CN204652817U - A kind of customizable satellite magnetic component control line road box - Google Patents
A kind of customizable satellite magnetic component control line road box Download PDFInfo
- Publication number
- CN204652817U CN204652817U CN201520343049.7U CN201520343049U CN204652817U CN 204652817 U CN204652817 U CN 204652817U CN 201520343049 U CN201520343049 U CN 201520343049U CN 204652817 U CN204652817 U CN 204652817U
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- circuit box
- body frame
- backboard
- front panel
- control circuit
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Abstract
The utility model discloses a kind of customizable satellite magnetic component control line road box, relate to space industry.The body structure that described circuit box is assemblied to form by front panel, rear board, left plate, right plate, upper cover and base; In body structure, install back of the body frame, back of the body frame is parallel to front panel and is arranged on upper cover and base near front panel; Back of the body frame connects and is parallel to the backboard of front panel, on backboard, vertical welding connects connector seat, arranges guide groove respectively being on the described left plate inwall of same horizontal plane and described right plate inwall with connector seat; On be covered with through hole, mounting socket on through hole; Described socket is connected with described backplane communication.The utility model circuit box is the customizable circuit box of size, meets satellite application environment to aspect requirements such as circuit box structural strength, thermal characteristicss, reduces circuit box weight and size to greatest extent.
Description
Technical field
The utility model relates to space industry, particularly relates to a kind of customizable satellite magnetic component control line road box.
Background technology
Satellite magnetic component control line road for the treatment of and export the three-axle magnetic field signal that magnetometer probe acquires arrives, as the authentic data of its attitude of Satellite observation, control command can be received simultaneously and drive magnetic torquer work to reach the object exporting corresponding magnetic moment.Magnetic component control line road box is for installing magnetic assembly process circuit, ensure space environment protective when mechanical when process circuit has a transmitting and heaven flight, comprise electrostatic defending, Flouride-resistani acid phesphatase protection etc., make magnetic assembly process circuit meet ground test transport, requirement of launching and fly in-orbit, therefore satellite magnetic component control line road meet ground test transport, launch and in-orbit fly requirement there is important function.But the existing satellite magnetic component control line road box for satellite attitude measurement and control is fixed dimension, there is the deficiency that weight is large, size large and application is inconvenient.
Utility model content
The purpose of this utility model is to provide a kind of customizable satellite magnetic component control line road box, thus solves the foregoing problems existed in prior art.
To achieve these goals, customizable satellite magnetic component control line road described in the utility model box, the body structure that described circuit box is assemblied to form by front panel, rear board, left plate, right plate, upper cover and base, the connection between any two panels all removably connects;
Described circuit box also comprises the back of the body frame be arranged in described body structure, and described back of the body frame is parallel to described front panel, and is arranged on described upper cover and described base near described front panel;
Described circuit box also comprises backboard, described backboard is arranged on the side that described back of the body frame deviates from described front panel, on described backboard, vertical welding connects connector seat, arranges guide groove respectively being on the described left plate inwall of same horizontal plane and described right plate inwall with described connector seat;
Be covered with through hole on described, described through hole is installed the socket mated with described through hole, and the number of described through hole is identical with the number of described socket, and is no less than 1; Described socket is connected with described backplane communication.
Preferably, removably connect described in and comprise screw connection.
Preferably, described back of the body frame upper stupefied is connected by screw that described upper cover is upper and lower is stupefiedly connected by screw described base.
Preferably, on the left stupefied and right side of described back of the body frame is stupefied, be symmetrical arranged interface relative to the vertical center line of described back of the body frame, described backboard is connected by screw on the interface of described back of the body frame.
Preferably, described connector seat is arranged on the side that described backboard deviates from described back of the body frame.
Preferably, circuit board is inserted in described circuit box by the guide groove on described left plate, described right plate inwall, with the connector seat socket connection on described backboard.
Preferably, the minor axis center line of all described through holes overlaps, centered by line P, and described center line P is parallel with the long axis centerline M of described upper cover, and described center line P and described back of the body frame vertical range are greater than described center line M and described back of the body frame vertical range.
Preferably, described connector seat is identical with needing the quantity of the circuit board be installed in described circuit box.
Preferably, the base outer wall of described circuit box is also provided with fixing feet interface.
Preferably, described socket be screwed be connected to described on cover.
The beneficial effects of the utility model are:
Satellite magnetic component control line road described in the utility model box is according to the concrete size custom fabricated of magnetometer control circuit board and magnetic torquer control circuit board, meet satellite application environment to aspect requirements such as circuit box structural strength, thermal characteristicss, reduce circuit box weight and size to greatest extent.
Accompanying drawing explanation
Fig. 1 is the front view cross-sectional schematic of customizable satellite magnetic component control line road box;
Fig. 2 is that schematic diagram is looked on a left side for customizable satellite magnetic component control line road box;
Fig. 3 is the schematic top plan view of customizable satellite magnetic component control line road box;
Wherein, 1 represents front panel, and 2 represent rear board, and 3 represent left plate, and 4 represent right plate, 5 represent upper cover, and 6 represent base, and 7 represent back of the body frame, and 8 represent backboard, and 9 represent connector base, 10 represent guide groove, 11 indication circuit plates, and 51 represent socket, and 61 represent fixing feet interface.
Embodiment
In order to make the purpose of this utility model, technical scheme and advantage clearly understand, below in conjunction with accompanying drawing, the utility model is further elaborated.Should be appreciated that embodiment described herein only in order to explain the utility model, and be not used in restriction the utility model.
Embodiment
Referring to figs. 1 through Fig. 3, the box of customizable satellite magnetic component control line road described in the present embodiment, the body structure that described circuit box is assemblied to form by front panel 1, rear board 2, left plate 3, right plate 4, upper cover 5 and base 6, the connection between any two panels is all that screw removably connects; Described circuit box also comprises the back of the body frame 7 be arranged in body structure, and described back of the body frame 7 is parallel to described front panel 1, and is arranged on described upper cover 5 and described base 6 near described front panel 1; Be specially: described back of the body frame upper stupefied is connected by screw that described upper cover 5 is upper and lower is stupefiedly connected by screw described base 6.
The left side stupefied 71 and the right side stupefied 72 of described back of the body frame 7 are symmetrical arranged interface 75 relative to the vertical center line of described back of the body frame, by described interface, described back of the body frame 7 connects backboard 8, on described backboard 8, vertical welding connects connector seat 9, guide groove 10 is set respectively being on the described left plate inwall of same horizontal plane and described right plate inwall with described connector seat 9; Described backboard 8 is connected by screw on the interface of described back of the body frame 7, and one end that described backboard 8 deviates from described back of the body frame 7 is provided with plug holder.The quantity 1 of described backboard, the guide groove sum on left and right side plate inwall totally 8, the left cold-peace of back of the body frame right stupefied on interface sum totally 3.
In the present embodiment, described upper cover 5 is provided with through hole, and described through hole is installed the socket 51 mated with described through hole, the number of described through hole is identical with the number of described socket 51, be 7, and described socket is connected with described backplane communication.The minor axis center line of all described through holes overlaps, centered by line P, and described center line P is parallel with the long axis centerline M of described upper cover, and described center line P and described back of the body frame vertical range are greater than described center line M and described back of the body frame vertical range.The quantity of socket is determined by with the interface data list totally consulted, and the size of socket is determined by connector model, and being covered with through hole is therefore customize according to the size of insert pocket.
In the present embodiment, by the guide groove on described left plate, described right plate inwall, circuit board is inserted in described circuit box, is connected with the connector seated connection on described backboard 7.Base 6 outer wall of described circuit box is also provided with fixing feet interface 61.
Control circuit box described in the utility model is the circuit box of customizable size, is embodied in: the length of described circuit box inner chamber as required in socket connection to described circuit box the length of the most long circuit plate of length arrange; The width of described circuit box inner chamber as required socket connection is arranged to the width of the most stretch circuit plate of described circuit box insied width, the total height setting of all circuit boards in socket connection to described circuit box as required of the height of described circuit box inner chamber.
Connection procedure of the present utility model is as follows:
The size of the circuit board connected as required, the length of how many customization circuit box, wide and high, and at left plate, have on the inwall of side plate and be symmetrical arranged guide groove, back of the body frame arranges symmetrical corresponding interface, and ensure that symmetrically arranged interface and symmetrically arranged guide groove are in same level, then by front panel, left plate, right plate is connected on base with the back of the body frame screw being connected with backboard, then circuit board is plugged on backboard by guide groove, then upper cover screw is connected to front panel, left plate, right plate, on backboard, finally by rear board and left plate, right plate, upper cover screw is connected and fixed.
By adopting technique scheme disclosed in the utility model, obtain effect useful as follows:
Satellite magnetic component control line road described in the utility model box is according to the concrete size custom fabricated of magnetometer control circuit board and magnetic torquer control circuit board, meet satellite application environment to aspect requirements such as circuit box structural strength, thermal characteristicss, reduce circuit box weight and size to greatest extent.
The above is only preferred implementation of the present utility model; it should be pointed out that for those skilled in the art, under the prerequisite not departing from the utility model principle; can also make some improvements and modifications, these improvements and modifications also should look protection range of the present utility model.
Claims (10)
1. a customizable satellite magnetic component control line road box, it is characterized in that, the body structure that described circuit box is assemblied to form by front panel, rear board, left plate, right plate, upper cover and base, the connection between any two panels all removably connects;
Described circuit box also comprises the back of the body frame be arranged in described body structure, and described back of the body frame is parallel to described front panel, and is arranged on described upper cover and described base near described front panel;
Described circuit box also comprises backboard, described backboard is arranged on the side that described back of the body frame deviates from described front panel, on described backboard, vertical welding connects connector seat, arranges guide groove respectively being on the described left plate inwall of same horizontal plane and described right plate inwall with described connector seat;
Be covered with through hole on described, described through hole is installed the socket mated with described through hole, and the number of described through hole is identical with the number of described socket, and is no less than 1; Described socket is connected with described backplane communication.
2. control circuit box according to claim 1, is characterized in that, described in removably connect and comprise screw and connect.
3. control circuit box according to claim 1, is characterized in that, described back of the body frame upper stupefied is connected by screw that described upper cover is upper and lower is stupefiedly connected by screw described base.
4. control circuit box according to claim 1, is characterized in that, on the left stupefied and right side of described back of the body frame is stupefied, be symmetrical arranged interface relative to the vertical center line of described back of the body frame, described backboard is connected by screw on the interface of described back of the body frame.
5. control circuit box according to claim 1, it is characterized in that, described connector seat is arranged on the side that described backboard deviates from described back of the body frame.
6. control circuit box according to claim 1, it is characterized in that, circuit board is inserted in described circuit box by the guide groove on described left plate, described right plate inwall, with the connector seat socket connection on described backboard.
7. control circuit box according to claim 1, it is characterized in that, the minor axis center line of all described through holes overlaps, centered by line P, and described center line P is parallel with the long axis centerline M of described upper cover, and described center line P and described back of the body frame vertical range are greater than described center line M and described back of the body frame vertical range.
8. control circuit box according to claim 1, it is characterized in that, described connector seat is identical with needing the quantity of the circuit board be installed in described circuit box.
9. control circuit box according to claim 1, it is characterized in that, the base outer wall of described circuit box is also provided with fixing feet interface.
10. control circuit box according to claim 1, is characterized in that, described socket be screwed be connected to described on cover.
Priority Applications (1)
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CN201520343049.7U CN204652817U (en) | 2015-05-25 | 2015-05-25 | A kind of customizable satellite magnetic component control line road box |
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CN201520343049.7U CN204652817U (en) | 2015-05-25 | 2015-05-25 | A kind of customizable satellite magnetic component control line road box |
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CN201520343049.7U Active CN204652817U (en) | 2015-05-25 | 2015-05-25 | A kind of customizable satellite magnetic component control line road box |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116506256A (en) * | 2023-06-29 | 2023-07-28 | 合肥岭雁科技有限公司 | High integration gateway convenient to installation |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN116506256A (en) * | 2023-06-29 | 2023-07-28 | 合肥岭雁科技有限公司 | High integration gateway convenient to installation |
CN116506256B (en) * | 2023-06-29 | 2023-08-22 | 合肥岭雁科技有限公司 | High integration gateway convenient to installation |
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