in the at least partially forwarding state of the at least one mask unit can be conducted to the receiving unit. A method for optical communication is also provided.
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公开(公告)号：US20230237224A1
公开(公告)日：2023-07-27
申请号：US18002281
申请日：2021-06-23
发明人： Christoph RÄTH , Sebastian BAUR
IPC分类号： G06F30/27
CPC分类号： G06F30/27
摘要： The invention relates to a method for determining a state evolution of a real system with a plurality N of degrees of freedom, comprising the following steps: determining states for each of the plurality N of degrees of freedom up to a time t0, wherein the determining of states for each of the plurality N of degrees of freedom is carried out by measuring corresponding state variables of the real system; selecting a degree of freedom f from the plurality N of degrees of freedom; determining a measure of similarity between the selected degree of freedom f and each other degree of freedom of the plurality N of degrees of freedom of the real system for the determined states; determining a selection M of degrees of freedom from the plurality N of degrees of freedom based on the measure of similarity; and determining the state evolution of measured states for the selected degree of freedom f based on the selection M of degrees of freedom.
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公开(公告)号：US20230227144A1
公开(公告)日：2023-07-20
申请号：US18125535
申请日：2023-03-23
发明人： Frank Theurich , Jan Himisch
摘要： An aircraft includes a fuselage, a wing attached thereto, a wing tip device attached to a wing end of the wing (2), a wing-like element having a wing root, a wing leading edge and a wing trailing edge, and a torque control device having a rotatable interface means. The torque control device is adapted for rotatably supporting the wing root of the wing-like element on the interface means about a rotational axis extending from the interface means into the wing-like element and to limit the degree of rotation depending on a torque introduced into the interface means by the wing-like element. The wing-like element is adapted to induce a rotation around the rotational axis in an air flow. The wing root is coupled with the wing tip device, the wing or the fuselage through the torque control device such that the leading edge extends into an airflow surrounding the aircraft.
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