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1. 发明申请

WO2019025771A1 METHOD AND APPARATUS FOR BACTERIAL ANALYSIS 审中-公开
公开(公告)号：WO2019025771A1
公开(公告)日：2019-02-07
申请号：PCT/GB2018/052154
申请日：2018-07-30
申请人： THE UNIVERSITY OF BRISTOL
发明人： ANTOGNOZZI, Massimo , BERMINGHAM, Charlotte , BALRAM, Krishna Coimbatore , OULTON, Ruth
IPC分类号： G01N21/552 , G01N33/543 , G01N33/569 , G01N21/47 , G01N21/55
摘要： An apparatus (10) comprising: a light source (12); to cast light toward a substrate (20) defining a bacteria binding volume to create an evanescent field (22), the bacteria binding volume being within the evanescent field; a detector (32, 34) arranged to receive light from the bacteria binding volume and output data (36, 37); and a processor (38) arranged to determine vibration of bacteria (26) within the bacteria binding volume in three-dimensions from the data.

2. 发明申请

WO2016009174A1 WIRELESS SENSOR 审中-公开
标题翻译：无线传感器
公开(公告)号：WO2016009174A1
公开(公告)日：2016-01-21
申请号：PCT/GB2015/051912
申请日：2015-06-30
申请人： THE UNIVERSITY OF BRISTOL
发明人： ZHONG, ChengHuan , CROXFORD, Anthony , WILCOX, Paul
IPC分类号： G01N29/24
CPC分类号： H02J50/10 , G01D11/30 , G01N29/2475 , G01N29/2481 , H01F27/2804 , H01F27/2823 , H01F27/2885 , H01F38/14 , H02J50/90
摘要： This application relates to a wireless sensor (10) suitable for non-destructive testing of a test object. The sensor comprises a transducer (12) and an electrically conductive transducer coil (16) configured to define an enclosure and being electrically coupled to the transducer to enable the transducer to be inductively operated by a remote device. The enclosure defined by the transducer coil has an internal width dimension that is wider than a corresponding width dimension of the transducer.
摘要翻译：本申请涉及适用于测试对象的非破坏性测试的无线传感器（10）。传感器包括换能器（12）和导电换能器线圈（16），其被配置为限定外壳并且电耦合到换能器，以使得换能器能够被远程设备感应地操作。由换能器线圈限定的外壳具有比换能器对应的宽度尺寸更宽的内部宽度尺寸。

3. 发明申请

WO2015036730A1 AIRCRAFT LANDING GEAR ASSEMBLY WITH A GROUND LOCK 审中-公开
标题翻译：飞机接地齿轮总成与地面锁
公开(公告)号：WO2015036730A1
公开(公告)日：2015-03-19
申请号：PCT/GB2014/052624
申请日：2014-08-29
申请人： MESSIER-DOWTY LIMITED
发明人： BENNETT, Ian Robert
IPC分类号： B64C25/26 , B64C25/20
CPC分类号： B64C25/26 , B64C25/20 , F16H25/18
摘要： A mechanical lock (10) for a vehicle assembly such as an aircraft landing gear assembly. The lock is either pivotally mounted and substantially mass balanced, or part of an aircraft landing gear assembly (30) and arranged to be mechanically operated from the ground by a mechanical actuation device.
摘要翻译：一种用于诸如飞机起落架组件的车辆组件的机械锁（10）。锁可枢转地安装并且基本上均匀地平衡，或者是飞机起落架组件（30）的一部分并被布置成通过机械致动装置从地面机械地操作。

4. 发明申请

WO2012136978A1 AN AIRCRAFT LANDING GEAR 审中-公开
标题翻译：飞机起落架
公开(公告)号：WO2012136978A1
公开(公告)日：2012-10-11
申请号：PCT/GB2012/050622
申请日：2012-03-22
申请人： MESSIER-DOWTY LIMITED , LACY, Stuart , CUMNER, Geoff
发明人： LACY, Stuart , CUMNER, Geoff
IPC分类号： B64C25/00
CPC分类号： B64C25/001 , B64C2025/003
摘要： An aircraft landing gear (10) comprising a noise-inducing component region (12) and an airflow disruption element (16) having a first configuration in which it is spaced from, and arranged in an upstream relationship with respect to, the noise-inducing component region such that, in use with the landing gear deployed, the airflow disruption element faces, and at least partially disrupts, an airflow(A) moving towards the noise-inducing component region, wherein the cross-sectional area of the airflow disruption element is less than the cross-sectional area of the noise-inducing component region.
摘要翻译：一种飞机起落架（10），包括噪声诱导组件区域（12）和气流破坏元件（16），其具有第一配置，其中它与噪声诱导分配区域，使得在使用起落架部署时，气流破坏元件面向并且至少部分地中断朝向噪声诱导部件区域移动的气流（A），其中气流破坏元件的横截面积小于噪声诱导分量区域的横截面面积。

5. 发明申请

WO2012069806A1 MECHANICAL POSITION INDICATOR FOR UN AIRCRAFT LANDING GEAR 审中-公开
标题翻译：联合国飞机起落架机械位置指示器
公开(公告)号：WO2012069806A1
公开(公告)日：2012-05-31
申请号：PCT/GB2011/052182
申请日：2011-11-09
申请人： MESSIER-DOWTY LIMITED , HODGKINSON, Ben , LACY, Stuart , WEBB, Chris , ANSON, Garry
发明人： HODGKINSON, Ben , LACY, Stuart , WEBB, Chris , ANSON, Garry
IPC分类号： B64D45/00 , B64C25/00
CPC分类号： B64D45/0005 , B64C25/00 , B64D2045/008
摘要： A mechanical position indicator (9a) for providing a visual indication that a first part of an aircraft landing gear (1) has assumed a predetermined position relative to a second part, the position indicator (9a) being arranged to be coupled to a first one of the first and second parts and in a first state arranged to hold an indicator element (15a) in a deployed position, the position indicator (9a) being arranged such that upon the first part assuming the predetermined position relative to the second part, a second one of the first and second parts changes the position indicator (9a) from the first state to a second state in which the indicator element (15a) is displaced from the deployed position, the position indicator (9a) being arranged to inhibit the indicator element (15a) thereafter returning to the deployed position.
摘要翻译：一种用于提供飞行器起落架（1）的第一部分相对于第二部分已经具有预定位置的视觉指示的机械位置指示器（9a），所述位置指示器（9a）被布置成联接到第一部分的第一和第二部分，并且在布置成将展示元件（15a）保持在展开位置的第一状态下，位置指示器（9a）被布置成使得在第一部分相对于第二部分呈现预定位置时，第一和第二部分中的第二部分将位置指示器（9a）从第一状态改变到指示元件（15a）从展开位置移位的第二状态，位置指示器（9a）布置成禁止指示器元件（15a）此后返回到展开位置。

6. 发明申请

WO2021111188A1 GAS FILTRATION APPARATUS 审中-公开
公开(公告)号：WO2021111188A1
公开(公告)日：2021-06-10
申请号：PCT/IB2020/001018
申请日：2020-12-02
申请人： PORVAIR FILTRATION GROUP LIMITED
发明人： GINGERICH, Nathan, D. , NUNES, Paul , YOUNG, Jerry, A.
IPC分类号： B01D46/00 , B01D46/12 , B01D46/24
摘要： A filtration element assembly for use with a cylindrical filter casing has a prismatic support body with a support body interior space. The side walls of the support body form a polygonal outer cross-sectional shape defining a circumscribed circle with a diameter less than or equal to the casing diameter. At least one side wall has an inlet flow passage with a receiving channel surrounding it. A porous filtration structure is disposed within the receiving channel so as to cover the inlet flow passage. A clamping member attached to each of the at least one side wall has a framing portion and a flange portion. The framing portion has a flow window formed there-through in registration with the inlet flow passage. The flange portion extends from the framing portion and is sized and configured for reception into the receiving channel to engage and retain the filtration element within the channel.

7. 发明申请

WO2019053436A1 SPATIO-TEMPORAL SUB-SAMPLING OF DIGITAL VIDEO SIGNALS 审中-公开
公开(公告)号：WO2019053436A1
公开(公告)日：2019-03-21
申请号：PCT/GB2018/052604
申请日：2018-09-13
申请人： THE UNIVERSITY OF BRISTOL
发明人： ZHANG, Fan , AFONSO, Mariana , BULL, David
IPC分类号： H04N19/587 , H04N19/59 , H04N19/132 , H04N19/154 , H04N19/177 , H04N19/179
CPC分类号： H04N19/587 , H04N19/132 , H04N19/154 , H04N19/177 , H04N19/179 , H04N19/59
摘要： A computer implemented video processing method comprising content-adaptive spatiotemporal down-sampling based on a measure of quality degradation due to down-sampling.

8. 发明申请

WO2014181084A1 METHOD AND APPARATUS FOR PRODUCING AN ACOUSTIC FIELD 审中-公开
标题翻译：用于产生声学场的方法和装置
公开(公告)号：WO2014181084A1
公开(公告)日：2014-11-13
申请号：PCT/GB2014/051319
申请日：2014-04-29
申请人： THE UNIVERSITY OF BRISTOL
发明人： CARTER, Thomas Andrew , LONG, Benjamin John Oliver , SUBRAMANIAN, Sriram
IPC分类号： H04S7/00
CPC分类号： G01S7/52004 , G01S7/52003 , G01S7/539 , G01S15/36 , G01S15/876 , G01S2007/52007 , H04S7/30
摘要： A plurality of control points (10) are defined which each have a known spatial relationship relative to an array of transducers. An amplitude is assigned to each control point (12). A matrix (16) is produced containing elements which represent, for each of the control points, the effect that producing a modeled acoustic field having the assigned amplitude with a particular phase at the control point has on the consequential amplitude and phase of the modeled acoustic field at the other control points (14). Eigenvectors of the matrix (18) are determined, each eigenvector representing a set of phases and relative amplitudes of the modeled acoustic field at the control points. One of the sets (20) is selected and the transducer array is operated to cause one or more of the transducers to output an acoustic wave each having an initial amplitude and phase such that the phases and amplitudes of the resultant acoustic field at the control points correspond to the phases and relative amplitudes of the selected set (22, 24).
摘要翻译：定义了多个控制点（10），每个控制点相对于换能器阵列具有已知的空间关系。向每个控制点（12）分配一个振幅。产生一个矩阵（16），其中包含元素，对于每个控制点，表示在控制点处产生具有特定相位的具有分配幅度的建模声场的效果在建模声学的相应振幅和相位上在其他控制点（14）处。确定矩阵（18）的特征向量，每个特征向量表示控制点处的建模声场的一组相位和相对幅度。选择组（20）中的一个，并且操作换能器阵列以使一个或多个换能器输出每个具有初始振幅和相位的声波，使得在控制点处的所得声场的相位和振幅对应于所选择的组（22,24）的相位和相对幅度。

9. 发明申请

WO2014174302A1 ACTUATOR 审中-公开
标题翻译：执行器
公开(公告)号：WO2014174302A1
公开(公告)日：2014-10-30
申请号：PCT/GB2014/051282
申请日：2014-04-24
申请人： MESSIER-DOWTY LIMITED
发明人： GREEN, Christopher , SCHMIDT, Robert Kyle , SMART, David
IPC分类号： B64C25/60 , F16F9/48
CPC分类号： F15B15/1457 , B64C25/60 , F15B11/123 , F15B15/1409 , F15B15/1438 , F16F9/063 , F16F9/486
摘要： An actuator (10) arranged to be movable between an extended condition and a compressed condition and being biased to an intermediate condition between and distinct from the extended condition and the compressed condition. The actuator includes a damping device (40) arranged to define the damping coefficient of the actuator. The damping device is arranged to provide a relatively low damping coefficient when the actuator is in a first condition distinct from the intermediate condition, and a relatively high damping coefficient when the actuator is in a second condition, the second condition being distinct from the first condition and being equal or adjacent to the intermediate condition.
摘要翻译：致动器（10）被布置成能够在伸展状态和压缩状态之间移动并且被偏压到延伸状态和压缩状态之间的中间状态。致动器包括布置成限定致动器的阻尼系数的阻尼装置（40）。阻尼装置被布置成当致动器处于不同于中间状态的第一状态时提供相对较低的阻尼系数，以及当致动器处于第二状态时相对较高的阻尼系数，第二条件不同于第一条件并且与中间条件相等或相邻。

10. 发明申请

WO2014170636A1 DYNAMIC PLAIN BEARING 审中-公开
标题翻译：动态普通轴承
公开(公告)号：WO2014170636A1
公开(公告)日：2014-10-23
申请号：PCT/GB2014/051041
申请日：2014-04-03
申请人： MESSIER-DOWTY LIMITED
发明人： BENNETT, Ian Robert
IPC分类号： F16C33/10 , F16C33/12 , F16C17/02
CPC分类号： F16C33/125 , B64C25/001 , F16C17/02 , F16C33/102 , F16C33/1065 , F16C33/1095 , F16C33/121 , F16C2204/12 , F16C2326/43
摘要： A dynamic bearing (10) for an aircraft landing gear. The bearing comprises a lug (12); a shaft (16) comprising a first material; and a bearing surface (14) comprising a second material that is softer than the first material. The bearing surface defines a bore and is arranged to support the shaft when the shaft is movably housed within the bore in use. The bearing surface is defined by the lug or a coating applied to the lug.
摘要翻译：飞机起落架的动态轴承（10）。所述轴承包括凸耳（12）; 包括第一材料的轴（16）; 和包括比第一材料软的第二材料的支承表面（14）。轴承表面限定了孔，并且当轴可移动地容纳在使用中的孔内时被布置成支撑轴。轴承表面由凸耳或施加到凸耳的涂层限定。

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