CN102494845A - Device and method for measuring inertia product of object - Google Patents

Device and method for measuring inertia product of object Download PDF

Info

Publication number
CN102494845A
CN102494845A CN201110375927XA CN201110375927A CN102494845A CN 102494845 A CN102494845 A CN 102494845A CN 201110375927X A CN201110375927X A CN 201110375927XA CN 201110375927 A CN201110375927 A CN 201110375927A CN 102494845 A CN102494845 A CN 102494845A
Authority
CN
China
Prior art keywords
dull
turnover panel
stereotyped
angle
inertia
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
CN201110375927XA
Other languages
Chinese (zh)
Inventor
毕凤荣
邵康
张俊红
王霞
毕晓阳
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Tianjin University
Original Assignee
Tianjin University
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Tianjin University filed Critical Tianjin University
Priority to CN201110375927XA priority Critical patent/CN102494845A/en
Publication of CN102494845A publication Critical patent/CN102494845A/en
Pending legal-status Critical Current

Links

Images

Landscapes

  • Force Measurement Appropriate To Specific Purposes (AREA)

Abstract

The invention relates to a device and method for testing static balance of a machine or a structural component, in particular to measurement of the inertia product of an object. The invention provides a device and method for measuring the inertia product of an object, which are convenient to operate. The device comprises a first flat plate, an overturning plate, three slings arranged at the outer edge of the first flat plate, a bracket connected with the other ends of the slings, tension sensors, a tiny break arranged on the first flat plate, a photoelectric signal sensor arranged at the tiny break, an optical signal reading device connected with the photoelectric signal sensor, wherein the first flat plate is provided with a through hole at the center, the overturning plate is similar to the polygonal through hole in shape and can respectively rotate for any angle along a hinge joint connection line relative to the first flat plate, and a tension sensor is arranged on each sling. The method is based on a simple principle, is easy to control and convenient to operate and is applicable to most of complicated power devices.

Description

Object product of inertia measurement mechanism and method
Technical field
The present invention relates to the orthostatic proving installation and the method for machine or structure member, further relate to the mensuration of the object product of inertia.
Background technology
The object product of inertia is an important physical parameter in the Machine Design, still has nothing to do in the record of this respect in the prior art.Therefore, be badly in need of a kind of easy object mass center measurement mechanism and method.
Summary of the invention
The invention provides a kind of object product of inertia measurement mechanism and method easy and simple to handle.Surpass 500kg for quality, the large-sized power plant that physical dimension surpasses 1.5m has remarkable advantages more.
The technical scheme that the present invention adopted is following:
Object product of inertia measurement mechanism comprises:
First flat board of the unsettled placement of level, the first dull and stereotyped geometric shape is that circle or limit number are the regular polygon of 3N, N is the integer more than or equal to 1; There is 1 through hole the first dull and stereotyped center, and the geometric shape that through hole is is that circle or limit number are the regular polygon of 2N, and N is the integer more than or equal to 2; The turnover panel similar with the regular polygon via hole profile, turnover panel is used to hold testee; At least 1 pair of pin joint in center of the center, 2 sides that is positioned at turnover panel symmetry and the corresponding equilateral through hole of first dull and stereotyped polygon side, said turnover panel can overturn with respect to first flat board respectively along the pin joint line at any angle; Be positioned at the first dull and stereotyped outer rim place, equidistantly distribute, equal length and perpendicular to first dull and stereotyped 3 hoist cables; The support that is connected with the hoist cable other end; Be positioned at the pulling force sensor on the every hoist cable; Be positioned at the small gap on first flat board; Be positioned at the photoelectric sensor of opening position, under the static steady state (SS), said photoelectric sensor and support keep fixing position relation, and when first flat board along the center of circle minor rotation took place, the signal of photoelectric sensor changed; The photosignal reading device links to each other with photoelectric signal sensor.
Said regular polygon through hole is square preferably, and said turnover panel profile is square preferably; Said first dull and stereotyped preferred equilateral triangle of geometric shape or the equilateral hexagon is positioned at the place, summit with the junction of hoist cable.
On said apparatus, realize object product of inertia measuring method, definition: three ropes are respectively first rope, second rope, the 3rd rope, and its length is defined as L; Its corresponding pulling force sensor is respectively first pulling force sensor, second pulling force sensor, the 3rd pulling force sensor; On first flat board, three ropes and the first dull and stereotyped node are defined as first node, second node, the 3rd node respectively, and the first dull and stereotyped center is true origin O; The horizontal range at the hoist cable node distance first dull and stereotyped center is defined as R; The acceleration of gravity of measuring the place is defined as g, and the cycle of rocking is T, and first flat board is I with the common moment of inertia of turnover panel Pi
Barycenter with testee is true origin O 1, be the Z axle perpendicular to the turnover panel direction, two other direction that is parallel to turnover panel is X axle and Y axle, sets up the rectangular coordinate system of testee;
Step comprises:
Step 1: the adjustment horizontal stand, guarantee to be in same surface level with the node of rope; Adjust first flat board, make it keep surface level, the adjustment turnover panel is to horizontal level; Testee is placed on the turnover panel, guarantee that the barycenter of testee and the first dull and stereotyped center are on the same perpendicular line; Give first dull and stereotyped small power, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read torsional oscillation cycle T 1 through photoelectric sensor; At this moment, the reading of first, second, third pulling force sensor is respectively F 11, F 12, F 13First flat board is I with the common moment of inertia of turnover panel P1
Step 2: let testee at first around O 1Angle of Z axle rotation lets turnover panel along rotating a certain angle around pin joint then, lets testee translation in reprint, guarantees true origin O 1Be on the same perpendicular line with the first dull and stereotyped center, measure O this moment 1X axle, O 1Y axle, O 1The angle of Z axle and vertical direction 1, β 1, γ 1Give first dull and stereotyped small power then, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read the torsional oscillation cycle T through photoelectric sensor 2At this moment, the reading of first, second, third pulling force sensor is respectively F 21, F 22, F 23
Step 3: turnover panel recovers horizontal, and repeating step two records other at least four groups of different angle i, β i, γ i, read the torsional oscillation cycle T i, read the reading F of first, second, third pulling force sensor I1, F I2, F I3
Step 4: according to formula I Z = ( F 11 + F 12 + F 13 ) * R 2 * T 1 2 4 π 2 * L - I p 1 Calculate and obtain Iz, under other anglec of rotation, at first calculate and obtain first flat board and the common moment of inertia I of turnover panel Pi,
I iNumerical computation method following: I i = ( F i 1 + F i 2 + F i 3 ) * R 2 * T i 2 4 π 2 * L - I Pi
Then with I 2, I 3, I 4, I 5, I 6Numerical value and corresponding angle α i, β i, γ iValue is brought equation into,
I i = cos α i cos β i cos γ i * I x - I xy - I xz - I yx I y - I yz - I zx - I zy I z * cos α i cos β i cos γ i
At I zUnder the known situation, simultaneous equations are tried to achieve other five variate-value: I x, I y, I Xy, I Xz, I Yz
And then, can obtain the ellipsoid of inertia equation of testee about barycenter.
Use in the engineering that this method finally can record object and use more the center principal moment of inertia and the center principal axis of inertia.This method principle is simple, is easy to control, is convenient to operation, is suitable for the power-equipment of most of complicacies.
Description of drawings
Fig. 1 is the synoptic diagram of embodiment.1 represents support among the figure, and 2 represent pulling force sensor; 3 represent testee, and 4 represent hoist cable, and 5 represent the rope lengths regulating device, and 6 represent first flat board, and 7 represent charge amplifier, and 8 represent computing machine, and 9 represent photoelectric sensor, and 10 represent turnover panel.
Fig. 2 is the synoptic diagram that rotates to an angle.
Fig. 3 is the local enlarged drawing of A among Fig. 2.
Embodiment
Map 1 explanation embodiment of the present invention.
Object product of inertia measurement mechanism comprises:
First dull and stereotyped 6, the first dull and stereotyped geometric shape of the unsettled placement of level is circular; There is 1 through hole the first dull and stereotyped center, and the geometric shape that through hole is is a rectangle; With the turnover panel 10 of rectangular through-hole appearance similar, turnover panel is used to hold testee 3; At least 1 pair of pin joint in center of the center, 2 sides that is positioned at turnover panel symmetry and the first corresponding dull and stereotyped rectangular through-hole side, said turnover panel can overturn with respect to first flat board respectively along the pin joint line at any angle; Be positioned at the first dull and stereotyped outer rim place, equidistantly distribute, equal length and perpendicular to first dull and stereotyped 3 hoist cables 4; The support 1 that is connected with the hoist cable other end; Be positioned at the pulling force sensor 2 on the every hoist cable; Be positioned at the small gap on first flat board; Be positioned at the photoelectric sensor 9 of opening position, under the static steady state (SS), said photoelectric sensor and support keep fixing position relation, and when first flat board along the center of circle minor rotation took place, the signal of photoelectric sensor changed; Photosignal reading device---computing machine 8 links to each other with photoelectric signal sensor.
On said apparatus, realize object product of inertia measuring method, definition: three ropes are respectively first rope, second rope, the 3rd rope, and its length is defined as L; Its corresponding pulling force sensor is respectively first pulling force sensor, second pulling force sensor, the 3rd pulling force sensor; On first flat board, three ropes and the first dull and stereotyped node are defined as first node, second node, the 3rd node respectively, and the first dull and stereotyped center is true origin O; The horizontal range at the hoist cable node distance first dull and stereotyped center is defined as R; The acceleration of gravity of measuring the place is defined as g, and the cycle of rocking is T, and first flat board is I with the common moment of inertia of turnover panel Pi
Barycenter with testee is true origin O 1, be the Z axle perpendicular to the turnover panel direction, two other direction that is parallel to turnover panel is X axle and Y axle, sets up the rectangular coordinate system of testee;
Step comprises:
Step 1: the adjustment horizontal stand, guarantee to be in same surface level with the node of rope; Adjust first flat board, make it keep surface level, the adjustment turnover panel is to horizontal level; Testee is placed on the turnover panel, guarantee that the barycenter of testee and the first dull and stereotyped center are on the same perpendicular line; Give first dull and stereotyped small power, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read the torsional oscillation cycle T through photoelectric sensor 1At this moment, the reading of first, second, third pulling force sensor is respectively F 11, F 12, F 13First flat board is I with the common moment of inertia of turnover panel P1
Step 2: let testee at first around O 1Angle of Z axle rotation lets turnover panel along rotating a certain angle around pin joint then, lets testee translation in reprint, guarantees true origin O 1Be on the same perpendicular line with the first dull and stereotyped center, measure O this moment 1X axle, O 1Y axle, O 1The angle of Z axle and vertical direction 1, β 1, γ 1Give first dull and stereotyped small power then, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read the torsional oscillation cycle T through photoelectric sensor 2At this moment, the reading of first, second, third pulling force sensor is respectively F 21, F 22, F 23
Step 3: turnover panel recovers horizontal, and repeating step two records other at least four groups of different angle i, β i, γ i, read the torsional oscillation cycle T i, read the reading F of first, second, third pulling force sensor I1, F I2, F I3
Step 4: according to formula I Z = ( F 11 + F 12 + F 13 ) * R 2 * T 1 2 4 π 2 * L - I p 1 Calculate and obtain Iz, under other anglec of rotation, at first calculate and obtain first flat board and the common moment of inertia I of turnover panel Pi,
I iNumerical computation method following: I i = ( F i 1 + F i 2 + F i 3 ) * R 2 * T i 2 4 π 2 * L - I Pi
Then with I 2, I 3, I 4, I 5, I 6Numerical value and corresponding angle α i, β i, γ iValue is brought equation into,
I i = cos α i cos β i cos γ i * I x - I xy - I xz - I yx I y - I yz - I zx - I zy I z * cos α i cos β i cos γ i
At I zUnder the known situation, simultaneous equations are tried to achieve other five variate-value: I x, I y, I Xy, I Xz, I Yz
And then, can obtain the ellipsoid of inertia equation of testee about barycenter.

Claims (4)

1. object product of inertia measurement mechanism is characterized in that, comprising:
First flat board of the unsettled placement of level, the first dull and stereotyped geometric shape is that circle or limit number are the regular polygon of 3N, N is the integer more than or equal to 1;
There is 1 through hole the first dull and stereotyped center, and the geometric shape that through hole is is that circle or limit number are the regular polygon of 2N, and N is the integer more than or equal to 2;
The turnover panel similar with the regular polygon via hole profile, turnover panel is used to hold testee;
At least 1 pair of pin joint in center of the center, 2 sides that is positioned at turnover panel symmetry and corresponding 2 sides of the first dull and stereotyped regular polygon through hole, said turnover panel can overturn with respect to first flat board respectively along the pin joint line at any angle;
Be positioned at the first dull and stereotyped outer rim place, equidistantly distribute, equal length and perpendicular to first dull and stereotyped 3 hoist cables;
The support that is connected with the hoist cable other end;
Be positioned at the pulling force sensor on the every hoist cable;
Be positioned at the small gap on first flat board;
Be positioned at the photoelectric sensor of opening position, under the static steady state (SS), said photoelectric sensor and support keep fixing position relation, and when first flat board along the center of circle minor rotation took place, the signal of photoelectric sensor changed;
The photosignal reading device links to each other with photoelectric signal sensor.
2. according to the said object product of inertia of claim 1 measurement mechanism, it is characterized in that said regular polygon through hole is a square, said turnover panel profile is a square.
3. according to the said object product of inertia of claim 1 measurement mechanism, it is characterized in that the said first dull and stereotyped geometric shape is equilateral triangle or regular hexagon, be positioned at the place, summit with the junction of hoist cable.
4. on any one said device of claim 1 to 3, realize object product of inertia measuring method; Definition: three ropes are respectively first rope, second rope, the 3rd rope; Its length is defined as L, and its corresponding pulling force sensor is respectively first pulling force sensor, second pulling force sensor, the 3rd pulling force sensor, on first flat board; Three ropes and the first dull and stereotyped node are defined as first node, second node, the 3rd node respectively; The first dull and stereotyped center is true origin O, and the horizontal range at the hoist cable node distance first dull and stereotyped center is defined as R, and the acceleration of gravity of measuring the place is defined as g; The cycle of rocking is T, and first flat board is I with the common moment of inertia of turnover panel Pi
Barycenter with testee is true origin O 1, be the Z axle perpendicular to the turnover panel direction, two other direction that is parallel to turnover panel is X axle and Y axle, sets up the rectangular coordinate system of testee;
It is characterized in that step comprises:
Step 1: the adjustment horizontal stand, guarantee to be in same surface level with the node of rope; Adjust first flat board, make it keep surface level, the adjustment turnover panel is to horizontal level; Testee is placed on the turnover panel, guarantee that the barycenter of testee and the first dull and stereotyped center are on the same perpendicular line; Give first dull and stereotyped small power, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read the torsional oscillation cycle T through photoelectric sensor 1At this moment, the reading of first, second, third pulling force sensor is respectively F 11, F 12, F 13First flat board is I with the common moment of inertia of turnover panel P1
Step 2: let testee at first around O 1Angle of Z axle rotation lets turnover panel along rotating a certain angle around pin joint then, lets testee translation in reprint, guarantees true origin O 1Be on the same perpendicular line with the first dull and stereotyped center, measure O this moment 1X axle, O 1Y axle, O 1The angle of Z axle and vertical direction 1, β 1, γ 1Give first dull and stereotyped small power then, make it with a low-angle torsional oscillation, said angle is greater than 0, and smaller or equal to 5 degree; Read the torsional oscillation cycle T through photoelectric sensor 2At this moment, the reading of first, second, third pulling force sensor is respectively F 21, F 22, F 23
Step 3: turnover panel recovers horizontal, and repeating step two records other at least four groups of different angle i, β i, γ i, read the torsional oscillation cycle T i, read the reading F of first, second, third pulling force sensor I1, F I2, F I3
Step 4: according to formula I Z = ( F 11 + F 12 + F 13 ) * R 2 * T 1 2 4 π 2 * L - I p 1 Calculate and obtain Iz, under other anglec of rotation, at first calculate and obtain first flat board and the common moment of inertia I of turnover panel Pi,
I iNumerical computation method following: I i = ( F i 1 + F i 2 + F i 3 ) * R 2 * T i 2 4 π 2 * L - I Pi
Then with I 2, I 3, I 4, I 5, I 6Numerical value and corresponding angle α i, β i, γ iValue is brought equation into,
I i = cos α i cos β i cos γ i * I x - I xy - I xz - I yx I y - I yz - I zx - I zy I z * cos α i cos β i cos γ i
At I zUnder the known situation, simultaneous equations are tried to achieve other five variate-value: I x, I y, I Xy, I Xz, I Yz
And then, can obtain the ellipsoid of inertia equation of testee about barycenter.
CN201110375927XA 2011-11-22 2011-11-22 Device and method for measuring inertia product of object Pending CN102494845A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201110375927XA CN102494845A (en) 2011-11-22 2011-11-22 Device and method for measuring inertia product of object

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201110375927XA CN102494845A (en) 2011-11-22 2011-11-22 Device and method for measuring inertia product of object

Publications (1)

Publication Number Publication Date
CN102494845A true CN102494845A (en) 2012-06-13

Family

ID=46186687

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201110375927XA Pending CN102494845A (en) 2011-11-22 2011-11-22 Device and method for measuring inertia product of object

Country Status (1)

Country Link
CN (1) CN102494845A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103487211A (en) * 2013-10-14 2014-01-01 北京航空航天大学 Method for measuring rotational inertia and inertia product of small-sized air vehicle
CN104680533A (en) * 2015-03-04 2015-06-03 福建师范大学 Organ positioning method based on sectional image reconstruction
CN108982012A (en) * 2018-09-25 2018-12-11 国网新疆电力有限公司电力科学研究院 Vertical pump dynamic balance running method based on virtual-sensor
CN111024308A (en) * 2019-12-19 2020-04-17 中国特种飞行器研究所 Method for measuring weight, gravity center and rotational inertia of ship model
CN111811733A (en) * 2020-07-01 2020-10-23 上海航天精密机械研究所 Universal device for measuring axial rotational inertia of eccentric revolving body
CN113624399A (en) * 2021-08-20 2021-11-09 哈尔滨工业大学 Object rotational inertia measuring method applied to large-space rope driving system

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1262318A1 (en) * 1984-02-27 1986-10-07 Предприятие П/Я В-2203 Device for determining inertia tensor
CN1546971A (en) * 2003-12-09 2004-11-17 西北工业大学 Measuring method and device for moment of inertia and product of inertia
KR20060124267A (en) * 2005-05-31 2006-12-05 재단법인서울대학교산학협력재단 The in-plane 3-axis inertia measurement systems with the exact alignment
CN101281075A (en) * 2008-05-28 2008-10-08 天津大学 Large-sized power plant mass inertia characteristic parameters measuring and taking synthetic experimental bench
CN201508270U (en) * 2009-09-25 2010-06-16 宁波拓普减震系统股份有限公司 Novel power assembly rotation inertia testing platform
CN201803831U (en) * 2010-08-25 2011-04-20 襄樊达安汽车检测中心 Device for measuring inertia moment parameters of automobile engine assembly
CN202329938U (en) * 2011-11-22 2012-07-11 天津大学 Object inertia product measuring device

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU1262318A1 (en) * 1984-02-27 1986-10-07 Предприятие П/Я В-2203 Device for determining inertia tensor
CN1546971A (en) * 2003-12-09 2004-11-17 西北工业大学 Measuring method and device for moment of inertia and product of inertia
KR20060124267A (en) * 2005-05-31 2006-12-05 재단법인서울대학교산학협력재단 The in-plane 3-axis inertia measurement systems with the exact alignment
CN101281075A (en) * 2008-05-28 2008-10-08 天津大学 Large-sized power plant mass inertia characteristic parameters measuring and taking synthetic experimental bench
CN201508270U (en) * 2009-09-25 2010-06-16 宁波拓普减震系统股份有限公司 Novel power assembly rotation inertia testing platform
CN201803831U (en) * 2010-08-25 2011-04-20 襄樊达安汽车检测中心 Device for measuring inertia moment parameters of automobile engine assembly
CN202329938U (en) * 2011-11-22 2012-07-11 天津大学 Object inertia product measuring device

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
张俊红,毕凤荣,胡春林,田新伟,张微: "动力设备质量惯性特性参数测取试验台研究", 《内燃机学报》, vol. 27, no. 1, 31 January 2009 (2009-01-31), pages 81 - 87 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103487211A (en) * 2013-10-14 2014-01-01 北京航空航天大学 Method for measuring rotational inertia and inertia product of small-sized air vehicle
CN103487211B (en) * 2013-10-14 2016-02-03 北京航空航天大学 A kind of method measuring small aircraft moment of inertia and the product of inertia
CN104680533A (en) * 2015-03-04 2015-06-03 福建师范大学 Organ positioning method based on sectional image reconstruction
CN108982012A (en) * 2018-09-25 2018-12-11 国网新疆电力有限公司电力科学研究院 Vertical pump dynamic balance running method based on virtual-sensor
CN111024308A (en) * 2019-12-19 2020-04-17 中国特种飞行器研究所 Method for measuring weight, gravity center and rotational inertia of ship model
CN111811733A (en) * 2020-07-01 2020-10-23 上海航天精密机械研究所 Universal device for measuring axial rotational inertia of eccentric revolving body
CN113624399A (en) * 2021-08-20 2021-11-09 哈尔滨工业大学 Object rotational inertia measuring method applied to large-space rope driving system

Similar Documents

Publication Publication Date Title
CN102494845A (en) Device and method for measuring inertia product of object
CN102507091B (en) Object mass center measuring device and method
CN105084213B (en) Mobile crane, moment limiting system of mobile crane and moment limiting method of mobile crane
CN102692206B (en) Device and method for measuring suspended deflection angle and direction of lifting hook of lifting device
CN101723239A (en) Hanging hook attitude detection device and crane
CN107091705A (en) Micro-thrust measuring method and device
CN102037341A (en) System and procedure for the real-time monitoring of fixed or mobile rigid structures such as building structures, aircraft, ships and/or the like
CN202329938U (en) Object inertia product measuring device
CN202736352U (en) Young modulus measuring instrument for experiment teaching
CN108573639B (en) Device capable of measuring inertial mass of object with arbitrary shape
CN202329937U (en) Object rotary inertia measurement device
CN102393277A (en) Measuring apparatus of rotational inertia of object and method thereof
CN202329939U (en) Device for measuring center of mass of object
CN105319082A (en) Historic building wooden pillar overturning deformation loading measurement device and loading measurement method thereof
CN205919940U (en) Be used for bridge model loading measuring device
CN205262866U (en) Take pulling force stabilising arrangement's young modulus apparatus
CN101832834B (en) Grasping rod force measuring device for climbing training under weightless environment
RU176241U1 (en) Device for calibrating tensometric scales
CN205209795U (en) Ancient building post topples and warp loading measuring device
CN213658220U (en) Microbalance calibrating device
CN101244790B (en) Mechanical weighing mechanism of gantry crane dynamic grab bucket electronic weighing scale
CN202648650U (en) Hook hanging deflection angle and position measuring device of hoisting device
RU2562445C2 (en) Test bench for measurement of stato-dynamic characteristics of physical objects
CN107796578B (en) The detection method of titanium alloy gyroplane frame strength
CN108151957B (en) Cable force dynamic tester calibration device and method

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20120613