CN112857639B - Servo incremental high-precision pressure sensor and using method thereof - Google Patents
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Abstract
Description
技术领域technical field
本发明涉及一种伺服增量式高精度压力传感器及其使用方法,属于压力传感器技术领域。The invention relates to a servo incremental high-precision pressure sensor and a using method thereof, belonging to the technical field of pressure sensors.
背景技术Background technique
压力传感器广泛用于各行各业,其精度与量程密切相关,通常表示为满量程的系数,高精度的传感器能够达到满量程的万分之二左右。因此,当量程增加时,精度也随之变差,如何在大承载条件下实现高精度成为压力传感器的瓶颈问题。另一方面,质心测试台、卫星模拟器等很多应用中,往往不关心初始加载的大小,而关系相对于初始加载的载荷变化量,即压力增量。Pressure sensors are widely used in all walks of life, and their accuracy is closely related to the range, usually expressed as a coefficient of the full range, and a high-precision sensor can reach about 2/10,000 of the full range. Therefore, when the range increases, the accuracy also deteriorates, and how to achieve high accuracy under large load conditions becomes the bottleneck of the pressure sensor. On the other hand, in many applications such as centroid test benches and satellite simulators, the size of the initial load is often not concerned, but the load change relative to the initial load, that is, the pressure increment.
发明内容SUMMARY OF THE INVENTION
本发明的目的是提出一种伺服增量式高精度压力传感器及其使用方法,以解决现有技术中存在的问题。The purpose of the present invention is to propose a servo incremental high-precision pressure sensor and a method for using the same, so as to solve the problems existing in the prior art.
一种伺服增量式高精度压力传感器,所述伺服增量式高精度压力传感器包括加载台、压力传感器、气囊、微位移驱动器、微位移传感器和基座,所述气囊的下侧安装在所述基座的上表面上,所述气囊的上侧支撑所述加载台,所述微位移驱动器和微位移传感器以所述气囊为中心周向设置在所述基座的上表面上,所述压力传感器与所述微位移驱动器一一对应,且每个压力传感器均由对应的所述微位移驱动器支撑,所述压力传感器的上侧支撑所述加载台。A servo incremental high-precision pressure sensor, the servo incremental high-precision pressure sensor includes a loading table, a pressure sensor, an air bag, a micro-displacement driver, a micro-displacement sensor and a base, and the lower side of the air bag is installed on the On the upper surface of the base, the upper side of the air bag supports the loading table, the micro-displacement driver and the micro-displacement sensor are circumferentially arranged on the upper surface of the base with the air bag as the center, the The pressure sensors are in one-to-one correspondence with the micro-displacement drivers, and each pressure sensor is supported by the corresponding micro-displacement driver, and the loading table is supported on the upper side of the pressure sensors.
进一步的,所述加载台和基座为同轴的圆台。Further, the loading table and the base are coaxial circular tables.
进一步的,所述气囊设置在所述加载台和基座的轴心上。Further, the airbag is arranged on the axis of the loading platform and the base.
进一步的,所述气囊为可调节充气量的气囊。Further, the airbag is an airbag with an adjustable inflation volume.
进一步的,所述微位移驱动器和压力传感器同轴心。Further, the micro-displacement driver and the pressure sensor are coaxial.
进一步的,所述微位移驱动器和微位移传感器均沿所述气囊周向均匀设置有N个,N≥3。Further, N micro-displacement drivers and micro-displacement sensors are evenly arranged along the circumferential direction of the airbag, and N≥3.
进一步的,所述微位移驱动器和微位移传感器同圆交错设置。Further, the micro-displacement driver and the micro-displacement sensor are arranged staggered in the same circle.
进一步的,所述微位移驱动器和微位移传感器同向不同圆设置。Further, the micro-displacement driver and the micro-displacement sensor are arranged in different circles in the same direction.
进一步的,所述基座设置有通用的固定接口。Further, the base is provided with a universal fixing interface.
一种伺服增量式高精度压力传感器的使用方法,基于上述的一种伺服增量式高精度压力传感器,所述使用方法包括以下内容:A method of using a servo incremental high-precision pressure sensor, based on the above-mentioned servo incremental high-precision pressure sensor, the using method includes the following contents:
首先,根据工作点载荷F0调节气囊的压力,使压力传感器的示数位于量程中位,并记录微位移传感器的示数Pi0和压力传感器的示数Fi0,下标i表示压力传感器或微位移传感器的编号,i=1,2,…,N,N表示压力传感器或微位移传感器的总数;下标0表示初始值,然后,在加载台上施加载荷,此时微位移传感器的示数为Pi,如果First, adjust the pressure of the airbag according to the working point load F 0 so that the indication of the pressure sensor is in the middle of the range, and record the indication P i0 of the micro-displacement sensor and the indication F i0 of the pressure sensor, the subscript i represents the pressure sensor or The number of the micro-displacement sensor, i=1,2,...,N, N represents the total number of pressure sensors or micro-displacement sensors; the subscript 0 represents the initial value, and then a load is applied on the loading table, and the display of the micro-displacement sensor is at this time. number is P i , if
且/或and/or
其中,ò和σ分别表示预设的位移精度参数和位移分布参数,μΔP和σΔP分别表示产生载荷增加时,所有微位移传感器位移变化量的均值和方差,Among them, ò and σ represent the preset displacement accuracy parameters and displacement distribution parameters, respectively, μ ΔP and σ ΔP represent the mean and variance of the displacement changes of all micro-displacement sensors when the load increases, respectively,
调节微位移驱动器(4)使μΔP和σΔP减小,直到μΔP<ò且σΔP<σ,读取此时的压力传感器示数Fi,则加载台(1)上相对于工作点载荷F0增加的载荷为:Adjust the micro-displacement driver (4) to reduce μ ΔP and σ ΔP until μ ΔP <ò and σ ΔP <σ, read the pressure sensor reading F i at this time, then the load table (1) is relative to the working point The added load for load F 0 is:
记压力传感器的相对测量精度为r0、量程为G,气囊在工作点的刚度为k时,上述新增载荷的相对测量精度为:When the relative measurement accuracy of the pressure sensor is r 0 , the range is G, and the stiffness of the airbag at the working point is k, the relative measurement accuracy of the above-mentioned newly added load is:
其中,工作点刚度k表示在工作点,载荷发生微小变化时造成位移的变化,载荷变化量与位移变化量的比值;a表示设计的相对工作点,即工作点载荷与压力传感器的总量程之比,Among them, the working point stiffness k represents the displacement change caused by the slight change of the load at the operating point, and the ratio of the load change to the displacement change; a represents the designed relative operating point, that is, the operating point load and the total range of the pressure sensor Ratio,
通过设计选择较小的k和ò使得kò<<NG,选择较大的a使得a>>1,得到By designing smaller k and ò such that kò<<NG, and choosing larger a such that a>>1, we get
即实现了更高的测量精度。That is, higher measurement accuracy is achieved.
本发明的有以下优点:本发明采用气囊作为主支撑,实现对工作点载荷的卸载,并把工作点的位置作为平衡位置,通过微位移传感器监测在施加增量载荷后的位移变化量,并通过微位移驱动器将这一变化量减小到一定范围,通过与微位移驱动器串联的小量程高精度压力传感器测量使增量位移减小到一定范围所施加的增量驱动力,所有压力传感器的合力给出了施加在加载台上的载荷增量。由于采用气囊作为主支撑对工作点载荷进行了卸载,压力传感器只需要测量增量载荷,在增量载荷相对于工作点载荷很小时,可以选择量程很小的压力传感器,从而提高对增量载荷的测量精度。主支撑带来的误差由主支撑的刚度、微位移传感器的测量精度和微位移驱动器的驱动分辨率确定,通过选择高精度的微位移传感器和高分辨率的微位移驱动器,该误差可以很小予以忽略。从而实现了大承载下增量载荷的高精度测量。The present invention has the following advantages: the present invention adopts the airbag as the main support, realizes the unloading of the load at the working point, and uses the position of the working point as the equilibrium position, and monitors the displacement change after the incremental load is applied by the micro-displacement sensor, and This variation is reduced to a certain range through the micro-displacement driver, and the incremental driving force applied to reduce the incremental displacement to a certain range is measured by a small-range high-precision pressure sensor connected in series with the micro-displacement driver. The resultant force gives the incremental load applied to the loading table. Since the air bag is used as the main support to unload the working point load, the pressure sensor only needs to measure the incremental load. When the incremental load is small relative to the working point load, a pressure sensor with a small range can be selected, thereby improving the accuracy of the incremental load. measurement accuracy. The error brought by the main support is determined by the stiffness of the main support, the measurement accuracy of the micro-displacement sensor and the drive resolution of the micro-displacement driver. By choosing a high-precision micro-displacement sensor and a high-resolution micro-displacement driver, the error can be very small. be ignored. Thus, high-precision measurement of incremental loads under large loads is achieved.
附图说明Description of drawings
图1为本发明的一种伺服增量式高精度压力传感器的正视图;1 is a front view of a servo incremental high-precision pressure sensor of the present invention;
图2为图1的侧视图;Fig. 2 is the side view of Fig. 1;
图3为本发明的一种伺服增量式高精度压力传感器的立体示意图;3 is a schematic perspective view of a servo incremental high-precision pressure sensor of the present invention;
图4为本发明的一种伺服增量式高精度压力传感器的使用方法的使用流程图。FIG. 4 is a flow chart of a method for using a servo incremental high-precision pressure sensor according to the present invention.
其中,1为加载台,2为压力传感器,3为气囊,4为微位移驱动器,5为微位移传感器,6为基座。Among them, 1 is a loading table, 2 is a pressure sensor, 3 is an air bag, 4 is a micro-displacement driver, 5 is a micro-displacement sensor, and 6 is a base.
具体实施方式Detailed ways
下面将结合本发明实施例中的附图对本发明实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例仅是本发明一部分实施例,而不是全部的实施例。基于本发明中的实施例,本领域普通技术人员在没有做出创造性劳动前提下所获得的所有其他实施例,都属于本发明保护的范围。The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.
参照图1-图3所以,本发明为了解决质心测试台、卫星模拟器等应用中对大承载下增量载荷的高精度测量的需求,设计了一种伺服增量式高精度压力传感器,通过中心的气囊3平衡掉工作点的初始载荷,通过高精度的微位移传感器5测量增量载荷造成的位移变化量,通过高分辨率的微位移驱动器4使加载台1恢复至工作点位置,通过与微位移驱动器4串联的小量程高精度压力传感器2测量恢复至工作点时需要施加的示数增量,所有的压力传感器2的示数增量之和给出了相对于工作点载荷的载荷增量。由于工作点的大初始载荷被气囊3平衡掉,压力传感器2的量程只需要满增量载荷的测量需求就可以,可以选用较小量程的压力传感器2,当增量载荷相对于初始载荷很小时,可以选用较小量程的压力传感器2,从而显著提高测量精度。Referring to Fig. 1-Fig. 3, the present invention designs a servo incremental high-precision pressure sensor in order to solve the demand for high-precision measurement of incremental loads under large loads in applications such as centroid test benches and satellite simulators. The
本发明的伺服增量式高精度压力传感器,包括:加载台1、压力传感器2、气囊3、微位移驱动器4、微位移传感器5、基座6。The servo incremental high-precision pressure sensor of the present invention includes: a loading table 1 , a
加载台1支撑在压力传感器2和气囊3上侧,用于施加载荷,可以设计标准接口或者根据施加载荷设计专用接口,加载载荷的中心应当接近加载台1的几何中心,加载台1的几何尺寸要考虑气囊3的几何尺寸和压力传感器2、微位移驱动器4、微位移传感器5的分布和尺寸,通常可以以投影能够包络气囊3、压力传感器2、微位移驱动器4和微位移传感器5为宜,也可以根据安装空间的约束进行设计;The loading table 1 is supported on the upper side of the
压力传感器2下侧安装在微位移驱动器4上,上侧支撑加载台1,沿气囊3周向布局N个,N=3、4、……,用于测量待测载荷,N通常取3或者4,周向以均匀布局为宜,压力传感器2的量程需要根据待测增量载荷的大小、加载位置和N共同确定,以待测的最大的增量载荷为ΔFmax为例,同时,载荷施加时通过球铰施加,即不允许载荷出现偏心,此时压力传感器2的量程应满足The lower side of the
气囊3下侧安装在基座6上,上侧支撑加载台1,与基座6和加载台1同轴心,用于加载台1上的工作点载荷的承载,可以外接充气装置对气囊3充气,实现对气囊3刚度的调节,气囊3的承载能力需要根据加载载荷的大小进行选择,供气压力需要根据工作点的载荷大小和所需刚度进行确定,以工作点载荷F0为例,气囊3的承载能力应满足Fmax≥F0+ΔFmax,假设微位移驱动器4的位移分辨率为δPa,由于气囊3没有完全复位造成误差的容许的最大值为δFs,则气囊3在工作点的刚度应满足The lower side of the
如果微位移驱动器4采用压电陶瓷作动器,其位移分辨率通常可以达到纳米级,以δFs=0.001N为例,气囊3在工作点的刚度只需满足If the
这样的刚度要求,无需特别设计,很容易满足。Such rigidity requirements can be easily met without special design.
微位移驱动器4下侧安装在基座6上,上侧支撑压力传感器2,并与压力传感器2同轴心,沿气囊3周向布局N个,N=3、4、……,用于驱动加载台1恢复工作点位置,此处N与压力传感器2的数量N相同,其行程和驱动能力应该满足在施加增量载荷后,将气囊3的变形恢复到工作点位置,其精度需要根据对增量载荷的测量精度进行设计,在施加工作点载荷时,微位移驱动器4应当处于行程中位,在增加和减小最大的增量载荷时,分别位于行程的两个极限位置,由于其承载和位移成单向变化关系,可以从承载和行程上进行综合设计,即保证载荷增量最小(负值最大)时,微位移驱动器4的承载和位移输出不为零,而承载最大(正值最大)时,微位移驱动器4的承载不超出其最大承载能力,因此,微位移驱动器4的最大承载能力应满足The lower side of the
以N=4、ΔFmax=100N为例,Lmax≥50N。如果微位移驱动器4采用压电陶瓷作动器,其驱动能力通常能达到数百牛到数千牛,因此,这样的驱动能力要求极其容易实现。Taking N=4 and ΔF max =100N as an example, L max ≥50N. If the
微位移传感器5下侧安装在基座6,沿气囊3周向布局N个,N=3、4、……,用于测量加载台1的位移变化,此处N与压力传感器2的数量N相同,布局时可以与微位移驱动器4和压力传感器2交错布局或者同方向但在不同的分布圆上,其量程应该满足在施加增量载荷后测量变形增量的需求,或者设计有保护装置避免变形增量超出其量程造成损坏,其位移分辨率δPs需要根据增量载荷的测量精度进行设计,应该比微位移驱动器4的位移分辨率δPa小,即δPs<δPa,如果采用电容传感器作为微位移传感器5,位移分辨率通常可以达到亚纳米级;The
基座6其上安装气囊3,沿气囊3周向布置微位移传感器5和微位移驱动器4,底部可以加工通用的固定接口或根据需要设计专用的连接接口。The
如图4所示,在使用时,分为调试标定和应用两个阶段。As shown in Figure 4, in use, it is divided into two stages: debugging, calibration and application.
首先,在安装时需要保证压力传感器2的示数在量程中位时,微位移驱动器4也基本位于行程中位。根据工作点载荷F0调节气囊3的压力,使压力传感器2的示数位于量程中位,并记录微位移传感器5示数Pi0和压力传感器2示数Fi0,下标i表示压力传感器2或微位移传感器5的编号,i=1,2,…,N,N表示压力传感器2或微位移传感器5的总数;下标0表示初始值;First of all, when installing, it is necessary to ensure that when the indication of the
然后,在加载台1上施加载荷,此时微位移传感器5示数为Pi,如果加载台1的位移增量的平均值Then, apply a load on the loading table 1, at this time the
且/或多个微位移传感器5的位移增量的方差And/or the variance of the displacement increments of the plurality of
其中,ò和σ分别表示预设的位移精度参数和位移分布参数,μΔP和σΔP分别表示产生载荷增加时,所有微位移传感器5位移变化量的均值和方差。Among them, ò and σ represent the preset displacement accuracy parameters and displacement distribution parameters, respectively, and μΔP and σ ΔP represent the mean and variance of the displacement changes of all the
调节微位移驱动器4使μΔP和σΔP减小,直到μΔP<ò且σΔP<σ。读取此时的压力传感器2示数Fi,则加载台1上相对于工作点载荷F0增加的载荷为The
对增量载荷的测量误差包含两部分:多个压力传感器2的测量误差和由于气囊3没有完全复位带来的误差。作为保守估计,两部分误差直接叠加(采用误差传播公式计算时,综合误差小于直接叠加的结果);而多个压力传感器2的测量误差采用误差传播原理解算。记压力传感器2的相对测量精度为r0、量程为G,气囊3在工作点的刚度为k时,上述新增载荷的相对测量精度为The measurement error of the incremental load includes two parts: the measurement error of the
其中,工作点刚度k表示在工作点,载荷发生微小变化时造成位移的变化,载荷变化量与位移变化量的比值;a表示设计的相对工作点,即工作点载荷与压力传感器2的总量程之比Among them, the working point stiffness k represents the displacement change caused by the slight change of the load at the operating point, and the ratio of the load change to the displacement change; a represents the designed relative operating point, that is, the total amount of the operating point load and the
通过设计选择较小的k和ò使得kò<<NG,选择较大的a使得a>>1,可以得到By designing a smaller k and ò such that kò<<NG, and a larger a such that a>>1, we can get
即实现了更高的测量精度。根据前文的参数,这里进一步假设G=Lmax=100N、F0=2000N,可以得到a=5、r≈0.1r0,即精度提高了10倍。That is, higher measurement accuracy is achieved. According to the aforementioned parameters, it is further assumed here that G=L max =100N, F 0 =2000N, a=5, r≈0.1r 0 can be obtained, that is, the accuracy is improved by 10 times.
本发明针对大初始承载条件下高精度载荷增量的测量需求,提出了一种伺服增量式高精度传感器。该传感器采用气囊作为主承载,将初始载荷的位置作为平衡位置,在载荷发生变化后,利用微位移传感器5监测和微位移驱动器4驱动,使加载台1恢复到平衡位置,小量程的高精度的压力传感器2与微位移驱动器4串联后整体与气囊3主承载并联,因此,它们的示数变化之和给出了加载台的载荷增量。由于气囊3主承载抵消的初始的载荷,压力传感器2可以选择小量程的传感器,提高了整体的测量精度,实现了载荷增量的高精度测量。The invention proposes a servo incremental high-precision sensor for the measurement requirements of high-precision load increments under large initial bearing conditions. The sensor uses the airbag as the main load, and the position of the initial load as the equilibrium position. After the load changes, the
以上实施示例只是用于帮助理解本发明的方法及其核心思想,对于本领域的一般技术人员,依据本发明的思想,在具体实施方式及应用范围上还可以做出若干改进和润饰,这些改进和润饰也应视为本发明的保护范围。The above implementation examples are only used to help understand the method of the present invention and its core idea. For those skilled in the art, according to the idea of the present invention, several improvements and modifications can also be made in the specific implementation and application scope. These improvements and retouching should also be regarded as the protection scope of the present invention.
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Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1271720A (en) * | 1968-11-02 | 1972-04-26 | Schenck Gmbh Carl | Load cell with pressure member |
US6122976A (en) * | 1994-04-14 | 2000-09-26 | Cecap Ab | Pressure sensor with housing, sensor element having ceramic components, and support ring mounting sensor element to housing |
CN101067432A (en) * | 2006-09-26 | 2007-11-07 | 哈尔滨工业大学 | Air spring vibration isolation foundation with magnetic levitation unit |
CN201081720Y (en) * | 2007-10-26 | 2008-07-02 | 东南大学 | Capacitance method tester for testing driving force characteristics of electrostriction material |
CN103091008A (en) * | 2011-10-31 | 2013-05-08 | 爱信精机株式会社 | Load detection device for vehicle seat |
CN103353364A (en) * | 2013-06-20 | 2013-10-16 | 西安交通大学 | Load sensor possessing deformation compensation function |
CN103838259A (en) * | 2014-03-25 | 2014-06-04 | 哈尔滨工业大学 | Servo-type heavy-load ultraprecise air bag supporting electric leveling system and leveling method thereof |
CN107560933A (en) * | 2017-10-25 | 2018-01-09 | 北京富力通达科技有限公司 | A kind of device and method of big load testing machine loading and measurement |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
AU756444B2 (en) * | 1998-12-04 | 2003-01-16 | Weatherford Technology Holdings, Llc | Bragg grating pressure sensor |
CN103148818B (en) * | 2012-12-06 | 2016-03-02 | 北京控制工程研究所 | A kind of high accuracy gyroscope motor bearing loading method |
-
2021
- 2021-02-18 CN CN202110187585.2A patent/CN112857639B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1271720A (en) * | 1968-11-02 | 1972-04-26 | Schenck Gmbh Carl | Load cell with pressure member |
US6122976A (en) * | 1994-04-14 | 2000-09-26 | Cecap Ab | Pressure sensor with housing, sensor element having ceramic components, and support ring mounting sensor element to housing |
CN101067432A (en) * | 2006-09-26 | 2007-11-07 | 哈尔滨工业大学 | Air spring vibration isolation foundation with magnetic levitation unit |
CN201081720Y (en) * | 2007-10-26 | 2008-07-02 | 东南大学 | Capacitance method tester for testing driving force characteristics of electrostriction material |
CN103091008A (en) * | 2011-10-31 | 2013-05-08 | 爱信精机株式会社 | Load detection device for vehicle seat |
CN103353364A (en) * | 2013-06-20 | 2013-10-16 | 西安交通大学 | Load sensor possessing deformation compensation function |
CN103838259A (en) * | 2014-03-25 | 2014-06-04 | 哈尔滨工业大学 | Servo-type heavy-load ultraprecise air bag supporting electric leveling system and leveling method thereof |
CN107560933A (en) * | 2017-10-25 | 2018-01-09 | 北京富力通达科技有限公司 | A kind of device and method of big load testing machine loading and measurement |
Non-Patent Citations (3)
Title |
---|
Fibre-optic temperature and pressure sensor based on a deformable concave micro-mirror;Abdelhak Guermat 等;《Sensors and Actuators A: Physical》;20180102;全文 * |
光干涉法测量微机械零件变形的研究;田云辉 等;《光电工程》;20021031;全文 * |
离心力场中微型土压力传感器非线性响应分析;魏永权 等;《岩土力学》;20150131;全文 * |
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