CN205076770U - Aircraft part is ascended a height and is maintained device - Google Patents
Aircraft part is ascended a height and is maintained device Download PDFInfo
- Publication number
- CN205076770U CN205076770U CN201520883978.7U CN201520883978U CN205076770U CN 205076770 U CN205076770 U CN 205076770U CN 201520883978 U CN201520883978 U CN 201520883978U CN 205076770 U CN205076770 U CN 205076770U
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- hydraulic press
- hinge
- height
- ascended
- aircraft component
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Abstract
The utility model relates to an aircraft part is ascended a height and is maintained device, which comprises a base, the base upper portion left and right sides is provided with first hydraulic press and second hydraulic press respectively, first hydraulic press and second hydraulic press top do not are connected with first pneumatic telescopic link and the pneumatic telescopic link of second, the pneumatic telescopic link top of first pneumatic telescopic link and second do not is provided with first hinge pillar and A second hinge post, first hinge pillar and A second hinge post upper portion hinged joint have lift platform, lift platform upper portion right side is provided with electric motor, electric motor upper portion is connected with motor shaft, motor shaft upper portion is connected with rotary platform, rotary platform upper portion is connected with the backup pad, lift platform upper portion left side fixedly connected with stand. The utility model discloses a device can be effectively to maintenances of ascending a height of aircraft part, has improved and has maintained the effect, convenient adjustment is as required maintained, helps maintaining better the use.
Description
Technical field
The utility model belongs to craft preservation technical field, is specifically related to a kind of aircraft component and ascends a height attending device.
Background technology
Aircraft is the apparatus flyer in endoatmosphere or exoatmosphere spaceflight being manufactured by the mankind, can fly away from ground, control in spaceflight and by people.In order to protect the safety of people, aircraft all needs to be serviced before take-off, ensures that each parts can normally run, avoids accidents.Due to aircraft bulky, section components is positioned at eminence, brings inconvenience to the handling labor of people.Therefore, need to provide equipment of ascending a height accordingly, easily people can be transported to suitable height, be convenient to safeguard the aircraft component of eminence.
Utility model content
The purpose of this utility model is to provide a kind of aircraft component to ascend a height attending device, to ascend a height better safeguard aircraft component, improves result of use, conveniently uses as required.
To achieve these goals, the technical solution of the utility model is as follows.
A kind of aircraft component is ascended a height attending device, comprise pedestal, the left and right sides, pedestal top is respectively arranged with the first hydraulic press and the second hydraulic press, first hydraulic press and the second hydraulic press top are connected to the first Pneumatic extension bar and the second Pneumatic extension bar, first Pneumatic extension bar and the second Pneumatic extension bar top are respectively arranged with the first hinge pillar and the second hinge pillar, first hinge pillar and the second hinge pillar upper hinge are connected with lifting table, lifting table upper right is provided with electro-motor, electro-motor top is connected with motor drive shaft, motor drive shaft top is connected with rotation platform, rotary platform upper is connected with stay bearing plate, lifting table upper left-hand is fixedly connected with column, and column top is provided with the 3rd hinge pillar, and the 3rd hinge pillar right side hinge is connected with bracing frame, is connected with supporting seat, is connected with lamp bracket on the right side of supporting seat on the right side of bracing frame, is provided with multiple projection light on the right side of lamp bracket, be provided with the 3rd hydraulic press on the left of column, the 3rd hydraulic press top is connected with the 3rd Pneumatic extension bar, and the 3rd Pneumatic extension bar top is provided with the 4th hinge pillar, and the 4th hinge pillar right side hinge is connected with pipe link, is connected between pipe link with bracing frame by hinge.
Further, the electro-motor left and right sides is provided with pillar stiffener, and pillar stiffener top is provided with the ball for supporting rotation platform.
Further, supporting seat side is provided with power interface, power interface is provided with power lead and is connected with projection light.
Further, pedestal bottom is provided with multiple castor for movement.
Further, lifting table bottom is provided with dust exhaustor, and dust exhaustor top is connected with into dirt pipe, enters on the right side of dirt pipe and is connected with into dirt chamber, enters on the right side of dirt chamber and is connected with multiple sweep-up pipe, enters dirt pipe and is arranged on lifting table inside.
Further, multiple storage chamber is provided with on the right side of column.
Further, the first hydraulic press, the second hydraulic press, the 3rd hydraulic press and electro-motor is provided with signal wire (SW) and is connected with controller.
In this device, people station on the supporting plate, utilizes controller to start the first hydraulic press and the second hydraulic press, control the first Pneumatic extension bar and the elongation of the second Pneumatic extension bar, drive lifting table rises, and people is transported to suitable height, safeguards the aircraft component of eminence.Storage chamber internal memory is placed with device for subsequent use, can be used for changing the device of fault, makes aircraft component recover normal.Open dust exhaustor and carry out dedusting, suck into dirt chamber in the process risen by the dust on aircraft component surface from sweep-up pipe, dust enters in dust exhaustor collect from entering dirt pipe again, avoids dust to enter aircraft component inside and damages.Start electro-motor, motor drive shaft driven rotary platform rotates, and changes the position of stay bearing plate, people can be safeguarded aircraft component in each position.Power interface connects external power supply, and projection light starts illumination, makes the projecting environment of the illumination on aircraft component, makes people can clearly observation flight device parts.Utilize the 3rd hydraulic press to control the 3rd Pneumatic extension bar to extend, 3rd Pneumatic extension bar recycling pipe link drives bracing frame to rotate, in the process that lifting table rises, change the position of lamp bracket, make the luminous energy that projection light penetrates impinge upon the correspondence position of aircraft component.
The beneficial effect of this utility model is: this utility model device can carry out for aircraft component maintenance of ascending a height effectively, improves maintenance effects, and convenient adjustment and maintenance as required, contributes to safeguarding use better.
Accompanying drawing explanation
Fig. 1 is institute's operative installations structural representation in the utility model embodiment.
Description of symbols in figure: 1, pedestal; 2, the first hydraulic press; 3, the first Pneumatic extension bar; 4, the first hinge pillar; 5, castor; 6, lifting table; 7, the 3rd hydraulic press; 8, the 3rd Pneumatic extension bar; 9, storage chamber; 10, the 4th hinge pillar; 11, pipe link; 12, column; 13, the 3rd hinge pillar; 14, the second hinge pillar; 15, bracing frame; 16, dirt chamber is entered; 17, supporting seat; 18, power interface; 19, pillar stiffener; 20, dust exhaustor; 21, motor drive shaft; 22, ball; 23, electro-motor; 24, rotation platform; 25, stay bearing plate; 26, dirt pipe is entered; 27, lamp bracket; 28, projection light; 29, the second Pneumatic extension bar; 30, the second hydraulic press; 31, sweep-up pipe.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is described, better to understand the utility model.
Aircraft component is as shown in Figure 1 ascended a height attending device, comprise pedestal 1, the left and right sides, pedestal 1 top is respectively arranged with the first hydraulic press 2 and the second hydraulic press 30, first hydraulic press 2 and the second hydraulic press 30 top are connected to the first Pneumatic extension bar 3 and the second Pneumatic extension bar 29, first Pneumatic extension bar 3 and the second Pneumatic extension bar 29 top are respectively arranged with the first hinge pillar 4 and the second hinge pillar 14, first hinge pillar 4 and the second hinge pillar 14 upper hinge are connected with lifting table 6, lifting table 6 upper right is provided with electro-motor 23, electro-motor 23 top is connected with motor drive shaft 21, motor drive shaft 21 top is connected with rotation platform 24, rotation platform 24 top is connected with stay bearing plate 25, lifting table 6 upper left-hand is fixedly connected with column 12, column 12 top is provided with the 3rd hinge pillar 13,3rd hinge pillar 13 right side hinge is connected with bracing frame 15, supporting seat 17 is connected with on the right side of bracing frame 15, be connected with lamp bracket 27 on the right side of supporting seat 17, on the right side of lamp bracket 27, be provided with multiple projection light 28, the 3rd hydraulic press 7 is provided with on the left of column 12,3rd hydraulic press 7 top is connected with the 3rd Pneumatic extension bar 8,3rd Pneumatic extension bar 8 top is provided with the 4th hinge pillar the 10, four hinge pillar 10 right side hinge and is connected with pipe link 11, is connected between pipe link 11 with bracing frame 15 by hinge.Electro-motor 23 left and right sides is provided with pillar stiffener 19, and pillar stiffener 19 top is provided with the ball 22 for supporting rotation platform 24.Supporting seat 17 side is provided with power interface 18, power interface 18 is provided with power lead and is connected with projection light 28.Pedestal 1 bottom is provided with multiple castor 5 for movement.Lifting table 6 bottom is provided with dust exhaustor 20, and dust exhaustor 20 top is connected with into dirt pipe 26, enters on the right side of dirt pipe 26 and is connected with into dirt chamber 16, enters on the right side of dirt chamber 16 and is connected with multiple sweep-up pipe 31, enters dirt pipe 26 and is arranged on lifting table 6 inside.Multiple storage chamber 9 is provided with on the right side of column 12.First hydraulic press 2, second hydraulic press 30, the 3rd hydraulic press 7 with electro-motor 23 be provided with signal wire (SW) be connected with controller.
This device in the specific implementation, people stands on stay bearing plate 25, controller is utilized to start the first hydraulic press 2 and the second hydraulic press 30, control the first Pneumatic extension bar 3 and the second Pneumatic extension bar 29 extends, lifting table 6 is driven to rise, people is transported to suitable height, the aircraft component of eminence is safeguarded.Storage chamber 9 internal memory is placed with device for subsequent use, can be used for changing the device of fault, makes aircraft component recover normal.Open dust exhaustor 20 and carry out dedusting, suck into dirt chamber 16 in the process risen by the dust on aircraft component surface from sweep-up pipe 31, dust enters in dust exhaustor 20 collect from entering dirt pipe 26 again, avoids dust to enter aircraft component inside and damages.Start electro-motor 23, motor drive shaft 21 driven rotary platform 24 rotates, and changes the position of stay bearing plate 25, people can be safeguarded aircraft component in each position.Power interface 18 connects external power supply, and projection light 28 starts illumination, makes the projecting environment of the illumination on aircraft component, makes people can clearly observation flight device parts.Utilize the 3rd hydraulic press 7 to control the 3rd Pneumatic extension bar 8 to extend, 3rd Pneumatic extension bar 8 recycles pipe link 11 and drives bracing frame 15 to rotate, in the process that lifting table 6 rises, change the position of lamp bracket 27, make the luminous energy of injection on projection light 28 impinge upon the correspondence position of aircraft component.
The above is 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 are also considered as protection domain of the present utility model.
Claims (7)
1. an aircraft component is ascended a height attending device, comprise pedestal, it is characterized in that: the left and right sides, described pedestal top is respectively arranged with the first hydraulic press and the second hydraulic press, described first hydraulic press and the second hydraulic press top are connected to the first Pneumatic extension bar and the second Pneumatic extension bar, described first Pneumatic extension bar and the second Pneumatic extension bar top are respectively arranged with the first hinge pillar and the second hinge pillar, described first hinge pillar and the second hinge pillar upper hinge are connected with lifting table, described lifting table upper right is provided with electro-motor, described electro-motor top is connected with motor drive shaft, described motor drive shaft top is connected with rotation platform, described rotary platform upper is connected with stay bearing plate, described lifting table upper left-hand is fixedly connected with column, described column top is provided with the 3rd hinge pillar, described 3rd hinge pillar right side hinge is connected with bracing frame, supporting seat is connected with on the right side of support frame as described above, be connected with lamp bracket on the right side of described supporting seat, on the right side of described lamp bracket, be provided with multiple projection light, the 3rd hydraulic press is provided with on the left of described column, described 3rd hydraulic press top is connected with the 3rd Pneumatic extension bar, described 3rd Pneumatic extension bar top is provided with the 4th hinge pillar, and described 4th hinge pillar right side hinge is connected with pipe link, and described pipe link is connected by hinge with between bracing frame.
2. aircraft component according to claim 1 is ascended a height attending device, and it is characterized in that: the described electro-motor left and right sides is provided with pillar stiffener, described pillar stiffener top is provided with the ball for supporting rotation platform.
3. aircraft component according to claim 1 is ascended a height attending device, it is characterized in that: described supporting seat side is provided with power interface, described power interface is provided with power lead and is connected with projection light.
4. aircraft component according to claim 1 is ascended a height attending device, it is characterized in that: described pedestal bottom is provided with multiple castor for movement.
5. aircraft component according to claim 1 is ascended a height attending device, it is characterized in that: described lifting table bottom is provided with dust exhaustor, described dust exhaustor top is connected with into dirt pipe, describedly enter to be connected with into dirt chamber on the right side of dirt pipe, describedly enter to be connected with multiple sweep-up pipe on the right side of dirt chamber, described in enter dirt pipe and be arranged on lifting table inside.
6. aircraft component according to claim 1 is ascended a height attending device, it is characterized in that: be provided with multiple storage chamber on the right side of described column.
7. aircraft component according to claim 1 is ascended a height attending device, it is characterized in that: described first hydraulic press, the second hydraulic press, the 3rd hydraulic press and electro-motor is provided with signal wire (SW) and is connected with controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520883978.7U CN205076770U (en) | 2015-11-09 | 2015-11-09 | Aircraft part is ascended a height and is maintained device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520883978.7U CN205076770U (en) | 2015-11-09 | 2015-11-09 | Aircraft part is ascended a height and is maintained device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205076770U true CN205076770U (en) | 2016-03-09 |
Family
ID=55429189
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520883978.7U Expired - Fee Related CN205076770U (en) | 2015-11-09 | 2015-11-09 | Aircraft part is ascended a height and is maintained device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205076770U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105671798A (en) * | 2016-03-31 | 2016-06-15 | 安徽颍上县天成印业包装有限公司 | Novel woven bag machine |
| CN114634140A (en) * | 2022-04-13 | 2022-06-17 | 国网汇通金财（北京）信息科技有限公司 | Electric power overhauls device |
-
2015
- 2015-11-09 CN CN201520883978.7U patent/CN205076770U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105671798A (en) * | 2016-03-31 | 2016-06-15 | 安徽颍上县天成印业包装有限公司 | Novel woven bag machine |
| CN114634140A (en) * | 2022-04-13 | 2022-06-17 | 国网汇通金财（北京）信息科技有限公司 | Electric power overhauls device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20160309 Termination date: 20161109 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |