CN112105197B - Sealed power supply control box - Google Patents
Sealed power supply control box Download PDFInfo
- Publication number
- CN112105197B CN112105197B CN202011013206.XA CN202011013206A CN112105197B CN 112105197 B CN112105197 B CN 112105197B CN 202011013206 A CN202011013206 A CN 202011013206A CN 112105197 B CN112105197 B CN 112105197B
- Authority
- CN
- China
- Prior art keywords
- electric connector
- fixedly connected
- circuit breaker
- mounting plate
- box body
- 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.)
- Active
Links
- 238000005192 partition Methods 0.000 claims abstract description 12
- 238000001514 detection method Methods 0.000 claims abstract 6
- 238000007789 sealing Methods 0.000 claims description 22
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Substances [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 5
- 238000012423 maintenance Methods 0.000 claims description 4
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 230000003647 oxidation Effects 0.000 claims description 3
- 238000007254 oxidation reaction Methods 0.000 claims description 3
- 238000007689 inspection Methods 0.000 description 5
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 238000009413 insulation Methods 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 3
- 230000007613 environmental effect Effects 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
- 239000003973 paint Substances 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000005070 sampling Methods 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
- 230000007704 transition Effects 0.000 description 1
Classifications
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- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0247—Electrical details of casings, e.g. terminals, passages for cables or wiring
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01R—ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS
- H01R13/00—Details of coupling devices of the kinds covered by groups H01R12/70 or H01R24/00 - H01R33/00
- H01R13/02—Contact members
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/02—Details
- H05K5/0217—Mechanical details of casings
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K5/00—Casings, cabinets or drawers for electric apparatus
- H05K5/06—Hermetically-sealed casings
- H05K5/069—Other details of the casing, e.g. wall structure, passage for a connector, a cable, a shaft
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K7/00—Constructional details common to different types of electric apparatus
- H05K7/02—Arrangements of circuit components or wiring on supporting structure
-
- H—ELECTRICITY
- H05—ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
- H05K—PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
- H05K9/00—Screening of apparatus or components against electric or magnetic fields
- H05K9/0007—Casings
Landscapes
- Engineering & Computer Science (AREA)
- Microelectronics & Electronic Packaging (AREA)
- Patch Boards (AREA)
- Connection Or Junction Boxes (AREA)
Abstract
The invention relates to the technical field of aerospace, in particular to a sealed power supply control box which comprises a box body, a first electric connector, a second electric connector, a third electric connector, a lamp detection button, a switch, a circuit breaker and a relay, wherein the box body is of a cuboid, a first accommodating chamber and a second accommodating chamber are arranged in the box body, the circuit breaker, the relay, the lamp detection button and the switch are arranged in the second accommodating chamber, the third electric connector is fixedly connected with a partition wall, a contact pin of the third electric connector extends into the first accommodating chamber, the third electric connector is fixedly connected with the relay, one end of the circuit breaker is fixedly connected with a circuit breaker assembly, the other end of the circuit breaker is fixedly connected with a component mounting plate, the lamp detection button and the switch are further fixedly arranged on the component mounting plate, and the second electric connector is electrically connected with the third electric connector and the circuit breaker assembly through wires respectively.
Description
Technical Field
The invention relates to the technical field of aerospace, in particular to a sealed power supply control box.
Background
Most of the existing aircraft power supplies are directly input by a ground power supply socket on a power supply control box, power supply signals are identified and monitored through an upper system and a lower system of the aircraft, the ground power supply interface is limited by a control box structure and can only be installed on a frame of a non-airtight cabin of the aircraft, and the ground power supply interface is connected into the airtight cabin through a connecting cable, so that excessive large-current cables are left, the layout is overlong, the reliability and the safety of the aircraft are reduced, and the severe environmental conditions and longer service life requirements cannot be met. Therefore, there is a strong need for a bottom power control box with more reasonable layout in the box body.
Disclosure of Invention
In order to solve the problems, the invention provides a sealed power supply control box which has the advantages of reasonable layout, low transmission loss, good sealing performance, electromagnetic signal interference reduction and the like.
In order to achieve the above purpose, the invention adopts the following technical scheme:
The utility model provides a sealed power control box, includes box body, first electric connector, second electric connector, third electric connector, lamp examine button, switch, circuit breaker and relay, the box body main part is the cuboid, has detachable components and parts mounting panel and hou gai on the box body, has first holding cavity and second holding cavity in the box body inside, first holding cavity and second holding cavity have shared partition wall, first electric connector one end is through insulating mounting panel and the first holding cavity front wall fixed connection of box body, the other end and hou gai fixed connection, second electric connector and hou gai fixed connection, the circuit breaker subassembly of circuit breaker is fixed in first holding cavity, circuit breaker subassembly one end and partition wall fixed connection, the other end is through the copper bar of circuit breaker subassembly and first electric connector fixed connection, install circuit breaker, relay, lamp examine button and switch in the second holding cavity, third electric connector and partition wall fixed connection, the first electric connector and the second electric connector are used for transmitting signal to the aircraft to the first aircraft power supply, the second aircraft is connected to the first aircraft is fixed with the second aircraft is fixed with the power supply subassembly through electric connector, the signal connection is fixed connection to the first aircraft component, the second aircraft is fixed connection to the power supply subassembly, signal connection is kept down to the aircraft is fixed to the second aircraft, the signal connection to the second aircraft is fixed connection to the power supply component through the first aircraft is fixed connection, the third electrical connector is used for transmitting signals between the second electrical connector and the relay.
Preferably, the first electric connector comprises an insulating mounting plate, a sealing gasket and a pin assembly, the pin assembly is fixedly connected with the insulating mounting plate through embedding plastic pressure, the insulating mounting plate is fixedly connected with a front wall plate of a first accommodating cavity of the box body, the sealing gasket is clamped by the insulating mounting plate and the front wall plate of the first accommodating cavity of the box body, the tail part of the pin assembly is provided with a thread section, the thread section is fixedly connected with the rear cover through a screw cap, and an axial sealing ring and a radial sealing ring are further arranged at the joint of the pin assembly and the rear cover.
Preferably, the first electrical connector further has an insulating pad and an insulating boot, the insulating pad being sandwiched by the insulating boot and the rear cover.
Preferably, the component mounting plate is also connected with an indicator lamp.
Preferably, the insulating mounting plate is provided with a plurality of insulating rib platforms with through holes at intervals.
Preferably, an iron strap is also fixed at the rear of the box body.
Preferably, the surface of the case is subjected to conductive oxidation treatment.
The beneficial effects of using the invention are as follows: according to the invention, a traditional copper bar switching transition mode is eliminated, the length of the contact body of the first electric connector is prolonged, after the assembly is completed, the control box is directly extended from the corresponding position of the rear cover to serve as a binding post, so that the loss during ground power supply transmission is greatly reduced, the layout is better and more reasonable, and the power supply quality is improved; two mutually independent accommodating chambers are formed in the box body, wherein the first accommodating chamber forms a first sealing layer through a front wall plate, a partition wall, a first electric connector, a circuit breaker assembly and a third electric connector socket, and a second sealing layer is formed by the box body, a rear cover, a second electric connector and an insulating pad through a second layer, so that an independent sealing chamber is formed, the control box meets the technical requirement of being mounted on a hermetic cabin frame, and corrosion-prone conducting pieces are distributed in the first accommodating chamber to prevent damage caused by environmental factors; the second accommodating chamber is internally provided with a layout of vulnerable electric parts, so that the maintenance and the replacement are convenient; the indication, control and sampling functions of the ground power supply are integrated into a whole through the indication lamp, the switch, the relay and the circuit breaker, so that the transmission of the ground power supply has wider functions, good environment resistance and electromagnetic compatibility.
Drawings
FIG. 1 is a bottom view of the present invention;
FIG. 2 is a schematic view of the internal structure of the present invention;
FIG. 3 is a schematic view of an assembly structure of an insulating mounting plate, a gasket, and a pin assembly in a first electrical connector according to the present invention;
fig. 4 is a perspective view of the dielectric mounting plate of the first electrical connector of the present invention.
The reference numerals include:
1-box body, 11-component mounting plate, 12-rear cover, 13-partition wall, 2-first electric connector, 21-insulation mounting plate, 211-insulation rib platform, 22-sealing gasket, 23-insulation gasket, 24-insulation protection cover, 3-second electric connector, 4-third electric connector, 5-lamp inspection button, 6-switch, 7-circuit breaker, 71-circuit breaker assembly, 711-conductive copper bar, 8-relay, 9-bonding wire and 10-indicator lamp.
Detailed Description
The present invention will be described in detail below with reference to the accompanying drawings.
As shown in fig. 1-4, a sealed power supply control box comprises a box body 1, a first electric connector 2, a second electric connector 3, a third electric connector 4, a lamp inspection button 5, a switch 6, a circuit breaker 7 and a relay 8, wherein the box body 1 is a cuboid, a detachable component mounting plate 11 and a rear cover 12 are arranged on the box body 1, a first accommodating chamber and a second accommodating chamber are arranged in the box body 1, the first accommodating chamber and the second accommodating chamber are provided with a shared partition wall 13, one end of the first electric connector 2 is fixedly connected with a front wall plate of the first accommodating chamber of the box body 1 through an insulating mounting plate 21, the other end of the first electric connector is fixedly connected with the rear cover 12, the second electric connector 3 is fixedly connected with the rear cover 12, a circuit breaker component 71 of the circuit breaker 7 is fixed in the first accommodating chamber, one end of the breaker component 71 is fixedly connected with the partition wall 13, the other end of the breaker component is fixedly connected with the first electric connector 2 through a conductive copper bar 711 of the breaker component 71, a breaker 7, a relay 8, a lamp inspection button 5 and a switch 6 are installed in the second accommodating chamber, the third electric connector 4 is fixedly connected with the partition wall 13, a contact pin of the third electric connector 4 extends into the first accommodating chamber, the third electric connector 4 is fixedly connected with the relay 8, one end of the breaker 7 is fixedly connected with the breaker component 71, the other end of the breaker 7 is fixedly connected with the component mounting plate 11, a lamp inspection button 5 and a switch 6 are also fixed on the component mounting plate 11, the second electric connector 3 is respectively electrically connected with the third electric connector 4 and the breaker component 71 through wires, the relay 8 is respectively electrically connected with the lamp inspection button 5 and the switch 6 through wires, the first electric connector 2 is used for transmitting external power signals to an airplane, the second electric connector 3 is used for inputting a direct current power signal to the sealed power supply control box, transmitting an external power signal and a maintenance signal to the aircraft, and the third electric connector 4 is used for transmitting signals between the second electric connector and the relay. The third electric connector 4 transits the non-sealing wire from the first accommodating chamber to the second accommodating chamber, namely transits from the non-airtight area to the airtight area, the sealed power supply control box adopts airtight design, the first accommodating chamber is provided with two air sealing layers, and the first layer consists of a front wall plate and a partition wall 13 of the first accommodating chamber of the box body 1, the first electric connector 2, a circuit breaker component 71 and a socket of the third electric connector 4; the second layer consists of the case 1, the rear cover 12, the second electrical connector 3 connector and the insulating pad 23. The sealed power supply control box adopts an electromagnetic cavity-separating design, low-voltage electronic components are arranged on the component mounting plate 11 and are independently formed into cavities, namely, the second accommodating cavity, and the design can achieve the purposes of replacing vulnerable electronic components on the premise of not damaging the tightness of the components in the first accommodating cavity of the product, isolating an external power supply from a control power supply through a metal box body, preventing mutual interference during working and effectively improving the electromagnetic shielding effect.
When in use, an external power signal is input from the front end of the first electric connector 2, the external power signal is divided into two parts, one part of the external power signal is directly output from the rear end of the first electric connector 2, and the other part of the external power signal is transmitted to the circuit breaker 7 through the circuit breaker assembly 71 and then is transmitted to the second electric connector for output by the circuit breaker 7; the maintenance signal is input by the second electric connector 2, transmitted to the relay 8 through the third electric connector 4, transmitted to the indicator lamp 10 and the switch 6 through the relay 8, transmitted back to the third electric connector 4, and simultaneously transmitted back to the second electric connector 2 together with the auxiliary point signal on the first electric connector 2 and then output.
The first electric connector 2 comprises an insulating mounting plate 21, a sealing gasket 22 and a contact pin assembly, wherein the contact pin assembly is fixedly connected with the insulating mounting plate 21 through embedding plastic pressure, the insulating mounting plate 21 is fixedly connected with a front wall plate of a first accommodating cavity of the box body 1, the sealing gasket 22 is clamped by the insulating mounting plate 21 and the front wall plate of the first accommodating cavity of the box body 1, the tail part of the contact pin assembly is provided with a thread section, the thread section is fixedly connected with the rear cover 12 through a screw cap, and an axial sealing ring and a radial sealing ring are further arranged at the joint of the contact pin assembly and the rear cover 12 and realize an airtight function through two layers of sealing rings and a connector sealing piece matched with the two layers of sealing rings.
The first electrical connector also has an insulating pad 23 and an insulating boot 24, the insulating pad 23 being sandwiched by the insulating boot 24 and the rear cover 12.
An indicator lamp 10 is also connected to the component mounting plate 11.
The insulating mounting plate 21 is provided with a plurality of insulating rib stand 211 with spaced through holes.
An iron strap 9 is also fixed behind the box body 1. The bonding wires 9 connect all parts of the aircraft to form an equipotential body, the overall electric potential is equal, and the tip discharge is prevented from being influenced by static electricity and lightning.
And conducting oxidation treatment is carried out on the surface of the box body 1. Except for the parts of the local connection parts, other parts are subjected to paint spraying treatment, so that the overall environmental resistance of the product is improved.
The foregoing is merely exemplary of the present invention, and many variations may be made in the specific embodiments and application scope of the invention by those skilled in the art based on the spirit of the invention, as long as the variations do not depart from the gist of the invention.
Claims (5)
1. A sealed power control box, characterized in that: the electric power box comprises a box body (1), a first electric connector (2), a second electric connector (3), a third electric connector (4), a lamp detection button (5), a switch (6), a circuit breaker (7) and a relay (8), wherein the box body (1) is a cuboid, a detachable component mounting plate (11) and a rear cover (12) are arranged on the box body (1), a first accommodating chamber and a second accommodating chamber are arranged in the box body (1), the first accommodating chamber and the second accommodating chamber are provided with a shared partition wall (13), one end of the first electric connector (2) is fixedly connected with a front wall plate of the first accommodating chamber of the box body (1) through an insulating mounting plate (21), the other end of the first electric connector is fixedly connected with the rear cover (12), a circuit breaker component (71) of the circuit breaker (7) is fixedly connected with the rear cover (12), one end of the circuit breaker component (71) is fixedly connected with the partition wall (13), the other end of the circuit breaker component (71) is fixedly connected with the first electric connector (7), the second electric connector (3) is fixedly connected with the first electric connector (6) through the first electric connector (7), the second electric connector (711) and the first electric connector (6) are fixedly connected with the first electric connector (3), the contact pin of the third electric connector (4) extends into the first accommodating cavity, the third electric connector (4) is fixedly connected with the relay (8), one end of the circuit breaker (7) is fixedly connected with the circuit breaker assembly (71), the other end of the circuit breaker is fixedly connected with the component mounting plate (11), the component mounting plate (11) is also fixedly provided with the light detection button (5) and the switch (6), the second electric connector (3) is respectively electrically connected with the third electric connector (4) and the circuit breaker assembly (71) through wires, the relay (8) is respectively electrically connected with the light detection button (5) and the switch (6) through wires, the first electric connector (2) is used for transmitting external power signals to an airplane, the second electric connector (3) is used for inputting direct current power signals to the sealed power control box and transmitting external power signals and maintenance signals to the airplane, and the third electric connector (4) is used for transmitting signals between the second electric connector and the relay;
The first electric connector (2) comprises an insulating mounting plate (21), a sealing gasket (22) and a contact pin assembly, wherein the contact pin assembly is fixedly connected with the insulating mounting plate (21) through embedding plastic pressure, the insulating mounting plate (21) is fixedly connected with a front wall plate of a first accommodating cavity of the box body (1), the sealing gasket (22) is clamped by the insulating mounting plate (21) and the front wall plate of the first accommodating cavity of the box body (1), the tail part of the contact pin assembly is provided with a thread section, the thread section is fixedly connected with the rear cover (12) through a screw cap, and an axial sealing ring and a radial sealing ring are further arranged at the joint of the contact pin assembly and the rear cover (12);
the first electrical connector further has an insulating pad (23) and an insulating boot (24), the insulating pad (23) being sandwiched by the insulating boot (24) and the rear cover (12).
2. The sealed power control box according to claim 1, wherein: an indicator lamp (10) is also connected to the component mounting plate (11).
3. The sealed power control box according to claim 1, wherein: an insulating rib table (211) with a plurality of through holes is arranged on the insulating mounting plate (21).
4. The sealed power control box according to claim 1, wherein: and an iron bonding wire (9) is also fixed at the rear of the box body (1).
5. The sealed power control box according to claim 1, wherein: and conducting oxidation treatment is carried out on the surface of the box body (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011013206.XA CN112105197B (en) | 2020-09-23 | 2020-09-23 | Sealed power supply control box |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202011013206.XA CN112105197B (en) | 2020-09-23 | 2020-09-23 | Sealed power supply control box |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN112105197A CN112105197A (en) | 2020-12-18 |
| CN112105197B true CN112105197B (en) | 2024-06-18 |
Family
ID=73755218
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202011013206.XA Active CN112105197B (en) | 2020-09-23 | 2020-09-23 | Sealed power supply control box |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN112105197B (en) |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN212876331U (en) * | 2020-09-23 | 2021-04-02 | 沈阳兴华航空电器有限责任公司 | Sealed power control box |
Family Cites Families (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2015148596A1 (en) * | 2014-03-28 | 2015-10-01 | Google Inc. | User-relocatable self-learning environmental control device |
| CN104093288A (en) * | 2014-06-30 | 2014-10-08 | 沈阳兴华航空电器有限责任公司 | Small starting and unloading control box |
| CN208079563U (en) * | 2018-04-11 | 2018-11-09 | 河北华方电气机械有限公司 | A kind of wind turbine control cabinet |
-
2020
- 2020-09-23 CN CN202011013206.XA patent/CN112105197B/en active Active
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN212876331U (en) * | 2020-09-23 | 2021-04-02 | 沈阳兴华航空电器有限责任公司 | Sealed power control box |
Also Published As
| Publication number | Publication date |
|---|---|
| CN112105197A (en) | 2020-12-18 |
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