CN104819899A - Rigidity detector - Google Patents
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- CN104819899A CN104819899A CN201510181927.4A CN201510181927A CN104819899A CN 104819899 A CN104819899 A CN 104819899A CN 201510181927 A CN201510181927 A CN 201510181927A CN 104819899 A CN104819899 A CN 104819899A
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Abstract
The invention discloses a rigidity detector which is mainly used for detecting rigidity of a small-diameter formed part, particularly an aerospace gyroscope torsion bar. A clamping mechanism, a loading mechanism and an optical measuring device of a conventional optical rigidity detector are improved, importantly, the clamping mechanism is designed into a rotary clamping mechanism with a dual-axis rotating function, the part is fixed by a cylinder and an elastic clamp and abutted to the loading mechanism, a sine protractor adjusted by a micrometer is additionally arranged on the lower portion of a collimator in the optical measuring device, and collimator adjusting precision and convenience are greatly improved. Besides, an optical zero calibration device is added, so that the part can be calibrated and positioned without the collimator after the part is clamped again. Comprehensively, the rigidity detector is convenient in calibration and clamping, high in detection precision, fine in stability, simple in structure, convenient to operate and higher in detection efficiency.
Description
Technical field
The present invention relates to a kind of stiffness excitations instrument, belong to the accurate stiffness excitations equipment of thin footpath forming part (torsion bar in such as aircraft gyroscope).
Background technology
The stiffness measurement of the current thin footpath forming part higher for dimensional accuracy all needs configuration stiffness excitations instrument except adopting traditional detection gimmick.And the design quality of stiffness excitations instrument is often directly connected to the final accuracy of detection of part and production efficiency.
Torsion bar is the vital part in aircraft gyroscope, is also more representative one thin footpath forming part, the accurate Sensitive Apparatus of its to be the thin footpath of being made up of high elastic modulus alloy be 0.1mm.The thin footpath forming technique of torsion bar is applied widely in space industry.Its importance is, should play resiliency supported effect in gyroscope, meets requirement and the characteristic index of disengaging again.Its most important characteristic index is " torsion bar rigidity "." torsion bar rigidity " may be defined as under the effect of moment of face, and the ratio of the moment of reaction M that the elastic force that torsion bar produces is directly proportional to torsion bar angle and torsion angle Φ, represents with C, that is:
C=M/ Φ (unit: mNm/rad)
The known measurement for rigidity is pressed test philosophy and is divided, and is divided into static measurement and the large class of dynamic measuring method two, the stiffness excitations instrument of corresponding two types.
1. dynamic measuring method:
I.e. thin footpath part angular rigidity dynamic measuring method, its ultimate principle is fixed on by thin footpath part in measured material by applying moment of flexure excitation to it, it is made to produce certain vibratory response, then the response characteristic of part vibration is measured by vibration measuring dynamic sensor, be generally the time history of displacement function, then calculated the natural frequency of vibrational system by certain method, then according to following formula, obtain the angular rigidity K of part further:
Wherein: ω
nfor the natural frequency of vibrational system; J is the equivalent moment of inertia of vibrational system.Dynamic measuring instrument utensil have easy to operate, testing efficiency is high, the feature such as reproducible, but due to equivalent moment of inertia in vibrational system be calculated value, and the accurate measurement of resonance frequency still can not solve very well, and therefore, measuring accuracy can't be satisfactory.
2. static measurement:
Mainly comprise following two classes:
1) machinery (power sensing) mensuration:
A kind of is the rigidity automatic testing equipment be made up of force snesor, displacement transducer and Single Chip Microcomputer (SCM) system, thin footpath part is fixed in measured material, top connects a measurement ring, force snesor has gear train to drive rising, with measurement loop contacts, record reading F0, S0 of now force snesor and displacement transducer, continue raising force sensor, obtain F1, S1, then joint angles stiffness K can be expressed as:
Wherein: L is for measuring radius.
Another kind is the stiffness measurement device based on microcomputer, part to be measured is fixed in measured material by it, apply micro-power through gauge head to part by micro-displacement mechanism and reference rounds reed thus make it produce angular displacement and indirectly obtain this angular displacement by displacement transducer, applied force is then calculated by the distortion of reference rounds reed and indirectly obtains.Utilize fine motion stand and leaf spring to realize micro-moment of flexure in addition to load, indirectly obtained the method for automatic measurement of torque and corner by the measurement of micrometric displacement, the method is consistent with aforementioned means in principle, and just version there occurs change.But be all weak separation elastic component owing to measuring ring, standard spring or leaf spring, and belong to indirect inspection, therefore systematically stability and precision are just limited to.
2) optical measuring method: namely the main thought of foundation first measures the size being applied to moment of reaction M on thin footpath forming part (torsion bar) and torsion angle Φ, directly utilizes following formula to calculate rigidity value C:
C=M/ Φ (unit: mNm/rad);
Hanging counterweight method is continued to use in optical measurement, current related equipment is when measuring, part to be measured is fixed on pedestal, pedestal is arranged on optical dividing head (catoptron) by cone, reflecting optics (dividing head) reflection ray is aimed at, the angle value of recording optically dividing head with collimating light pipe (collimator); Realized the torque load of the relative own axes of part by hanging counterweight (applying power M), make part generation around the angular deformation of its axis; Rotate optical dividing head, again aim at eyeglass reflection ray with collimating light pipe, the angle value of recording optically dividing head; The difference of twice angle value is exactly the corner value Φ of joint under torque load.
Although above-mentioned optics stiffness measurement instrument in stability and precision all than machinery (power sensing) stiffness measurement equipment come superior, still existing problems are as follows:
1) zero adjustment of collimating light pipe is a difficult problem always, in known instrument, optical dividing head (catoptron) only has the one degree of freedom around own axes usually, cannot finely tune around the longitudinal axis left rotation and right rotation perpendicular to horizontal table, cause range of adjustment limitation during calibrating operation.The measure of current reply is the displacement governor motion (leading screw) in the bottom design transverse direction of collimation apparatus, but the precision of this type of coarse adjustment mechanism not (μ level), and the higher degree of freedom of collimator (such as pivot angle) cannot be supplied to, cause calibration difficulties, calibration accuracy is low, and operation is wasted time and energy.
2) the longitudinal clamping of part adopt bolt tightening to fix, dismounting and change inconvenience, causes detection efficiency low.
On the other hand, known optics rigidity test equipment is not designed with independently auxiliary dividing head zero adjustment equipment, when new parts changed by clamping when last piece test is complete, needs to re-start calibration operation, very loaded down with trivial details, greatly reduces work efficiency.
Summary of the invention
The present invention seeks to: provide that a kind of calibration is convenient, accuracy of detection is high and good stability, structure is simple simultaneously, and easy to operate, clamping is convenient, the stiffness excitations instrument that detection efficiency is higher.
Technical scheme of the present invention is: a kind of stiffness excitations instrument, comprise base, it is characterized in that described base be provided with clamping device for clamping measured workpiece, for measured workpiece is applied moment of face load maintainer and for measuring measured workpiece stand under load time moment angle variable quantity optical measuring device; Wherein:
Described clamping device is the rotation clamping device with dual-axis rotation function, it comprises bracing frame, Y-axis cylinder, is rotationally connected and the rotary sleeve that can rotate around Y-axis and the collet be fixed on rotary sleeve with Y-axis cylinder front end, and measured workpiece is fixedly clamped by collet; Support frame as described above is arranged on base by the turning axle arranged along Z-axis direction;
Described load maintainer is push against with measured workpiece and the lever weight mechanism of two ends reinforcing;
Described optical measuring device comprises collimator, double mirror, sine gauge and milscale; Described collimator along X axis arrange and relative with clamping device, described double mirror is fixed on described rotary sleeve, and described collimator is located on sine gauge, and the side, bottom of sine gauge is provided with the milscale for regulating its angle;
Described X, Y, Z axis becomes orthogonal space to distribute, and wherein Z axis is perpendicular to base.
It may be noted that the lever weight mechanism in the present invention and the hanging counterweight mechanism in routine techniques, its version is various, but core is all come for the two ends of thin footpath to be measured part increase load (reinforcing) by lever principle, and produces moment.In preferred structural design, described lever weight mechanism in the present invention comprises lever arm, the center pivotable of described lever arm to be located on bracing frame and to be pushed against with measured workpiece, and the bracing frame of lever arm both sides is respectively arranged with pulley, the two ends of lever arm are all fixed with by the line of force, and the pulley that described stressed wire-wound is excessively corresponding also arranges the line hook being used for fixing counterweight.By pulley can improve whole lever weight mechanism afterburning time smoothness and stability.
Further, the present invention also comprises double mirror zero adjustment device, this device comprises is located at reflecting plate on base and assisted calibration light source, when double mirror is positioned at the zero-bit of error allowed band, the light of described assisted calibration light source injection is default zero adjustment region in the region dropped on reflecting plate after double mirror reflection; During calibration, the injection of assisted calibration light source need be verified and whether fall within the above-mentioned default zero adjustment region of reflecting plate via the light that double mirror reflects.
Further, double mirror described in the present invention is between described reflecting plate and collimator.
Further, the bottom of sine gauge described in the present invention is provided with milscale briquetting, and the top of described milscale and milscale briquetting offset.Need point out the present invention design in sine gauge see prior art, it has sine plate and rotates two the sine gauge rotating shafts be located at bottom it, the sine gauge rotating shaft of its middle front part is supported by the pivot brackets of design on base, and be fixed by rotating shaft briquetting, the sine gauge rotating shaft at rear portion is then just positioned at directly over milscale.
Further, base described in the present invention is provided with the axis hole penetrated for turning axle, is provided with the Z axis bearing coordinated with turning axle in hole.
Further, bracing frame described in the present invention is provided with the perforate for rotary sleeve and Y-axis cylinders, is provided with the Y-axis bearing coordinated with rotary sleeve in hole.
By set up Z axis bearing can greatly promote rotary sleeve rotate time stability, thus improve detect time degree of regulation.Same Y-axis bearing of setting up can greatly promote stability when turning axle (bracing frame) rotates, thus degree of regulation when can improve detection equally.And in the specific implementation, Z axis bearing in this instrument and Y-axis bearing be sliding bearing all preferably, take into account the situation of moving vertically when considering rotary sleeve clamping, and the possible height of bracing frame regulates (now turning axle is up and down relative to bearing) for the requirement of slip stationarity.
Further, base bottom described in the present invention is provided with some horizontal adjustment screw for adjusting base levelness.Horizontal adjustment screw is prior art, and its screw rod top is bolted with the tight nut of spelling and contacts with base bottom, for the adjustment of base levelness.
Further, bracing frame described in the present invention is fixed with the Z-axis direction rotation adjusting lever rotated around Z axis for controlling bracing frame, the convenient rotation regulable control for bracing frame.
Further, rotary sleeve described in the present invention is fixed with the Y-axis rotation adjusting lever rotated around Y-axis for controlling rotary sleeve, the convenient rotation regulable control for rotary sleeve (thin footpath forming part also namely to be measured).
Principle of work of the present invention following (for torsion bar):
Time initial, first utilize collet to be clamped by torsion bar, then drive Y-axis cylinder to be held out against by torsion bar on lever arm, start immediately double mirror X to zero adjustment, period need to rotate rotary sleeve and by sine gauge to regulate collimator;
When double mirror is adjusted to the zero-bit in error allowed band, the light beam of collimator injection records the angle value of now double mirror (being also zero value) after double mirror reflects; Meanwhile, open assisted calibration light source, injection light region dropped on reflecting plate after double mirror reflection is default zero adjustment region (calibrating for during next part testing);
By lever weight mechanism be torsion bar apply power, torsion bar is made to produce the torque load M of relative own axes, and the angular deformation produced around its axis, then rotary sleeve is rotated, utilize collimator again to aim at the injection of double-sided reflecting eyeglass and reflection ray, record angle value now, the difference of twice angle value, be exactly the corner value Φ of torsion bar under torque load M, finally utilize formula:
C=M/ Φ (unit: mNm/rad), calculates torsion bar rigidity C;
When next piece test of replacing, and when need recalibrate double mirror zero-bit, only need open assisted calibration light source, rotate rotary sleeve simultaneously, whether the injection of verification assisted calibration light source also falls within zero adjustment region that reflecting plate is preset via the light of double mirror reflection, zero adjustment and conveniently.
Certainly, except torsion bar, the present invention also can realize the stiffness excitations of other thin footpath forming parts.
Advantage of the present invention is:
1. this stiffness excitations instrument provided by the invention, important improvement made by its optics stiffness excitations instrument for routine, by the rotation clamping device of design with dual-axis rotation function, the rotation adjustment of Y, Z two degree of freedom can be realized for double mirror (and part) when making to detect, break through the limitation of original calibration adjustments, thus contribute to improving calibration accuracy and calibration convenience.And because clamping device regulates with Y, Z double freedom, the design of the transversal displacement governor motion for collimator can be omitted, cost-saving, reduce calibration operation, improve operating efficiency.
2. this stiffness excitations instrument provided by the invention, sine gauge principle design sine gauge governor motion is utilized bottom its collimator, and by carrying out meticulous adjustment sine gauge angle by milscale, substantially increase the calibration accuracy of collimator and regulate convenience, thus contributing to the quality promoting the detection of final detail rigidity.
3. this stiffness excitations instrument provided by the invention, utilizes cylinder and collet to fix part in its clamping device, improves clamping convenience and the stability of part, contributes to the work efficiency and the work quality that improve stiffness excitations.
4. this stiffness excitations instrument provided by the invention, by setting up pulley in its lever weight mechanism, make the supporting by the line of force by pulley and be elevated of counterweight, can improve whole lever weight mechanism afterburning time smoothness and stability, guarantee to add loading accurately and reliable.
5. this stiffness excitations instrument provided by the invention, because being designed with independent double mirror zero adjustment device, the zero-bit being specifically designed to the tested part of new clamping is recalibrated and contraposition, therefore again correct without the need to collimation instrument as routine techniques by this device, the operational sequence simplified, reduce operation easier, substantially increase calibration efficiency.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the invention will be further described:
Fig. 1 is structural front view of the present invention;
Fig. 2 is the structure vertical view of Fig. 1.
Wherein: 1, assisted calibration light source; 2, reflecting plate; 3, lever arm; 4, Z axis bearing; 5, turning axle; 6, double mirror; 7, counterweight; 8, line hook; 9, by the line of force; 10, pulley; 11, sine gauge rotating shaft; 12, collimator; 13, horizontal adjustment screw; 14, tight nut is spelled; 15, sine gauge; 16, milscale briquetting; 17, milscale; 18, rotating shaft briquetting; 19, base; 20, Z-axis direction rotation adjusting lever; 21, torsion bar; 22, bracing frame; 23, rotary sleeve; 24, Y-axis cylinder; 25, Y-axis bearing; 26, collet; 27, Y-axis rotation adjusting lever.
Embodiment
Embodiment: shown in composition graphs 1 and Fig. 2, for a kind of embodiment of stiffness excitations instrument of the present invention, it is mainly used in the stiffness excitations of the vital part torsion bar in space flight gyroscope, being constructed as follows of this instrument: there is base 19, described base 19 be provided with clamping device for clamping measured workpiece 21, for measured workpiece 21 is applied moment of face load maintainer and for measuring measured workpiece 21 stand under load time moment angle variable quantity optical measuring device; Wherein:
Described clamping device is the rotation clamping device with dual-axis rotation function, the formation of this mechanism is: bracing frame 22, Y-axis cylinder 24, be rotationally connected and the rotary sleeve 23 that can rotate around Y-axis and the collet 26 be fixed on rotary sleeve 23 with Y-axis cylinder 22 front end, and measured workpiece 21 is fixedly clamped by collet 26; Support frame as described above 22 is arranged on base 19 by the turning axle 5 arranged along Z-axis direction;
Described load maintainer is push against with measured workpiece 21 and the lever weight mechanism of two ends reinforcing;
The formation of described optical measuring device is: collimator 12, double mirror 6, sine gauge 15 and milscale 17; Described collimator 12 along X axis arrange and relative with clamping device, described double mirror 6 is fixed on described rotary sleeve 23, and described collimator 12 is located on sine gauge 15, and the side, bottom of sine gauge 15 is provided with the milscale 17 for regulating its angle.
Described X, Y, Z axis becomes orthogonal space to distribute, and wherein Z axis is perpendicular to base.
The mechanism of lever weight described in the present embodiment is specifically constructed as follows: have lever arm 3, the center pivotable of described lever arm 3 to be located on bracing frame 22 and to be pushed against with measured workpiece 21, and the bracing frame 22 of lever arm 3 both sides is respectively arranged with pulley 10, the two ends of lever arm 3 are all fixed with by the line of force 9, and the described pulley 10 being subject to the line of force 9 to walk around correspondence also arranges the line hook 8 for fixing counterweight 7.By pulley 10 can improve whole lever weight mechanism afterburning time smoothness and stability.
Shown in composition graphs 1 and Fig. 2, double mirror zero adjustment device is also designed with in the present embodiment, the formation of this device is: have and be located at reflecting plate 2 on base 19 and assisted calibration light source 1, described double mirror 6 is between described reflecting plate 2 and collimator 12.When double mirror 6 is positioned at the zero-bit of error allowed band, the light that described assisted calibration light source 1 penetrates is default zero adjustment region in the region dropped on reflecting plate 2 after double mirror 6 reflects; During calibration, assisted calibration light source 1 need be verified and penetrate and whether fall within the above-mentioned default zero adjustment region of reflecting plate 2 via the light that double mirror 6 reflects.
The bottom of sine gauge 15 described in the present embodiment is also provided with milscale briquetting 16, and the top of described milscale 17 and milscale briquetting 16 offset.Need point out the present invention design in sine gauge 15 see prior art, it has sine plate (not marking) and rotates two the sine gauge rotating shafts 11 be located at bottom it, the sine gauge rotating shaft 11 of its middle front part is supported by the pivot brackets (not marking) of design on base 19, and be fixed by rotating shaft briquetting 18 (see Fig. 2), the sine gauge rotating shaft (not marking) at rear portion is then just positioned at directly over milscale 17.
Base 19 described in the present embodiment is provided with the axis hole penetrated for turning axle 5, is provided with the Z axis bearing 4 coordinated with turning axle in hole.And support frame as described above is provided with the perforate be connected with Y-axis cylinder 24 for rotary sleeve 23, in hole, be provided with the Y-axis bearing 25 coordinated with rotary sleeve 23.
Stability when rotary sleeve 23 rotates can greatly be promoted by setting up Z axis bearing 4, thus improve degree of regulation when detecting.Same Y-axis bearing 25 of setting up can greatly promote stability when turning axle 5 (bracing frame 22) rotates, thus degree of regulation when can improve detection equally.And in the specific implementation, Z axis bearing 4 in this instrument and Y-axis bearing 25 be sliding bearing all preferably, take into account the situation of moving vertically when considering rotary sleeve 23 clamping, and the height adjustment that bracing frame 22 is possible (now the relative bearing of turning axle 5 is up and down) is for the requirement of slip stationarity.
Some (specifically six) horizontal adjustment screw 13 for adjusting base 19 levelness is provided with bottom base 19 described in the present embodiment, horizontal adjustment screw 13 is prior art, its screw top is bolted with the tight nut 14 of spelling and contacts with bottom base 19, for the adjustment of base 19 levelness.
Bracing frame 22 described in the present embodiment is fixed with the Z-axis direction rotation adjusting lever 20 rotated around Z axis for controlling bracing frame 22, and described rotary sleeve 23 is fixed with the Y-axis rotation adjusting lever 27 rotated around Y-axis for controlling rotary sleeve 23.
Principle of work of the present invention following (stiffness excitations for torsion bar 21):
Time initial, collet 26 is first utilized to be clamped by torsion bar 21, then drive Y-axis cylinder 24 to hold out against torsion bar 21 on lever arm 3, start the X of double mirror 6 immediately to zero adjustment, period need to rotate rotary sleeve 23 and by sine gauge 15 to regulate collimator 12;
When double mirror 6 is adjusted to the zero-bit in error allowed band, the light beam that collimator 12 penetrates records the angle value (being also zero value) of now double mirror 6 after double mirror 6 reflects; Meanwhile, open assisted calibration light source 1, injection light region dropped on reflecting plate 2 after double mirror 6 reflects is default zero adjustment region (calibrating for during next part testing);
Be that torsion bar 21 applies power by lever weight mechanism, torsion bar 21 is made to produce the torque load M of relative own axes, and the angular deformation produced around its axis, then rotary sleeve 23 is rotated, utilize collimator 12 again to aim at the eyeglass injection also reflection ray of double mirror 6, record angle value now, the difference of twice angle value, be exactly the corner value Φ of torsion bar 21 under torque load M, finally utilize formula:
C=M/ Φ (unit: mNm/rad), calculates torsion bar rigidity C;
When next piece test of replacing, and when need recalibrate double mirror 6 zero-bit, only need open assisted calibration light source 1, rotate rotary sleeve 23 simultaneously, whether verification assisted calibration light source 1 penetrates and falls within zero adjustment region default on reflecting plate 2 via the light that double mirror 6 reflects, zero adjustment and convenience thereof.
Certain above-described embodiment, only for technical conceive of the present invention and feature are described, its object is to person skilled in the art can be understood content of the present invention and implement according to this, can not limit the scope of the invention with this.All modifications done according to the Spirit Essence of main technical schemes of the present invention, all should be encompassed within protection scope of the present invention.
Claims (10)
1. a stiffness excitations instrument, comprise base (19), it is characterized in that described base (19) be provided with clamping device for clamping measured workpiece (21), for measured workpiece (21) is applied moment of face load maintainer and for measuring measured workpiece (21) stand under load time moment angle variable quantity optical measuring device; Wherein:
Described clamping device is the rotation clamping device with dual-axis rotation function, it comprises bracing frame (22), Y-axis cylinder (24), is rotationally connected and the rotary sleeve (23) that can rotate around Y-axis and the collet (26) be fixed on rotary sleeve (23) with Y-axis cylinder (22) front end, and measured workpiece (21) is fixedly clamped by collet (26); Support frame as described above (22) is arranged on base (19) by the turning axle (5) arranged along Z-axis direction;
Described load maintainer is push against and the lever weight mechanism of two ends reinforcing with measured workpiece (21);
Described optical measuring device comprises collimator (12), double mirror (6), sine gauge (15) and milscale (17); Described collimator (12) along X axis arrange and relative with clamping device, described double mirror (6) is fixed on described rotary sleeve (23), described collimator (12) is located on sine gauge (15), and the side, bottom of sine gauge (15) is provided with the milscale (17) for regulating its angle;
Described X, Y, Z axis becomes orthogonal space to distribute, and wherein Z axis is perpendicular to base.
2. stiffness excitations instrument according to claim 1, it is characterized in that described lever weight mechanism comprises lever arm (3), the center pivotable of described lever arm (3) is located at bracing frame (22) and is gone up and push against with measured workpiece (21), and the bracing frame (22) of lever arm (3) both sides is respectively arranged with pulley (10), the two ends of lever arm (3) are all fixed with by the line of force (9), describedly walk around corresponding pulley (10) by the line of force (9) and arrange the line hook (8) being used for fixing counterweight (7).
3. stiffness excitations instrument according to claim 1, characterized by further comprising double mirror zero adjustment device, this device comprises is located at reflecting plate (2) on base (19) and assisted calibration light source (1), when double mirror (6) is positioned at the zero-bit of error allowed band, the light that described assisted calibration light source (1) is penetrated is default zero adjustment region in the region dropped on reflecting plate (2) after double mirror (6) reflection; During calibration, assisted calibration light source (1) injection need be verified and whether fall within the above-mentioned default zero adjustment region of reflecting plate (2) via the light that double mirror (6) reflects.
4. stiffness excitations instrument according to claim 3, is characterized in that described double mirror (6) is positioned between described reflecting plate (2) and collimator (12).
5. stiffness excitations instrument according to claim 1, it is characterized in that the bottom of described sine gauge (15) is provided with milscale briquetting (16), and the top of described milscale (17) and milscale briquetting (16) offset.
6. stiffness excitations instrument according to claim 1, is characterized in that described base (19) is provided with the axis hole penetrated for turning axle (5), is provided with the Z axis bearing (4) coordinated with turning axle in hole.
7. stiffness excitations instrument according to claim 1, it is characterized in that support frame as described above is provided with the perforate be connected with Y-axis cylinder (24) for rotary sleeve (23), in hole, be provided with the Y-axis bearing (25) coordinated with rotary sleeve (23).
8. stiffness excitations instrument according to claim 1, is characterized in that described base (19) bottom is provided with some horizontal adjustment screw (13) for adjusting base (19) levelness.
9. stiffness excitations instrument according to claim 1, is characterized in that support frame as described above (22) is fixed with the Z-axis direction rotation adjusting lever (20) rotated around Z axis for controlling bracing frame (22).
10. stiffness excitations instrument according to claim 1, is characterized in that described rotary sleeve (23) is fixed with the Y-axis rotation adjusting lever (27) rotated around Y-axis for controlling rotary sleeve (23).
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Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108132027A (en) * | 2016-11-30 | 2018-06-08 | 北京航天计量测试技术研究所 | Alignment measurement instrument integration school zero and alignment device |
| CN112595602A (en) * | 2020-11-13 | 2021-04-02 | 河北汉光重工有限责任公司 | Device and method for detecting rigidity of flexible joint of gyroscope |
| CN114441330A (en) * | 2022-02-07 | 2022-05-06 | 北京半导体专用设备研究所（中国电子科技集团公司第四十五研究所） | Air floatation rigidity loading device, air floatation rigidity testing equipment and air floatation rigidity testing method |
| CN114578327A (en) * | 2022-02-23 | 2022-06-03 | 森思泰克河北科技有限公司 | Detection device and detection method for laser radar reflecting mirror |
| CN114894451A (en) * | 2022-04-12 | 2022-08-12 | 北京航空航天大学 | Measuring platform for calibrating rotational stiffness of elastic element |
Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2413279Y (en) * | 2000-03-23 | 2001-01-03 | 铁道部科学研究院铁道建筑研究所 | Drop hammer type roadbed stiffness tester |
| US20060275045A1 (en) * | 2005-06-03 | 2006-12-07 | Canon Kabushiki Kaisha | Sheet material discrimination apparatus, sheet material information output apparatus, and image forming apparatus |
| CN101101248A (en) * | 2007-07-20 | 2008-01-09 | 上海应用技术学院 | Adjustable clamping mechanism for miniature torsion bar stiffness test |
| CN201600242U (en) * | 2010-01-28 | 2010-10-06 | 洛阳轴研科技股份有限公司 | Bearing axial rigidity measurement instrument |
| CN203414347U (en) * | 2013-09-13 | 2014-01-29 | 湘潭电机股份有限公司 | Rigidity detecting device |
| CN104458439A (en) * | 2014-09-10 | 2015-03-25 | 南通昱品通信科技有限公司 | Device for detecting flexural rigidity of seabed optical cable |
| CN204666448U (en) * | 2015-04-16 | 2015-09-23 | 吴江市天龙机械有限公司 | Stiffness excitations instrument |
-
2015
- 2015-04-16 CN CN201510181927.4A patent/CN104819899B/en active Active
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN2413279Y (en) * | 2000-03-23 | 2001-01-03 | 铁道部科学研究院铁道建筑研究所 | Drop hammer type roadbed stiffness tester |
| US20060275045A1 (en) * | 2005-06-03 | 2006-12-07 | Canon Kabushiki Kaisha | Sheet material discrimination apparatus, sheet material information output apparatus, and image forming apparatus |
| CN101101248A (en) * | 2007-07-20 | 2008-01-09 | 上海应用技术学院 | Adjustable clamping mechanism for miniature torsion bar stiffness test |
| CN201600242U (en) * | 2010-01-28 | 2010-10-06 | 洛阳轴研科技股份有限公司 | Bearing axial rigidity measurement instrument |
| CN203414347U (en) * | 2013-09-13 | 2014-01-29 | 湘潭电机股份有限公司 | Rigidity detecting device |
| CN104458439A (en) * | 2014-09-10 | 2015-03-25 | 南通昱品通信科技有限公司 | Device for detecting flexural rigidity of seabed optical cable |
| CN204666448U (en) * | 2015-04-16 | 2015-09-23 | 吴江市天龙机械有限公司 | Stiffness excitations instrument |
Non-Patent Citations (3)
| Title |
|---|
| 刘春节: ""动力调谐陀螺仪微弹性零件刚度系数的测量方法"", 《常州工学院学报》 * |
| 刘春节等: ""微型扭杆刚度自动测试仪的研制"", 《计量学报》 * |
| 赵维谦等: ""弹挠性零件刚度系数测量方法"", 《航天工艺》 * |
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| CN112595602A (en) * | 2020-11-13 | 2021-04-02 | 河北汉光重工有限责任公司 | Device and method for detecting rigidity of flexible joint of gyroscope |
| CN114441330A (en) * | 2022-02-07 | 2022-05-06 | 北京半导体专用设备研究所（中国电子科技集团公司第四十五研究所） | Air floatation rigidity loading device, air floatation rigidity testing equipment and air floatation rigidity testing method |
| CN114441330B (en) * | 2022-02-07 | 2023-09-22 | 北京半导体专用设备研究所（中国电子科技集团公司第四十五研究所） | Air floatation stiffness loading device, air floatation stiffness testing equipment and air floatation stiffness testing method |
| CN114578327A (en) * | 2022-02-23 | 2022-06-03 | 森思泰克河北科技有限公司 | Detection device and detection method for laser radar reflecting mirror |
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