CN202083405U - Multisection bearing universal balance compass mechanism - Google Patents

Multisection bearing universal balance compass mechanism Download PDF

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Publication number
CN202083405U
CN202083405U CN201020695201.5U CN201020695201U CN202083405U CN 202083405 U CN202083405 U CN 202083405U CN 201020695201 U CN201020695201 U CN 201020695201U CN 202083405 U CN202083405 U CN 202083405U
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China
Prior art keywords
compass
axis
piece
frame
articulated elements
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Expired - Lifetime
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CN201020695201.5U
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Chinese (zh)
Inventor
陈征峰
杨晟飞
张振华
张�荣
王璨
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704th Research Institute of CSIC
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704th Research Institute of CSIC
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Priority to CN201020695201.5U priority Critical patent/CN202083405U/en
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Abstract

A multisection bearing universal balance compass mechanism mainly solves the technical problems of improving the adjusting ability of the freedom degree of the mechanism, and the like. The mechanism employs the technical scheme of comprising an upper compass rack, a fork-shaped piece, a rod-shaped piece, and a lower compass rack, wherein the upper compass rack is in hinged connection with one end of the fork-shaped piece via the first hinged connection piece of a hinged connection assembly, the other end of the fork-shaped piece is in hinged connection with one end of the rod-shaped piece via the second hinged connection piece of the hinged connection assembly, the other end of the rod-shaped piece is in hinged connection with the lower compass rack via the third hinged connection piece of the hinged connection assembly, and the axis of the first hinged connection piece and the axis of the second hinged connection piece are vertical. The self-balance mechanism is suitable for hanging a plurality of components having a requirement on verticality.

Description

The universal balance compass of more piece bearing mechanism
Technical field:
The utility model relates to the self-adjusting mechanism of a kind of verticality, particularly a kind of mechanism of vertical hanging sophisticated sensor.
Background technology:
Existing typical compass mechanism is two joint adjustment structures, the sensor that is usually used in the vertical hanging precision, or be used for the vertical hanging parts the strict vertical occasion that requires need be arranged, typical case's compass mechanism as shown in Figure 9, this mechanism includes outer shroud 91, outer coupling shaft 92, compositions such as interior ring 93 and interior coupling shaft 94, wherein outer shroud 91 can rotate around being arranged on the outer coupling shaft 92 that compass puts on the shelf, but the interior coupling shaft 94 that 93 windings of interior ring are put at outer shroud 91 rotates, thereby the parts (as sensor etc.) that need to keep accurate verticality in guaranteeing to be installed on the ring 93 can be done 360 ° around the center line of structure and rotate freely motion, when the external structure part tilts, need to keep the parts of accurate verticality can automatically restore to plumbness, mechanism is used for vector sensor as compass, the direction of measurement that can make vector sensor all the time vertically downward, above-mentioned typical compass mechanism is in order to guarantee the verticality of installing component, in the requirement, the outer shroud process and assemble need have higher symmetry, require each member dead weight in the mechanism little simultaneously, each coupling shaft not only size is little, the friction of its supporting also should be as far as possible little, but still there is following point in existing typical compass mechanism:
1. existing typical compass mechanism is 2 joint adjustment structures (being outer shroud 91 and interior ring 93), and it is relatively poor that it regulates degree of freedom, and when the structure degree of tilt was big, compass mechanism was owing to the restriction of self structure loses the verticality regulating power, or appearance " stuck " phenomenon;
2. sliding bearing is all adopted in the supporting of the inside and outside coupling shaft 92,94 of existing typical compass mechanism, its sliding friction damping is bigger, influence the verticality regulatory function of mechanism, it is big simultaneously respectively to support span, the symmetry difficulty that realizes himself structure is bigger, and its symmetric difference bring big negative effect can further for mechanism's verticality regulating effect.
3. after using for a long time in the mechanism, or after using under the environment of vibration, its yielding structure and its sliding bearing easy to wear, its self-poise performance descends, cause the mounted component verticality can not satisfy the requirement of regulation, thereby need mechanism is carried out regular maintenance or changes member, serviceable life is short, the use cost height;
4. existing compass mechanism resistance to shock is poor, because essential glade plane space between each supporting surface of contact causes the instability in the structure use.
The utility model content:
Technical problem to be solved in the utility model provides the universal balance compass of a kind of more piece bearing mechanism, and it can have strong degree of freedom regulating power for mechanism, and can improve the verticality regulating effect, and structural stability is strong, and maintainability is good, long service life.
The technical scheme in the invention for solving the above technical problem is:
The universal balance compass of more piece bearing mechanism, the upper end of this mechanism is connected with structural member, the lower end of this mechanism is connected with the parts of strict demand are vertically arranged, be characterized in: described compass mechanism has compass frame on, should go up the compass frame is hinged with Y-piece through first articulated elements of hinge assembly a end, the other end of this Y-piece is hinged with rod like parts one end through second articulated elements of hinge assembly, the other end of this rod like parts is hinged with down the compass frame through the 3rd articulated elements of hinge assembly, the first articulated elements axis of described hinge assembly is vertical mutually with the second articulated elements axis, its second articulated elements axis is vertical mutually with the 3rd articulated elements axis, constitutes the universal balanced structure of more piece bearing.
The utility model adopts the more piece adjustment structure, compare with tradition 2 joint adjustment structures, the adjusting degree of freedom is better, can eliminate mechanism's " stuck " phenomenon, the utility model adopts hinge assembly to be rolling bearing, frictional damping is little, its upper and lower compass frame, Y-piece and rod supporting span is little and symmetry good, can further improve the verticality regulating effect of mechanism, simultaneously because hinged each member wearing and tearing are little, the rigidity of structure is big, can prolong mechanism serviceable life, reduce mechanism's use cost, and can improve the antivibration ability and the stability of mechanism.
Description of drawings:
Fig. 1 is the universal balance compass of the utility model more piece bearing master of a mechanism cross-sectional schematic.
Fig. 2 is that the Y-piece master looks synoptic diagram among Fig. 1.
Fig. 3 is that the A of Fig. 2 is to synoptic diagram.
Fig. 4 is the cross-sectional schematic of Fig. 2.
Fig. 5 is Fig. 3 partial schematic sectional view.
Fig. 6 is that the hinge assembly vertical profile is looked synoptic diagram among Fig. 1.
Fig. 7 is a rod like parts synoptic diagram among Fig. 1.
Fig. 8 be among Fig. 7 B to view.
Fig. 9 is traditional compass structural scheme of mechanism.
Embodiment:
With reference to Fig. 1, the universal balance compass of more piece bearing mechanism includes compass frame 1, Y-piece 2, hinge assembly 3, rod like parts 4 and following compass frame 5, is illustrated as the compass mechanism of 3 joint adjustment structures.
Last compass frame 1, has a circle, the tabular upper frame 11 of rectangle or other analogous shapes, can offer some through holes on this upper frame 11, to go up compass frame 11 in order to the bolt that stretches through is installed on hull structural member or other similar components, two upper lug 12 have been protruded out in the bottom surface of this upper frame 11, upper frame 11 and upper lug 12 can cast make or weld one-body molded, two upper lug 12 of symmetry have the upper shaft hole 13 of two coaxial cables, this upper shaft hole 13 can be installed the left side of hinge assembly 3, right axle 31,34, two upper lug 12 have screw 14 on two respectively, this on two screw 14 axis normal can revolve in the last screw 14 and establish a fixing left side in upper shaft hole 13 axis, right axle 31,34 screw.
Y-piece 2, shown in Fig. 2,3,4,5, Y-piece 2 include straight end 21 and forked end 24 one-body molded, should directly hold 21 outlines curved, directly hold 21 both sides to offer dead eye 22 at this with rotational symmetry, this dead eye 22 is connected with through hole 23 in order to 22 of left and right rolling bearing 32,33, two dead eyes that hinge assembly 3 is installed; This forked end 24 offers axis hole 25 in the fork-shaped both sides with rotational symmetry, this axis hole 25 is in order to install the left and right axle 31,34 of hinge assembly 3, two axis holes 25 vertically to having screw 26 respectively, can revolve the screw of establishing fixing left and right axle 31,34 in this screw 26, the axis of above-mentioned two dead eyes 22 and two axis holes 25 is vertical mutually;
Y-piece 2, the quantity that is exemplified as the used Y-piece 2 of 3 joint adjustment structures at Fig. 1 is 1, when compass mechanism need increase the adjusting degree of freedom, under installing space enabled condition, can adopt more piece to transfer structure, be 2 o'clock as the quantity of Y-piece 2 in mechanism, then can form 4 joint adjustment structures, and for example the quantity of Y-piece 2 is 3 o'clock, then can form 5 joint adjustment structures or the like.
Hinge assembly 3, include left side axle 31, the dynamic bearing 32 that rolls left, right rolling bearing 33 and right axle 34, as shown in Figure 6, the quantity of hinge assembly 3 is exactly the joint number of the adjustment structure of the universal balance compass of more piece bearing mechanism in the utility model, represent promptly that as typical 3 joint adjustment structures this mechanism has 3 hinge assemblies 3, and the like, for setting forth conveniently, the hinge assembly 3 of 3 different installation sites is denoted as first, second, third articulated elements 31,32,33 respectively in Fig. 1, and three's 26S Proteasome Structure and Function is identical; Wherein:
Left side axle 31, be two-stage structure as shown in Figure 6, the principal piece size can be installed on the upper shaft hole 13 of compass frame 1, the axis hole 25 of Y-piece 2 and the lower shaft hole 53 of following compass frame 5 more greatly respectively, and with screw retention, keep left side axle 31 that bigger rigidity is arranged, left side axle 31 has extended a location convex shoulder and a shaft extension at principal piece one end, the less inner ring that cooperates rolling bearing in order to the location of this shaft extension size;
Dynamic bearing 32 rolls left, the utility model adopts rolling bearing structure, can obviously reduce the motion of mechanism damping, the bearing wear of reducing mechanism, improve maintainability, prolonging mechanism serviceable life, improve structure stability in use, is one of important technique measure that improves compass mechanism verticality regulatory function;
The 26S Proteasome Structure and Function of right rolling bearing 33 is identical with the dynamic bearing 32 that rolls left;
The 26S Proteasome Structure and Function of right axle 34 is identical with left side axle 31, and the position that is the minute surface symmetry is installed in 31 described each axis hole of a left side;
Promptly this left and right axle 31,34 is installed in the upper and lower axis hole 13,53 of upper and lower compass frame 1,5 and the axis hole 25 of Y-piece 2 respectively, and the location is combined with the inner ring of left and right rolling bearing 32,33 on the shaft extension of this left and right axle 31,34;
The left side of hinge assembly 3, right axle 31,34, a left side, right rolling bearing 32,33 and after corresponding each corresponding axis hole and dead eye install, form the axis 35 of a common hinge assembly 3, in compass mechanism, the axis 35 of the hinge assembly 3 of variant installation is vertical mutually, is example (as Fig. 1) as the utility model with 3 joint governor motions, the axis 35 of first articulated elements 31 of described hinge assembly 3 is vertical mutually with the axis of second articulated elements 32 35, the axis 35 of its second articulated elements 32 is vertical mutually with the axis of the 3rd articulated elements 35, when compass mechanism is the more piece adjustment structure, the axis 35 of each hinge assembly 3 is all vertical mutually by above-mentioned arrangement, thereby form the function of better governor motion degree of freedom, the quantity of corresponding hinge assembly 3 is 3 to 5.
Rod like parts 4, it is a rectangle body of rod, its two ends and each corresponding axis hole are circular arc, the xsect of this body of rod can be square, the both sides of the upper end 41 of rod like parts offer the dead eye 22 of coaxial cable, dead eye 22 structures of this dead eye 22 and Y-piece 2, function are all identical, so use same numbering, two dead eyes 22 can be located the outer ring of the left and right rolling bearing 32,33 of coordination hinge assembly 3 respectively; The both sides of the lower end 42 of rod like parts offer the dead eye 22 of coaxial cable, and function is identical with above-mentioned two dead eyes 22; Upper end 41 2 dead eyes, 22 axis are vertical mutually with the axis of lower end 42 2 dead eyes 22; When the last compass frame 1 of compass mechanism or when compass frame 5 adopts single ledge arrangement down, can not adopt rod like parts 4 in this mechanism.
Following compass frame 5, has a circle, the tabular lower frame 51 of rectangle or other analogous shapes, can offer some through holes or screw on this lower frame 51, to keep the parts of accurate verticality to be installed in down on the compass frame 5 in order to wear bolt, end face at this lower frame 51 has protruded out lug 52 two times, lower frame 51 is with following lug 52 system of can casting or weld one-body molded, two times lugs 52 of symmetry have the lower shaft hole 53 of two coaxial cables, this lower shaft hole 53 can be installed the left side of hinge assembly 3, right axle 31,34, two times lug 52 has screw 54 respectively two times, these two times screw 54 axis normal can be revolved in the following screw 54 and establish a fixing left side in lower shaft hole 53 axis, right axle 31,34 screw.
The utility model is applicable to the occasion that vertical hanging parts verticality is had strict demand, have the sensor of tubular shell, portable surveying instrument, laser generator or other similar accurate devices or the like under water as suspension, the utility model all can be regulated its verticality automatically and can obtain good result.
The universal balance compass of more piece bearing mechanism, also can one the 3rd ring be set again at the inner ring that existing structure (as Fig. 9) is gone up at interior ring 93, the 3rd ring is hinged by the 3rd coupling shaft of ring 93 in being arranged on, thereby forms the universal balance compass of a more piece bearing mechanism with 3 joint adjustment structures (interior ring, outer shroud, the 3rd ring).

Claims (7)

1. the universal balance compass of more piece bearing mechanism, the upper end of this mechanism is connected with structural member, it is characterized in that: described compass mechanism has compass frame (1) on, should go up compass frame (1) is hinged with Y-piece (2) through first articulated elements (31) of hinge assembly (3) a end, the other end of this Y-piece (2) is hinged with rod like parts (4) one ends through second articulated elements (32) of hinge assembly (3), the other end (42) of this rod like parts (4) is hinged with down compass frame (5) through the 3rd articulated elements (31) of articulated elements assembly (3), first articulated elements (31) axis of described hinge assembly (3) is vertical mutually with second articulated elements (32) axis, its second articulated elements (32) axis is vertical mutually with the 3rd articulated elements axis, constitutes the universal balanced structure of more piece bearing.
2. the universal balance compass of more piece bearing according to claim 1 mechanism, upper frame (11) projection downwards that it is characterized in that compass frame (1) has symmetrical two upper lug (12), this two upper lug (12) has the upper shaft hole (13) of coaxial cable respectively, two upper lug (12) have screw on two (14) respectively, this on two screw (14) axis normal in upper shaft hole (13) axis.
3. the universal balance compass of more piece bearing according to claim 1 mechanism, the straight end (21) and the forked end (24) that it is characterized in that Y-piece (2) are one-body molded, should offer dead eye (22) with rotational symmetry in straight end (24) both sides, this forked end (24) both sides offer axis hole (25) with rotational symmetry, two axis holes (25) vertically to having screw (26) respectively, dead eye (22) is vertical mutually with the axis of axis hole (25).
4. the universal balance compass of more piece bearing according to claim 1 mechanism, it is characterized in that described hinge assembly (3) includes left side axle (31), dynamic bearing (32) rolls left, right rolling bearing (33) and right axle (34), this left side, right axle (31,34) be installed in respectively, following compass frame (1,5) on, lower shaft hole (13,53) and the axis hole (25) of Y-piece (2), this left side, right axle (31,34) location is combined with a left side on the shaft extension, right rolling bearing (32,33) inner ring, this left side, right rolling bearing (32,33) location, outer ring is combined with the dead eye (22) of Y-piece (2) and rod like parts (4), left side axle (31), dynamic bearing (32) rolls left, right rolling bearing (33) and right axle (34) have an axis (35).
5. the universal balance compass of more piece bearing according to claim 1 mechanism, it is characterized in that the both sides of the upper and lower end (41,42) of described rod like parts (4) offer the dead eye (22) of coaxial cable respectively, upper end (41) two dead eye (22) axis are vertical mutually with the axis of lower end (42) two dead eyes (22).
6. the universal balance compass of more piece bearing according to claim 1 mechanism, the lower frame (51) that it is characterized in that following compass frame (5) upwards projection has two times lugs (52) of symmetry, these two times lugs (5) have the lower shaft hole (53) of coaxial cable respectively, two times lugs (52) have two times screws (54) respectively, and this two times screws (54) axis normal is in the axis of lower shaft hole (53).
7. the universal balance compass of more piece bearing according to claim 1 mechanism, the quantity that it is characterized in that the Y-piece (2) of this mechanism is 1 to 3, the quantity of corresponding hinge assembly (3) is 3 to 5.
CN201020695201.5U 2010-12-28 2010-12-28 Multisection bearing universal balance compass mechanism Expired - Lifetime CN202083405U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201020695201.5U CN202083405U (en) 2010-12-28 2010-12-28 Multisection bearing universal balance compass mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201020695201.5U CN202083405U (en) 2010-12-28 2010-12-28 Multisection bearing universal balance compass mechanism

Publications (1)

Publication Number Publication Date
CN202083405U true CN202083405U (en) 2011-12-21

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Application Number Title Priority Date Filing Date
CN201020695201.5U Expired - Lifetime CN202083405U (en) 2010-12-28 2010-12-28 Multisection bearing universal balance compass mechanism

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102455194A (en) * 2010-12-28 2012-05-16 中国船舶重工集团公司第七〇四研究所 Multisection bearing universal balance compass mechanism

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN102455194A (en) * 2010-12-28 2012-05-16 中国船舶重工集团公司第七〇四研究所 Multisection bearing universal balance compass mechanism

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AV01 Patent right actively abandoned
AV01 Patent right actively abandoned
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Granted publication date: 20111221

Effective date of abandoning: 20140312

AV01 Patent right actively abandoned

Granted publication date: 20111221

Effective date of abandoning: 20140312