CN207398638U - Pull rod aircraft power distribution case - Google Patents
Pull rod aircraft power distribution case Download PDFInfo
- Publication number
- CN207398638U CN207398638U CN201721169835.5U CN201721169835U CN207398638U CN 207398638 U CN207398638 U CN 207398638U CN 201721169835 U CN201721169835 U CN 201721169835U CN 207398638 U CN207398638 U CN 207398638U
- Authority
- CN
- China
- Prior art keywords
- babinet
- pull rod
- power distribution
- aircraft power
- sets
- 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.)
- Expired - Fee Related
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Abstract
The utility model discloses pull rod aircraft power distribution case, including：Babinet, the babinet is hexahedron structure, the left side of the babinet sets pull rod and knob, the bottom of the babinet sets for mobile castor and is used to support the foot grain of babinet, the front side of the babinet sets display control unit, and the display control unit includes input master switch, output switch-dividing, for detecting the voltmeter of input voltage and electric current and ammeter, Insurance Block and voltage change-over switch for detecting voltage between every two-phase of three-phase input voltage；The rear side of the babinet sets to connect the input aero seat of external power supply and the output aero seat for connecting electrical equipment, and the output aero seat is also connected with output indicator.The utility model sets pull rod and castor on babinet, facilitates the movement and transport of distribution box；Distribution box power transmission using manually " power on step by step " it is upper be electrically effectively protected electrical equipment, improve power supply reliability.
Description
Technical field
The utility model is related to aircraft power distribution technical fields, and in particular to pull rod aircraft power distribution case.
Background technology
Distribution box is that switchgear, measuring instrumentss, protection electric appliance and ancillary equipment are assembled in envelope by electrical wiring requirement
Close or semiclosed metal safe in or screen width on, form low-voltage distribution equipment.It can be connect during normal operation by manual or automatic switch
Logical or disjunction circuit.By protection electric appliance cut-out circuit or alarm when failure or irregular operating.Fortune can be shown by means of measuring instrumentss
Various parameters in row can also be adjusted some electric parameters, and letter is prompted or sent to deviateing normal operating conditions
Number.It is usually used in each sending out, matching somebody with somebody, in electric substation.
Aircraft needs power supply in flight course, to meet the power demand of distinct device, existing aircraft power distribution
Case is generally using overall control architecture, and when being powered, all equipment for connecting the distribution box are turned on power supply, it is impossible to effectively
Carry out grading control, and cannot effectively be connected between distribution box, connection is complicated, inconvenient to use.
Utility model content
The technical problem to be solved by the utility model is to the deficiencies in for the above-mentioned prior art, disclose pull rod boat
Empty distribution box.
The technical solution adopted in the utility model is：Pull rod aircraft power distribution case, including：Babinet, the babinet are hexahedron
Structure, the left side of the babinet set pull rod and knob, and the bottom of the babinet sets for mobile castor and is used to support
The foot grain of babinet, the front side of the babinet set display control unit, and the display control unit includes input master switch, output
Switch-dividing, for detecting the voltmeter of input voltage and electric current and ammeter, Insurance Block and for detecting three-phase input voltage
Every two-phase between voltage voltage change-over switch；The rear side of the babinet sets to connect the input aero seat of external power supply
With for connecting the output aero seat of electrical equipment, the output aero seat is also connected with output indicator.
Further, the babinet also sets up protecgulum and rear cover, and the protecgulum and rear cover are with babinet to be detachably connected.
Further, lock core on the protecgulum is set, setting lock is covered after described, set on the babinet for it is preceding
The lock and lock core that lid and rear cover fasten.
Further, ring is also set up on rear side of the babinet and goes out five core aviation sockets.
Further, the corner of the babinet sets corner protector, the protecgulum and rear cover to set corner protector, institute with babinet connecting portion
The closed angle for stating protecgulum and rear cover is rounded structure.
Further, the input aero seat is using the socket of the prestige Pu TYP545 models of five core 65A, the output aviation
Seat uses the socket of three core 16A prestige Pu TYP5601 models.
Further, the babinet is made of metal plate.
The utility model has the following advantages compared with prior art：
Pull rod aircraft power distribution case provided by the utility model sets pull rod and castor on babinet, can facilitate to distribution
The movement of case sets knob on babinet, facilitates and lift distribution box, and pull rod is combined with shaking hands with castor, facilitates distribution box
Movement and transport；One end that castor is surveyed with being arranged on babinet, the other end in babinet bottom side sets foot grain, when placing, with
Castor plays the role of supporting box jointly, while prevents babinet from wearing；The front and rear sides of babinet set display control to fill respectively
It puts and input-output socket；Ring goes out five core aviation sockets for drawing the electric converting interface to next distribution box from a distribution box,
Realize the connection between distribution box；Output aero seat is the primary interface of electrical equipment, conveniently inserted quick, is referred to by output
Show that lamp inspection surveys whether three cores output aero seat has electricity；By setting protecgulum and rear cover, babinet is protected, improves reliability,
Direct body contact is avoided, is effectively isolated foreign matter；Distribution box power transmission using manually " power on step by step " it is upper electrically, avoid
Impact of the heavy load to power grid moment is effectively protected electrical equipment, improves power supply reliability.
Description of the drawings
Fig. 1 is the pull rod aircraft power distribution case explosive view of the utility model；
Fig. 2 is the pull rod aircraft power distribution case three-dimensional structure diagram of the utility model；
Fig. 3 is the pull rod aircraft power distribution case front view of the utility model；
Fig. 4 is the pull rod aircraft power distribution case left view of the utility model；
Fig. 5 is the pull rod aircraft power distribution case rearview of the utility model；
Fig. 6 is the pull rod aircraft power distribution case bottom view of the utility model；
Fig. 7 is the pull rod aircraft power distribution case of the utility model and protecgulum, rear cover Split type structure figure；
Fig. 8 is the pull rod aircraft power distribution case of the utility model and protecgulum, rear cover installation diagram.
Specific embodiment
The utility model is described in detail in shown each embodiment below in conjunction with the accompanying drawings, but it should explanation,
These embodiments are not limitation of the utility model, and those of ordinary skill in the art are according to these embodiment institute works
Energy, method or equivalent transformation or replacement in structure, belong within the scope of protection of the utility model.
Referring to Fig. 1 to Fig. 8, wherein Fig. 1 is the pull rod aircraft power distribution case explosive view of the utility model；Fig. 2 is new for this practicality
The pull rod aircraft power distribution case three-dimensional structure diagram of type；Fig. 3 is the pull rod aircraft power distribution case front view of the utility model；Fig. 4 is this reality
With new pull rod aircraft power distribution case left view；Fig. 5 is the pull rod aircraft power distribution case rearview of the utility model；Fig. 6 is this reality
With new pull rod aircraft power distribution case bottom view；Fig. 7 is the pull rod aircraft power distribution case of the utility model and protecgulum, rear cover split-type knot
Composition；Fig. 8 is the pull rod aircraft power distribution case of the utility model and protecgulum, rear cover installation diagram.
As shown in Figures 1 to 8, pull rod aircraft power distribution case, including：Babinet 1, the babinet 1 be hexahedron structure, the case
The left side of body 1 sets pull rod 2 and knob 3, and the bottom of the babinet 1 sets for mobile castor 4 and is used to support babinet 1
Foot grain 5, the front side of the babinet 1 set display control unit, and the display control unit includes input master switch 6, output point
Switch 7, for detecting the voltmeter 8 of input voltage and electric current and ammeter 9, Insurance Block 10 and for detecting three-phase input electricity
The voltage change-over switch 11 of voltage between every two-phase of pressure；The rear side of the babinet 1 sets to connect the input of external power supply
Aero seat 12 and the output aero seat 13 for connecting electrical equipment, the output aero seat 13 are also connected with output indicator
14。
Pull rod aircraft power distribution case provided by the utility model sets pull rod and castor on babinet, can facilitate to distribution
The movement of case sets knob on babinet, facilitates and lift distribution box, and pull rod is combined with shaking hands with castor, facilitates distribution box
Movement and transport.One end that castor is surveyed with being arranged on babinet, the other end in babinet bottom side sets foot grain, when placing, with
Castor plays the role of supporting box jointly, while prevents babinet from wearing, and the front and rear sides of babinet set display control to fill respectively
It puts and input-output socket, display control unit includes a digital display voltmeter, three digital display ammeters and voltage change-over switch,
Digital display voltmeter acts on：Detection come piezoelectric voltage it is whether normal, normal voltage value 380V；Digital display ammeter is for when running work
Detect three-phase electricity size of current, if it keeps in balance, it is no to adjust load in time, avoid failure；Voltage change-over switch
Reach normal voltage, such as 380V/220V for whether having between the every two-phase of rotation detection three-phase electricity；
The breaker that master switch uses DZ158-125/100A/3P models is inputted, for total lock of distribution box, distribution box institute
There is switch-dividing by incoming call, input master switch is acted on generally as isolated from power protector, does not make load switch under normal circumstances
Switching on；Export switch-dividing use DZ47-60/D32 1P models breaker, be equipment electricity consumption load switch, break, overload
It trips when can be anxious, ensures that equipment is without damage safely.
Ring is also set up on rear side of babinet and goes out five core aviation sockets 15.Ring go out five core aviation sockets 15 for 32A export, for from
One distribution box draws the converting interface that electricity arrives next distribution box；Realize the connection between distribution box.
Output aero seat 13 is the primary interface of electrical equipment, conveniently inserted quick, can set multiple output aviations
Seat according to the size of babinet, can set the output aero seat of fair amount；Three cores are detected by output indicator and export aviation
Whether seat has electricity.
In the utility model embodiment, babinet 1 also sets up protecgulum 16 and rear cover 17, the protecgulum 16 and rear cover 17 and babinet
1 is to be detachably connected.
Protecgulum 16 and rear cover 17 may be employed with babinet 1 is bolted, snaps connection or latches connection, it is preferred that preceding
Using lock connection between lid, rear cover and babinet, lock core wherein on protecgulum 16 is set, lock, corresponding case are set on rear cover 17
It is set on body 1 for the lock 20 and lock core 19 with protecgulum and rear cover fastening；Or protecgulum covers with after and is respectively provided with lock core, case
Lock is correspondingly arranged on body；Or protecgulum covers with after and is respectively provided with lock, and lock core is correspondingly arranged on babinet；Specifically in design,
Lock core and lock installation position are unrestricted, so as to realizing between babinet and protecgulum and rear cover subject to connection.
In the utility model embodiment, the corner of babinet 1 sets corner protector 18, and the protecgulum and rear cover are set with babinet connecting portion
Put corner protector, the closed angle of the protecgulum and rear cover is rounded structure.
Further, the input aero seat 12 is using the socket of the prestige Pu TYP545 models of five core 65A, the output boat
Vacant seat 13 uses the socket of three core 16A prestige Pu TYP5601 models.
Further, the babinet 1 is made of metal plate.Multi-function jack 21 is also set up on front side of babinet, for making
For spare accessory power outlet.
Pull rod aircraft power distribution case provided by the utility model, it is small, light-weight, it is portable, can be portable, Ke Yila,
Keep flat place vertically can, convenient and efficient, multiple-channel output, compatibility is strong, and flexibility ratio is high；It is designed using body structure, collection protection, control
For the multiple functions such as system, monitoring in one, components' placement is neat, cabling specification, is easy to use and safeguards；By set protecgulum and
Rear cover protects babinet, improves reliability, avoids direct body contact, be effectively isolated foreign matter, has short circuit, overcurrent, mistake
Pressure, overload, etc. protection features；Power supply electricity is inputted from five core aviation sockets, is inputted master switch into distribution box, is passed through ammeter, electricity
Pressure table and three phase mains indicator light show into electricity it is whether normal, through input master switch to each electrical equipment output switch-dividing,
Output switch-dividing is out connected to output aero seat.Distribution box power transmission using manually " power on step by step " it is upper electrically, keep away
Exempt from impact of the heavy load to power grid moment, be effectively protected electrical equipment, improve power supply reliability.
The a series of tool that the feasibility embodiment only for the utility model is described in detail of those listed above
Body illustrates, they are all to be made without departing from the utility model skill spirit not to limit the scope of protection of the utility model
Equivalent implementations or change should be included within the scope of protection of this utility model.
Moreover, it will be appreciated that although this specification is described in terms of embodiments, but not each embodiment is only wrapped
Containing an independent technical solution, this description of the specification is merely for the sake of clarity, and those skilled in the art should
Using specification as an entirety, the technical solutions in each embodiment can also be properly combined, forms those skilled in the art
It is appreciated that other embodiment.
Claims (7)
1. pull rod aircraft power distribution case, which is characterized in that including：Babinet, the babinet be hexahedron structure, the left side of the babinet
Pull rod and knob are set, and the bottom of the babinet sets for mobile castor and be used to support the foot grain of babinet, the babinet
Front side set display control unit, the display control unit include input master switch, output switch-dividing, for detect input
The voltmeter and ammeter of voltage and current, Insurance Block and the electricity for detecting voltage between every two-phase of three-phase input voltage
Press change-over switch；The rear side of the babinet sets to connect the input aero seat of external power supply and for connecting electrical equipment
Aero seat is exported, the output aero seat is also connected with output indicator.
2. pull rod aircraft power distribution case according to claim 1, which is characterized in that the babinet also sets up protecgulum and rear cover,
The protecgulum and rear cover are with babinet to be detachably connected.
3. pull rod aircraft power distribution case according to claim 2, which is characterized in that lock core is set on the protecgulum, after described
Setting lock is covered, is set on the babinet for the lock and lock core with protecgulum and rear cover fastening.
4. pull rod aircraft power distribution case according to claim 1, which is characterized in that also set up ring on rear side of the babinet and go out five
Core aviation socket.
5. pull rod aircraft power distribution case according to claim 2, which is characterized in that the corner of the babinet sets corner protector, institute
It states protecgulum and rear cover and babinet connecting portion and corner protector is set, the closed angle of the protecgulum and rear cover is rounded structure.
6. pull rod aircraft power distribution case according to claim 1, which is characterized in that the babinet is made of metal plate.
7. pull rod aircraft power distribution case according to claim 1, which is characterized in that the input aero seat uses five core 65A
Prestige Pu TYP545 models socket, it is described output aero seat use three core 16A prestige Pu TYP5601 models socket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721169835.5U CN207398638U (en) | 2017-09-13 | 2017-09-13 | Pull rod aircraft power distribution case |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721169835.5U CN207398638U (en) | 2017-09-13 | 2017-09-13 | Pull rod aircraft power distribution case |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207398638U true CN207398638U (en) | 2018-05-22 |
Family
ID=62417226
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721169835.5U Expired - Fee Related CN207398638U (en) | 2017-09-13 | 2017-09-13 | Pull rod aircraft power distribution case |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207398638U (en) |
-
2017
- 2017-09-13 CN CN201721169835.5U patent/CN207398638U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20180522 Termination date: 20180913 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |