CN103682560A - Module mounting structure used in limited cylindrical space - Google Patents
Module mounting structure used in limited cylindrical space Download PDFInfo
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- CN103682560A CN103682560A CN201310714573.6A CN201310714573A CN103682560A CN 103682560 A CN103682560 A CN 103682560A CN 201310714573 A CN201310714573 A CN 201310714573A CN 103682560 A CN103682560 A CN 103682560A
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- module
- frame
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- cylindrical space
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Abstract
The invention relates to a module mounting structure used in a limited cylindrical space. The module mounting structure is characterized by comprising a cylindrical module frame, wherein the module frame is formed by connecting a left frame and a right frame which are symmetrical; the left frame and the right frame are respectively partitioned by an upper faceplate, an intermediate plate and a base plate; the upper surface of the upper faceplate is a mounting surface of a top end module; the lower surface of the base plate is a mounting surface of an antenna; a mounting cavity of a first module is arranged in a space between the upper faceplate and the intermediate plate of the left frame; a mounting cavity of a third module is arranged in a space between the intermediate plate and the base plate of the left frame; a mounting cavity of a second module is arranged in a space between the upper faceplate and the intermediate plate of the right frame; a mounting cavity of a fourth module is arranged in a space between the intermediate plate and the base plate of the right frame. With a mutually-embedded integral structure, the module mounting structure is good in environmental strength, the modules are convenient to disassemble, and the environmental requirements inside the limited cylindrical space are met.
Description
Technical field
The present invention relates to a kind of for the module installation structure in limited cylindrical space, in especially a kind of limited cylindrical space, the module installation structure of the eccentric angle speed of instantaneous acceleration that environmental requirement is 800g and 2m/s.
Background technology
In prior art, the cylindrical space on some equipment (as radar) has certain space environment demand and applied environment demand, need to carry out the structural design of miniaturization.In the limited cylindrical space of this class, the eccentric angle speed of the instantaneous acceleration that environmental requirement is 800g and 2m/s, structural requirement is higher; And as enclosure space, need the certain thermal diffusivity requirement of tool.
Summary of the invention
The object of the invention is to overcome the deficiencies in the prior art, provide a kind of for the module installation structure in limited cylindrical space, adopt inter-embedding type overall structure, environment intensity is good, and module easy accessibility meets the environmental requirement in limited cylindrical space.
According to technical scheme provided by the invention, a kind of for the module installation structure in limited cylindrical space, it is characterized in that: comprise columned module frame, module frame is formed by connecting by symmetrical left frame and correct frame, and left frame and correct frame are separated by top panel, intermediate plate and base plate respectively; The upper surface of described top panel is the installed surface of top module, the lower surface of base plate is the installed surface of antenna, the top panel of left frame and the space between intermediate plate are the installation cavity of the first module, the intermediate plate of left frame and the space between base plate are the installation cavity of the 3rd module, the top panel of correct frame and the space between intermediate plate are the installation cavity of the second module, the installation cavity that the intermediate plate of correct frame and the space between base plate are four module.
Flange platform and installing hole are set on described top panel, and top module is circular, and the breach matching with flange platform and the first bolt coordinating with installing hole are set in the module of top.
The left surface of described the first module and the 3rd module is arc surface, the connection plane of right flank for being connected with the flat side of left frame, and the left surface of the second module and four module is that the connection plane, the right flank that are connected with the flat side of correct frame are arc surface; On the flat side of described left frame, be provided with the first pin-and-hole and first and patch groove, on the flat side of correct frame, be provided with the second pin-and-hole and second and patch groove; In the connection plane of described the first module and the 3rd module, the first pin and the first connector are set, the first pin coordinates with the first pin-and-hole, and the first connector inserts first and patches in groove; In the connection plane of described the second module and four module, the second pin and the second connector are set, the second pin coordinates with the second pin-and-hole, and the second connector inserts second and patches in groove; Both sides, front and back in described the first module and the 3rd module arrange respectively the second bolt, and the first module is connected with left frame by the second bolt with the 3rd module.
Described antenna is circular, at the sidepiece of antenna, the 3rd bolt is set, and antenna is connected with module frame by the 3rd bolt.
The outside diameter of described module frame from top to bottom reduces successively, on plate, intermediate plate and base plate, lightening grooves is set respectively in the above.
On the flat side of described left frame, draw-in groove is set, on the flat side of correct frame, positioning convex strip is set, positioning convex strip coordinates with draw-in groove.
Center in described top module arranges through hole, and journal stirrup is set in through hole.
Of the present inventionly for the module installation structure in limited cylindrical space, can be used for environmental requirement in cylindrical space and be: the situation of the eccentric angle speed of the instantaneous acceleration of 800g and 2m/s; The present invention adopts the overall construction design of inter-embedding type, and environment intensity is good, and module easy accessibility is convenient to independent dismounting and is detected replacing, can be applicable to series of similar components, and can be Related product provides structure to use for reference simultaneously.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is the structural representation of module frame of the present invention.
Fig. 3 is the structural representation of left frame of the present invention.
Fig. 4 is the schematic side view of left frame of the present invention.
Fig. 5 is the structural representation of correct frame of the present invention.
Fig. 6 is the end view of correct frame of the present invention.
Fig. 7 is the structural representation of described top module.
Fig. 8 is the vertical view of Fig. 7.
Fig. 9 is the structural representation of described the first module and the 3rd module.
Figure 10 is the right view of Fig. 9.
Figure 11 is the structural representation of described the second module and four module.
Figure 12 is the left view of Figure 11.
Figure 13 is the structural representation of described antenna.
Figure 14 is the vertical view of Figure 13.
Embodiment
Below in conjunction with concrete accompanying drawing, the invention will be further described.
As shown in Fig. 1～Figure 14: as described in for the module installation structure in limited cylindrical space, comprise top module 1, breach 1-1, the first bolt 1-2, through hole 1-3, journal stirrup 1-4, left frame 2, draw-in groove 2-1, the first pin-and-hole 2-2, first patches groove 2-3, correct frame 3, positioning convex strip 3-1, the second pin-and-hole 3-2, second patches groove 3-3, the first module 4, the second module 5, the 3rd module 6, four module 7, antenna 8, flange platform 9, installing hole 10, the first pin 11, the first connector 12, the second pin 13, the second connector 14, the second bolt 15, the 3rd bolt 16 etc.
As shown in Figure 1 and Figure 2, the present invention includes columned module frame, module frame is formed by connecting by symmetrical left frame 2 and correct frame 3; As shown in Figure 3, Figure 4, on the flat side of described left frame 2, draw-in groove 2-1 is set, on the flat side of correct frame 3, positioning convex strip 3-1 is set, positioning convex strip 3-1 coordinates with draw-in groove 2-1;
As shown in Figure 2 to 4, described left frame 2 and correct frame 3 are separated by top panel, intermediate plate and base plate respectively; As shown in Fig. 2, Fig. 7, Fig. 8, the upper surface of described top panel is the installed surface of top module 1, flange platform 9 and installing hole 10 are set on plate in the above, and top module 1 is circular, and the breach 1-1 matching with flange platform 9 and the first bolt 1-2 coordinating with installing hole 10 are set in top module 1; Described top module 1 is installed and is connected with breach 1-1 by flange platform 9, makes the moment of torsion of top module 1 directly act on module frame, can not make top module 1 be subject to the annular shear stress that moment of torsion produces, and reduces unnecessary risk; As shown in Figure 8, at the center of described top module 1, through hole 1-3 is set, journal stirrup 1-4 is set in through hole 1-3, journal stirrup 1-4 is used for placing connector;
As shown in Figure 1 and Figure 2, the top panel of described left frame 2 and the space between intermediate plate are the installation cavity of the first module 4, the intermediate plate of left frame 2 and the space between base plate are the installation cavity of the 3rd module 6, the top panel of correct frame 3 and the space between intermediate plate are the installation cavity of the second module 5, the installation cavity that the intermediate plate of correct frame 3 and the space between base plate are four module 7; As shown in Fig. 9～Figure 12, the left surface of described the first module 4 and the 3rd module 6 is arc surface, the connection plane of right flank for being connected with the flat side of left frame 2, and the left surface of the second module 5 and four module 7 is that the connection plane, the right flank that are connected with the flat side of correct frame 3 are arc surface; As shown in Fig. 2, Fig. 3, Fig. 5, on the flat side of described left frame 2, be provided with the first pin-and-hole 2-2 and first and patch groove 2-3, on the flat side of correct frame 3, be provided with the second pin-and-hole 3-2 and second and patch groove 3-3; As shown in Fig. 9～Figure 12, the first pin 11 is set in the connection plane of described the first module 4 and the 3rd module 6 and the first connector 12, the first pins 11 coordinate with the first pin-and-hole 2-2, the first connector 12 inserts first and patches in groove 2-3; The second pin 13 is set in the connection plane of described the second module 5 and four module 7 and the second connector 14, the second pins 13 coordinate with the second pin-and-hole 3-2, the second connector 14 inserts second and patches in groove 3-3; The second bolt 15, the first modules 3 are set respectively in the both sides, front and back of described the first module 3 and the 3rd module 6 to be connected with left frame 2 by the second bolt 15 with the 3rd module 6;
As shown in Figure 1 and Figure 2, the lower surface of the base plate of described module frame is the installed surface of antenna 8; As shown in Figure 13, Figure 14, described antenna 8 is circular, at the sidepiece of antenna 8, the 3rd bolt 16 is set, and antenna 8 is connected with module frame by the 3rd bolt 16;
As shown in Figure 2, the outside diameter of described module frame from top to bottom reduces successively, on plate, intermediate plate and base plate, lightening grooves is set respectively in the above, is guaranteeing to carry out loss of weight under some strength condition, and effectively heat loss through conduction, reduces the alluvial of module amount of localized heat.
Of the present invention for the module installation structure in limited cylindrical space can the condition for the instantaneous acceleration of environmental requirement: 800g and the eccentric angle speed of 2m/s under, and the certain thermal diffusivity of tool.
Claims (7)
1. one kind for the module installation structure in limited cylindrical space, it is characterized in that: comprise columned module frame, module frame is formed by connecting by symmetrical left frame (2) and correct frame (3), and left frame (2) and correct frame (3) are separated by top panel, intermediate plate and base plate respectively; The upper surface of described top panel is the installed surface of top module (1), the lower surface of base plate is the installed surface of antenna (8), the top panel of left frame (2) and the space between intermediate plate are the installation cavity of the first module (4), the intermediate plate of left frame (2) and the space between base plate are the installation cavity of the 3rd module (6), the top panel of correct frame (3) and the space between intermediate plate are the installation cavity of the second module (5), and the intermediate plate of correct frame (3) and the space between base plate are the installation cavity of four module (7).
2. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: flange platform (9) and installing hole (10) are set on described top panel, top module (1) is circular, at the upper breach (1-1) matching with flange platform (9) and the first bolt (1-2) coordinating with installing hole (10) of arranging of top module (1).
3. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: the left surface of described the first module (4) and the 3rd module (6) is arc surface, the connection plane of right flank for being connected with the flat side of left frame (2), and the left surface of the second module (5) and four module (7) is that the connection plane, the right flank that are connected with the flat side of correct frame (3) are arc surface; On the flat side of described left frame (2), be provided with the first pin-and-hole (2-2) and first and patch groove (2-3), on the flat side of correct frame (3), be provided with the second pin-and-hole (3-2) and second and patch groove (3-3); The first pin (11) and the first connector (12) are set in the connection plane of described the first module (4) and the 3rd module (6), the first pin (11) coordinates with the first pin-and-hole (2-2), and the first connector (12) inserts first and patches in groove (2-3); The second pin (13) and the second connector (14) are set in the connection plane of described the second module (5) and four module (7), the second pin (13) coordinates with the second pin-and-hole (3-2), and the second connector (14) inserts second and patches in groove (3-3); Both sides, front and back in described the first module (3) and the 3rd module (6) arrange respectively the second bolt (15), and the first module (3) is connected with left frame (2) by the second bolt (15) with the 3rd module (6).
4. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: described antenna (8) is for circular, sidepiece at antenna (8) arranges the 3rd bolt (16), and antenna (8) is connected with module frame by the 3rd bolt (16).
5. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: the outside diameter of described module frame from top to bottom reduces successively, on plate, intermediate plate and base plate, lightening grooves is set respectively in the above.
6. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: draw-in groove (2-1) is set on the flat side of described left frame (2), positioning convex strip (3-1) is set on the flat side of correct frame (3), and positioning convex strip (3-1) coordinates with draw-in groove (2-1).
7. as claimed in claim 1 for the module installation structure in limited cylindrical space, it is characterized in that: at the center of described top module (1), through hole (1-3) is set, journal stirrup (1-4) is set in through hole (1-3).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310714573.6A CN103682560B (en) | 2013-12-20 | 2013-12-20 | For the module installation structure in limited cylindrical space |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310714573.6A CN103682560B (en) | 2013-12-20 | 2013-12-20 | For the module installation structure in limited cylindrical space |
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| CN103682560A true CN103682560A (en) | 2014-03-26 |
| CN103682560B CN103682560B (en) | 2016-05-18 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN201310714573.6A Active CN103682560B (en) | 2013-12-20 | 2013-12-20 | For the module installation structure in limited cylindrical space |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625883A (en) * | 2018-12-18 | 2019-04-16 | 科捷智能装备有限公司 | Balance wheel modularization sorter and its manufacturing method |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5519407A (en) * | 1994-10-07 | 1996-05-21 | The United States Of America As Represented By The Secretary Of The Navy | Circularly polarized dual frequency lightweight deployable antenna system |
| US20030052828A1 (en) * | 2001-09-12 | 2003-03-20 | Metawave Communications Corporation | Co-located antenna array for passive beam forming |
| CN203733924U (en) * | 2013-12-20 | 2014-07-23 | 北方通用电子集团有限公司 | Module installation structure used for limited cylindrical space |
-
2013
- 2013-12-20 CN CN201310714573.6A patent/CN103682560B/en active Active
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5519407A (en) * | 1994-10-07 | 1996-05-21 | The United States Of America As Represented By The Secretary Of The Navy | Circularly polarized dual frequency lightweight deployable antenna system |
| US20030052828A1 (en) * | 2001-09-12 | 2003-03-20 | Metawave Communications Corporation | Co-located antenna array for passive beam forming |
| CN203733924U (en) * | 2013-12-20 | 2014-07-23 | 北方通用电子集团有限公司 | Module installation structure used for limited cylindrical space |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109625883A (en) * | 2018-12-18 | 2019-04-16 | 科捷智能装备有限公司 | Balance wheel modularization sorter and its manufacturing method |
| CN109625883B (en) * | 2018-12-18 | 2023-07-18 | 科捷智能科技股份有限公司 | Balance wheel modularized sorting machine and manufacturing method thereof |
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| Publication number | Publication date |
|---|---|
| CN103682560B (en) | 2016-05-18 |
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