CN201081704Y - Spatial inclination tester - Google Patents

Spatial inclination tester Download PDF

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Publication number
CN201081704Y
CN201081704Y CNU2007200842397U CN200720084239U CN201081704Y CN 201081704 Y CN201081704 Y CN 201081704Y CN U2007200842397 U CNU2007200842397 U CN U2007200842397U CN 200720084239 U CN200720084239 U CN 200720084239U CN 201081704 Y CN201081704 Y CN 201081704Y
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China
Prior art keywords
inclination angle
pointer
adjusting knob
utility
index dial
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Expired - Fee Related
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CNU2007200842397U
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Chinese (zh)
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孙闻笛
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Individual
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Individual
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Priority to CNU2007200842397U priority Critical patent/CN201081704Y/en
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Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a space inclination detector comprising a shell, wherein, the shell is fixed with a dial, the center of the dial is provided with an adjusting knob, a horizontal pointer and a luminous element are suspended below the adjusting knob, the adjusting knob, the horizontal pointer and the luminous element are connected through hanging lines. The utility model adopts the structure to project the horizontal pointer to the dial through rays produced by the luminous element, can measure the inclination angle and the inclination direction of the space inclination detector of the utility model according to the projection of the pointer on the dial; when the utility model is used to fix a measured object or is pressed against the measured object, the inclination angle and the inclination direction of the measured object can be measured. The utility model has a simple structure, convenient operation and low production cost, and can synchronously measure the inclination angle and the inclination direction through one-time reading (an inclination angle value and an inclination direction value marked on the dial).

Description

Space inclination angle detection instrument
Technical field
The utility model relates to a kind of space inclination angle detection instrument.
Background technology
In many engineerings field, for example building, highway, bridge, constructing tunnel, the installation of main equipment, pipeline, debugging, etc., not only need to measure the size at inclination angle, and need to measure vergence direction.
As shown in Figure 1, establish
Figure Y20072008423900031
Be the direction vector in the three dimensions, the direction in space of indicated object.Cross the A point and make AN perpendicular to plane X OY, N is for hanging down point, and then ∠ AON and ∠ YON are only has determined space vector
Figure Y20072008423900032
The inclination angle, and ∠ AON is called the inclination angle, ∠ YON is called vergence direction.
Space of the prior art inclination detecting device, as utilize the plumb aligner of gravity principle design can measure the inclination angle, but energy measurement vergence direction not are difficult to satisfy actual needs.Though existing gyroscope can be measured inclination angle and vergence direction simultaneously, its production cost height, working service complexity.
The utility model content
The utility model is exactly the space inclination angle detection instrument that a kind of simple in structure, easy to operate, low production cost is provided at the problem that above-mentioned prior art exists, and this space inclination angle detection instrument can be measured inclination angle and vergence direction simultaneously by single reading.
The technical scheme that the utility model provides is: space inclination angle detection instrument, comprise shell, be fixed with index dial on the shell, the index dial center is provided with adjusting knob, the adjusting knob below is hung with horizontal pointer and light-emitting component, and adjusting knob, horizontal pointer and light-emitting component connect by messenger wire.
Above-mentioned shell is rectangular parallelepiped or right cylinder etc.
Above-mentioned index dial is marked with a series of concentric circless, and circumference is marked with the angle value of expression vergence direction, and each concentric circles is marked with the angle value of expression inclination angle size.
Above-mentioned adjusting knob center, pointer center, light-emitting component center are on same pedal line.
The utility model adopts said structure, constitute vertical (if light-emitting component is lighter by adjusting knob, horizontal pointer and light-emitting component, can be at additional mass under the light-emitting component), the light that sends by light-emitting component projects to horizontal pointer on the index dial, according to the projection of pointer on index dial, can measure the inclination angle and the vergence direction of the utility model space inclination angle detection instrument, when the utility model is fixed or during near measurand, then can be measured the inclination angle and the vergence direction of measurand.The utility model is simple in structure, easy to operate, low production cost, by single reading (inclination angle of mark value and vergence direction value on the index dial), can measure inclination angle and vergence direction simultaneously.
Description of drawings
The presentation graphs at inclination angle, Fig. 1 space;
Fig. 2 is a structural representation of the present utility model;
Fig. 3 is the vertical view of Fig. 2;
Fig. 4 is the synoptic diagram that concerns between the shortest projected length and the inclination angle;
Fig. 5 is the perspective view of the utility model pointer on index dial when measuring 240 ° of 10 ° of vergence directions in inclination angle.
Embodiment
Referring to Fig. 2, Fig. 3, the utility model comprises rectangular parallelepiped (or right cylinder) shell 6, is fixed on the translucent index dial 1 on the shell, can be at the adjusting knob 9 of index dial 1 center rotation.Messenger wire 2 upper ends are fixed on the center of adjusting knob 9 and can rotate with adjusting knob 9, and simultaneously, messenger wire 2 can freely swing around the O point.Messenger wire 2 lower ends are passed and are fixed in the tubular shaft 4, and pointer 3 center fixation are on tubular shaft 4, and pointer 3 is vertical with tubular shaft 4.Messenger wire 2 lower ends are divided into four, and four messenger wires pass on the suspension ring 5 equally distributed four apertures respectively and are fixed on the suspension ring 5, and guarantee suspension ring 5 levels, and little electric torch 7 passes suspension ring 5 centers and is suspended on the suspension ring 5.
Index dial 1, adjusting knob 9, messenger wire 2, pointer 3, tubular shaft 4, suspension ring 5 and little electric torch 7 are formed a rotating and projection vertical, and wherein, pointer 3 remains horizontality, and rotation adjusting knob 9 can make pointer 3 rotate in surface level.The light that bulb 8 sends projects to pointer 3 on the index dial 1.When index dial 1 produced the space banking motion, the projection of pointer 3 on index dial 1 changed thereupon.Pointer 3 projections are by index dial 1 center dimidiation: projected length is short is called short projection.Rotation adjusting knob 9 makes pointer 3 short projected lengths the shortest, is called the shortest projection.
Index dial 1 is marked with a series of concentric circless, and circumference evenly is divided into some five equilibriums, and puts on angle value, is called vergence direction 11, and each concentric circles subscript upper angle value is called inclination angle 12.On the index dial 1 the direction of short projection equal the vergence direction of index dial 1.
On the index dial the length of short projection and the relation between the index dial inclination angle as shown in Figure 4, L wherein 1Be the fulcrum O of messenger wire distance, L to pointer 2Be the distance of pointer to bulb, 2r is the length of pointer, and α is the inclination angle.The shortest projection of pointer on index dial is divided into R and R ' two parts by index dial central point O, because long projection may exceed index dial, calculates (R is the shortest projection) so get R.Among Fig. 4, can get according to the sine in the trigonometric function:
R = ( L 1 + L 2 ) sin θ cos ( θ - α ) , θ = arctan r L 1 - - - ( 1 )
The inclination angle changes, and R changes thereupon, and when OE ⊥ AE, the R minimum is designated as R Min, this moment, corresponding inclination angle was designated as α MaxAs 0≤α≤α Max, α is corresponding one by one with R.In the interval [0, α Max] in evenly get some angles, be designated as 0 respectively, α 1, α 2... α Max, they are brought into (1) formula respectively, can obtain the shortest corresponding projected length, be designated as R respectively 0, R 1, R 2... R MaxRespectively with R 0, R 1, R 2... R MaxBe that radius draws concentric circles, and the inclination angle 12 of correspondence is marked on the circular arc, corresponding inclination angle of each concentric circles then, as shown in Figure 3 (0,10,30 etc.).
Plane with 240 ° of 10 ° of vergence directions in measurement inclination angle is an example, and rectangular parallelepiped of the present utility model (or right cylinder) bottom surface is placed in the plane, and pointer 3 remains horizontality, and the light that bulb 8 sends projects to pointer 3 on the index dial 1.Rotation adjusting knob 9 rotates pointer 3 in surface level, the projection of pointer 3 on index dial 1 changes thereupon.The shortest when pointer 3 short projected lengths, adjusting knob 9 promptly stops the rotation.Can read the inclination angle this moment according to the shortest projection indication of pointer on index dial is that 10 °, vergence direction are 240 ° (referring to Fig. 5).

Claims (5)

1. inclination angle detection instrument in space comprises shell, it is characterized in that: be fixed with index dial on the shell, the index dial center is provided with adjusting knob, and the adjusting knob below is hung with horizontal pointer and light-emitting component, and adjusting knob, horizontal pointer and light-emitting component connect by messenger wire.
2. space according to claim 1 inclination angle detection instrument is characterized in that: shell is a rectangular parallelepiped.
3. space according to claim 1 inclination angle detection instrument is characterized in that: shell is a right cylinder.
4. according to claim 1 or 2 or 3 described space inclination angle detection instrument, it is characterized in that: index dial is marked with a series of concentric circless, and circumference is marked with the angle value of expression vergence direction, and each concentric circles is marked with the angle value of expression inclination angle size.
5. according to claim 1 or 2 or 3 described space inclination angle detection instrument, it is characterized in that: adjusting knob center, pointer center and light-emitting component center are on same pedal line.
CNU2007200842397U 2007-04-18 2007-04-18 Spatial inclination tester Expired - Fee Related CN201081704Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CNU2007200842397U CN201081704Y (en) 2007-04-18 2007-04-18 Spatial inclination tester

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CNU2007200842397U CN201081704Y (en) 2007-04-18 2007-04-18 Spatial inclination tester

Publications (1)

Publication Number Publication Date
CN201081704Y true CN201081704Y (en) 2008-07-02

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CNU2007200842397U Expired - Fee Related CN201081704Y (en) 2007-04-18 2007-04-18 Spatial inclination tester

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Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102788571A (en) * 2011-05-19 2012-11-21 昆达电脑科技(昆山)有限公司 Gradient sensing device
CN104992592A (en) * 2015-07-22 2015-10-21 中国人民解放军镇江船艇学院 Gyroscope apparent motion demonstration device
CN108166970A (en) * 2016-12-06 2018-06-15 核工业北京地质研究院 A kind of drilling horizontal angle and vertical angle synchronous measuring apparatus and method

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102788571A (en) * 2011-05-19 2012-11-21 昆达电脑科技(昆山)有限公司 Gradient sensing device
CN102788571B (en) * 2011-05-19 2014-08-06 昆达电脑科技(昆山)有限公司 Gradient sensing device
CN104992592A (en) * 2015-07-22 2015-10-21 中国人民解放军镇江船艇学院 Gyroscope apparent motion demonstration device
CN104992592B (en) * 2015-07-22 2017-08-01 中国人民解放军镇江船艇学院 A kind of gyroscope apparent motion apparatus for demonstrating
CN108166970A (en) * 2016-12-06 2018-06-15 核工业北京地质研究院 A kind of drilling horizontal angle and vertical angle synchronous measuring apparatus and method
CN108166970B (en) * 2016-12-06 2023-11-14 核工业北京地质研究院 Synchronous measurement device and method for horizontal angle and vertical angle of drilling hole

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C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20080702

Termination date: 20100418