CN109510093A - Aircraft Electricity distribution panel box disassemblerassembler - Google Patents
Aircraft Electricity distribution panel box disassemblerassembler Download PDFInfo
- Publication number
- CN109510093A CN109510093A CN201811631663.8A CN201811631663A CN109510093A CN 109510093 A CN109510093 A CN 109510093A CN 201811631663 A CN201811631663 A CN 201811631663A CN 109510093 A CN109510093 A CN 109510093A
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- CN
- China
- Prior art keywords
- distribution panel
- panel box
- electricity distribution
- bottom plate
- telescopic rod
- 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.)
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Classifications
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02B—BOARDS, SUBSTATIONS OR SWITCHING ARRANGEMENTS FOR THE SUPPLY OR DISTRIBUTION OF ELECTRIC POWER
- H02B3/00—Apparatus specially adapted for the manufacture, assembly, or maintenance of boards or switchgear
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- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Power Engineering (AREA)
- Vibration Prevention Devices (AREA)
Abstract
The invention discloses a kind of aircraft Electricity distribution panel box disassemblerassemblers, including bottom plate, the bottom surface of bottom plate is equipped with electric telescopic rod vertically, the lower end of electric telescopic rod is fixedly connected with connecting rod, and the both ends of connecting rod are fixed with inserted link, through-hole there are two opening up is run through on bottom plate, the upper end of inserted link is movable to be upwardly extended after through-hole, and be connected with the bottom surface of support plate, two inserted links are arranged in parallel with electric telescopic rod, and symmetrical about electric telescopic rod；The bottom surface of bottom plate is provided with idler wheel.The upper surface of support plate is vertically arranged with motor, and the swivel plate for placing machine Electricity distribution panel box is fixedly installed on the output shaft of motor.By the equipment, the quick demolition, installation of aircraft Electricity distribution panel box are realized, it is easy to operate, efficiency is improved, eliminates a large amount of manpowers, and the device structure is simple, it is at low cost.
Description
Technical field
The present invention relates to a kind of aircraft Electricity distribution panel box disassemblerassemblers.
Background technique
The major function of flight sequencing is the electric energy by aircraft generator generation with different line systems, different distribution
Mode is transferred to busbar, then passes through busbar to electrical equipment.The key fitment of distribution system includes Electricity distribution panel box.
But the volume of existing Electricity distribution panel box increases, it is heavier, it is difficult to carry, manpower can not be relied solely on, disk case is installed
Specific position on to aircraft, therefore continue a kind of disassemblerassembler to assist the demolition, installation of Electricity distribution panel box.
Summary of the invention
The purpose of the present invention is to provide a kind of aircraft Electricity distribution panel box disassemblerassemblers, for solving in the prior art due to matching
The volume of electroplax case increases, heavier, it is difficult to carry, can not rely solely on the specific position that disk case is installed on aircraft by manpower
Technical problem.
Technical problem solved by the invention can be realized using following technical scheme:
Aircraft Electricity distribution panel box disassemblerassembler, including bottom plate, the bottom surface of bottom plate are equipped with electric telescopic rod, electric telescopic rod vertically
Lower end be fixedly connected with connecting rod, the both ends of connecting rod are fixed with inserted link, and through opening up, there are two through-hole, inserted links on bottom plate
Upper end it is movable pass through through-hole after upwardly extend, and with the bottom surface of support plate be connected, two inserted links are parallel with electric telescopic rod
Setting, and it is symmetrical about electric telescopic rod；The bottom surface of bottom plate is provided with idler wheel.
The upper surface of the support plate is vertically arranged with motor, is fixedly installed on the output shaft of motor for placing aircraft
The swivel plate of Electricity distribution panel box.
In use, first extending electric telescopic rod, driving support plate drives motor and swivel plate decline, facilitates distribution board
Case is placed on swivel plate；Then it pushes whole equipment to be moved to below the distribution storehouse on aircraft, then receives electric telescopic rod
Contracting, driving support plate drives motor, swivel plate and Electricity distribution panel box to rise, and after rising to appropriate location, starting motor makes swivel plate band
Dynamic Electricity distribution panel box rotates together, and after going to appropriate angle, Electricity distribution panel box is fixed in distribution storehouse by tool.It is set by this
It is standby, the quick demolition, installation of aircraft Electricity distribution panel box are realized, it is easy to operate, efficiency is improved, a large amount of manpowers, and the equipment are eliminated
Structure is simple, at low cost.
It is further improved, rubber ring, the lower end of rubber ring and plate upper surface is provided between the support plate and bottom plate
It is connected.When electric telescopic rod extends, and driving support plate drives motor and swivel plate to decline, the bottom surface of the support plate of rubber ring with
Rubber ring upper-end contact, and compressed, play buffer function.
Be further improved, the bottom surface of the swivel plate is fixedly installed support column, the lower end of support column open up it is fluted, it is recessed
Ball is embedded in slot, and the lower end of ball is contacted with the upper surface of support plate.By setting support column and ball, guarantee rotation
Plate during rotation, is not easy to shake, and improves structural stability.
It is further improved, the electric telescopic rod upper end and the first fixed frame are connected, and the first fixed frame and bottom plate bottom surface are solid
Fixed connection.By the way that the first fixed frame is arranged, it connect electric telescopic rod with bottom plate firm, improves structural stability.
It is further improved, is provided with the second fixed frame in the support plate, motor is fixedly connected with the second fixed frame.Pass through
Second fixed frame is set, connect motor with support plate firm, improves structural stability.
It is further improved, the motor is servo motor, realizes that swivel plate rotates clockwise or counterclockwise, and control precision
It is high.
It is further improved, is provided with handle on the bottom plate, whole equipment is pushed by handle, it is easy to operate.
It is further improved, the two sides of the electric telescopic rod are equipped with damping device, and damping device includes damper cylinder, spring
And damping block, the upper end of damping block and the bottom surface of bottom plate are connected, the lower end slidingtype of damping block is plugged in damper cylinder, spring position
In in damper cylinder, and the upper end of spring and damping block are connected, and the bottom plate of lower end and damper cylinder is fixed；The lower end of the damper cylinder is solid
Surely it is provided with supporting leg, idler wheel and supporting leg are rotatablely connected.By the way that damping device is arranged, increases the shock resistance of whole equipment, avoid transporting
Vibration causes Electricity distribution panel box to damage during defeated.
It is further improved, the idler wheel is universal wheel.
Compared with prior art, the present invention the invention has the following beneficial effects:
By the equipment, the quick demolition, installation of aircraft Electricity distribution panel box are realized, it is easy to operate, efficiency is improved, is eliminated big
Manpower is measured, and the device structure is simple, it is at low cost.
Detailed description of the invention
Fig. 1 is the structure chart of aircraft Electricity distribution panel box disassemblerassembler of the present invention.
Specific embodiment
To keep the purpose of the present invention and technical solution clearer, below in conjunction with the embodiment of the present invention to skill of the invention
Art scheme is clearly and completely described.
As shown in Figure 1, aircraft Electricity distribution panel box disassemblerassembler, including bottom plate 15, the bottom surface of bottom plate 15 are equipped with electronic stretch vertically
Contracting bar 10, the lower end of electric telescopic rod 10 are fixedly connected with connecting rod 9, and the both ends of connecting rod 9 are fixed with inserted link 5, bottom plate 15
Above through opening up there are two through-hole, the upper end of inserted link 5 is movable to be upwardly extended after through-hole, and solid with the bottom surface of support plate 17
Even, two inserted links 5 are arranged in parallel with electric telescopic rod 10, and symmetrical about electric telescopic rod 10；The bottom surface of bottom plate 15 is provided with
Idler wheel 8.
The upper surface of the support plate 17 is vertically arranged with motor 3, is fixedly installed on the output shaft of motor 3 for placing
The swivel plate 1 of machine Electricity distribution panel box.
In use, first extending electric telescopic rod 10, driving support plate 17 drives motor 3 and swivel plate 1 to decline, facilitate by
Electricity distribution panel box is placed on swivel plate；Then it pushes whole equipment to be moved to below the distribution storehouse on aircraft, then makes electronic stretch
Contracting bar 10 is shunk, and driving support plate 17 drives motor 3, swivel plate 1 and Electricity distribution panel box to rise, after rising to appropriate location, starting electricity
Machine makes swivel plate that Electricity distribution panel box be driven to rotate together, and after going to appropriate angle, Electricity distribution panel box is fixed on distribution storehouse by tool
In.By the equipment, the quick demolition, installation of aircraft Electricity distribution panel box are realized, it is easy to operate, efficiency is improved, a large amount of people are eliminated
Power, and the device structure is simple, it is at low cost.
In the present embodiment, be provided with rubber ring 16 between the support plate 17 and bottom plate 15, the lower end of rubber ring 16 with
15 upper surface of bottom plate is connected.When electric telescopic rod 10 extends, and driving support plate 17 drives motor 3 and swivel plate 1 to decline, rubber
The bottom surface of the support plate 17 of circle and rubber ring upper-end contact, and compressed, play buffer function.
In the present embodiment, the bottom surface of the swivel plate 1 is fixedly installed support column 18, and the lower end of support column 18 offers
Groove is embedded with ball 4 in groove, and the lower end of ball 4 is contacted with the upper surface of support plate 17.By the way that 18 He of support column is arranged
Ball 4 guarantees swivel plate 1 during rotation, is not easy to shake, and improves structural stability.
In the present embodiment, 10 upper end of electric telescopic rod and the first fixed frame 11 are connected, the first fixed frame 11 and bottom
15 bottom surface of plate is fixedly connected.By the way that the first fixed frame 11 is arranged, it connect electric telescopic rod 10 with bottom plate 15 firm, improves structure
Stability.
In the present embodiment, the second fixed frame 2, motor 3 and the fixed company of the second fixed frame 2 are provided in the support plate 17
It connects.By the way that the second fixed frame 2 is arranged, it connect motor 3 with support plate 17 firm, improves structural stability.
In the present embodiment, the motor 3 is servo motor, realizes that swivel plate 1 rotates clockwise or counterclockwise, and control
Precision is high.
In the present embodiment, it is provided with handle 6 on the bottom plate 15, whole equipment is pushed by handle 6, it is easy to operate.
In the present embodiment, the two sides of the electric telescopic rod 10 are equipped with damping device, and damping device includes damper cylinder
13, spring 7 and damping block 14, the upper end of damping block 14 and the bottom surface of bottom plate 15 are connected, and the lower end slidingtype of damping block 14 plugs
In damper cylinder 13, spring 7 is located in damper cylinder 13, and the upper end of spring 7 and damping block 14 are connected, lower end and damper cylinder 13
Bottom plate is fixed；The lower end of the damper cylinder 13 is fixedly installed supporting leg 12, and idler wheel 8 and supporting leg 12 are rotatablely connected.Subtracted by setting
Device is shaken, the shock resistance of whole equipment is increased, avoids vibration in transportational process that Electricity distribution panel box is caused to damage.
In the present embodiment, the idler wheel 8 is universal wheel.
As known by the technical knowledge, the present invention can pass through the embodiment party of other essence without departing from its spirit or essential feature
Case is realized.Embodiment disclosed above, in all respects are merely illustrative as a result, not the only.Institute
Have within the scope of the present invention or is included in the invention in the change being equal in the scope of the present invention.
Claims (9)
1. aircraft Electricity distribution panel box disassemblerassembler, it is characterised in that: including bottom plate (15), the bottom surface of bottom plate (15) is equipped with electronic vertically
Telescopic rod (10), the lower end of electric telescopic rod (10) are fixedly connected with connecting rod (9), and the both ends of connecting rod (9) are fixed with slotting
Bar (5), through opening up there are two through-hole on bottom plate (15), the upper end of inserted link (5) is movable pass through through-hole after upwardly extends, and with
The bottom surface of support plate (17) is connected, and two inserted links (5) are arranged in parallel with electric telescopic rod (10), and two inserted links (5) are about electricity
Dynamic telescopic rod (10) are symmetrical；The bottom surface of bottom plate (15) is provided with idler wheel (8)；
The upper surface of the support plate (17) is vertically arranged with motor (3), is fixedly installed on the output shaft of motor (3) for putting
Set the swivel plate (1) of aircraft Electricity distribution panel box.
2. aircraft Electricity distribution panel box disassemblerassembler according to claim 1, it is characterised in that: the support plate (17) and bottom plate
(15) it is provided between rubber ring (16), the lower end and bottom plate (15) upper surface of rubber ring (16) are connected.
3. aircraft Electricity distribution panel box disassemblerassembler according to claim 1 or 2, it is characterised in that: the bottom of the swivel plate (1)
Face is fixedly installed support column (18), and the lower end of support column (18) opens up fluted, is embedded in groove ball (4), and ball
(4) lower end is contacted with the upper surface of support plate (17).
4. aircraft Electricity distribution panel box disassemblerassembler according to claim 3, it is characterised in that: on the electric telescopic rod (10)
End is connected with the first fixed frame (11), and the first fixed frame (11) is fixedly connected with bottom plate (15) bottom surface.
5. aircraft Electricity distribution panel box disassemblerassembler according to claim 4, it is characterised in that: be arranged on the support plate (17)
Have the second fixed frame (2), motor (3) is fixedly connected with the second fixed frame (2).
6. aircraft Electricity distribution panel box disassemblerassembler according to claim 5, it is characterised in that: the motor (3) is servo electricity
Machine.
7. aircraft Electricity distribution panel box disassemblerassembler according to claim 6, it is characterised in that: be provided on the bottom plate (15)
Handle (6).
8. aircraft Electricity distribution panel box disassemblerassembler according to claim 7, it is characterised in that: the electric telescopic rod (10)
Two sides are equipped with damping device, and damping device includes damper cylinder (13), spring (7) and damping block (14), damping block (14) it is upper
The bottom surface at end and bottom plate (15) is connected, and the lower end slidingtype of damping block (14) is plugged in damper cylinder (13), and spring (7), which is located at, to be subtracted
It shakes in cylinder (13), and the upper end of spring (7) and damping block (14) are connected, the bottom plate of lower end and damper cylinder (13) is fixed；It is described to subtract
The lower end of shake cylinder (13) is fixedly installed supporting leg (12), and idler wheel (8) and supporting leg (12) are rotatablely connected.
9. aircraft Electricity distribution panel box disassemblerassembler according to claim 8, it is characterised in that: the idler wheel (8) is universal wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811631663.8A CN109510093A (en) | 2018-12-29 | 2018-12-29 | Aircraft Electricity distribution panel box disassemblerassembler |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201811631663.8A CN109510093A (en) | 2018-12-29 | 2018-12-29 | Aircraft Electricity distribution panel box disassemblerassembler |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN109510093A true CN109510093A (en) | 2019-03-22 |
Family
ID=65756773
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201811631663.8A Pending CN109510093A (en) | 2018-12-29 | 2018-12-29 | Aircraft Electricity distribution panel box disassemblerassembler |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN109510093A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206498098U (en) * | 2017-01-06 | 2017-09-15 | 天津市俊达新源电气设备有限公司 | A kind of damping switch cabinet kept off the rain that conveniently radiates |
| CN107919626A (en) * | 2017-12-15 | 2018-04-17 | 明光市嘉益电控科技有限公司 | A kind of conveying arrangement easy to power distribution cabinet installation |
| CN207601273U (en) * | 2017-12-19 | 2018-07-10 | 贵阳航空电机有限公司 | A kind of aerogenerator monitor station |
| CN108471073A (en) * | 2018-04-12 | 2018-08-31 | 国家电网公司 | A kind of middle-placed switch cabinet switching on/off handcart automatic propelling device |
| CN208046024U (en) * | 2018-04-23 | 2018-11-02 | 楼凯宇 | A kind of integrated multi-functional distribution box |
| CN209419077U (en) * | 2018-12-29 | 2019-09-20 | 南京工业职业技术学院 | Aircraft Electricity distribution panel box disassemblerassembler |
-
2018
- 2018-12-29 CN CN201811631663.8A patent/CN109510093A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN206498098U (en) * | 2017-01-06 | 2017-09-15 | 天津市俊达新源电气设备有限公司 | A kind of damping switch cabinet kept off the rain that conveniently radiates |
| CN107919626A (en) * | 2017-12-15 | 2018-04-17 | 明光市嘉益电控科技有限公司 | A kind of conveying arrangement easy to power distribution cabinet installation |
| CN207601273U (en) * | 2017-12-19 | 2018-07-10 | 贵阳航空电机有限公司 | A kind of aerogenerator monitor station |
| CN108471073A (en) * | 2018-04-12 | 2018-08-31 | 国家电网公司 | A kind of middle-placed switch cabinet switching on/off handcart automatic propelling device |
| CN208046024U (en) * | 2018-04-23 | 2018-11-02 | 楼凯宇 | A kind of integrated multi-functional distribution box |
| CN209419077U (en) * | 2018-12-29 | 2019-09-20 | 南京工业职业技术学院 | Aircraft Electricity distribution panel box disassemblerassembler |
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