CN210653675U

CN210653675U - Airplane airborne intelligent power distribution system

Info

Publication number: CN210653675U
Application number: CN201921773277.2U
Authority: CN
Inventors: 武彬; 陈维; 尹泽霖; 陈文章
Original assignee: Jiangxi Rongli Aviation Industry Co ltd
Current assignee: Jiangxi Rongli Aviation Industry Co ltd
Priority date: 2019-10-21
Filing date: 2019-10-21
Publication date: 2020-06-02
Anticipated expiration: 2029-10-21

Abstract

The utility model belongs to the technical field of distribution equipment, in particular to an aircraft onboard intelligent distribution system, which comprises a cabin, wherein the right side of the cabin is provided with a first space, the inner bottom end of the first space is detachably connected with two lower slide rails which are symmetrically distributed, the upper end surfaces of the two lower slide rails are both slidably connected with upper slide rails, the upper end surfaces of the two upper slide rails are provided with a bottom plate, the upper end surface of the first mounting plate is provided with a lifter, the upper end surface of the lifter is provided with a second mounting plate, the upper end surface of the second mounting plate is provided with a transformer, the right side of the bottom plate is provided with a door plate, the right side of the door plate is detachably connected with a handle, the lifter is opened, the lifter drives the second mounting plate to reach the corresponding height, the lifter is closed, then the transformer is checked and maintained, so that the height of the transformer can be conveniently adjusted, the working efficiency of staff and the comfort level during maintenance are improved.

Description

Airplane airborne intelligent power distribution system

Technical Field

The utility model relates to a distribution equipment technical field, concretely relates to aircraft machine carries intelligent power distribution system.

Background

At present, storage batteries are installed on some mobile mechanical equipment, certain electric quantity can be stored in the storage batteries, when the equipment is started or the electric quantity of the equipment is insufficient, electric energy stored in the storage batteries is provided for the equipment to be used after voltage is changed through a transformer, and the power supply mode is widely used on automobiles, ships and airplanes.

The height of the transformer can not be adjusted according to the height of workers when the transformer is maintained and checked, so that the working efficiency of the workers is reduced.

SUMMERY OF THE UTILITY MODEL

For solving the problem that proposes among the above-mentioned background art, the utility model provides an aircraft machine carries intelligent power distribution system has the maintenance and conveniently adjusts the characteristics of transformer height when looking over the transformer.

In order to achieve the above object, the utility model provides a following technical scheme: aircraft machine carries intelligent distribution system, including the cabin, first space has been seted up on the right side of cabin, the inside bottom in first space can be dismantled and be connected with two symmetric distribution's lower slide rail, two the equal sliding connection of up end of slide rail has last slide rail, two go up the up end of slide rail and be provided with the bottom plate, two symmetric distribution's first fluting, two are seted up to the lower terminal surface of bottom plate the up end of going up the slide rail all can be dismantled with first grooved inside top and be connected, the up end of bottom plate can be dismantled and be connected with first mounting panel, the lift is installed to the up end of first mounting panel, the second mounting panel is installed to the up end of lift, the transformer is installed to the up end of second mounting panel, the door plant is installed on the right side of bottom plate, the right side detachable connection of door plant has the handle.

In order to avoid hindering the staff to maintain the transformer among the maintenance process to the up end of parallel placement's door plant makes things convenient for the staff to place maintenance tool, as the utility model discloses aircraft machine carries intelligent distribution system preferred, the up end of bottom plate can be dismantled and is connected with the first installation piece of two symmetric distributions, two first installation piece is located both sides around the first mounting panel, two the equal swing joint in up end of first installation piece has first pivot, two the equal swing joint in right side of first pivot has the cylinder, two the hydraulic stem is all installed to the output of cylinder, two the equal swing joint in right side of hydraulic stem has the second pivot, two the equal swing joint in lower terminal surface of second pivot has the second installation piece, two the lower terminal surface of second installation piece all can be dismantled with the up end of door plant and be connected.

For the weight of convenient supporting baseplate top, avoid the bottom plate to lead to the bottom plate to damage because gravity factor, as the utility model discloses aircraft machine carries intelligent distribution system preferred, the second fluting has been seted up to the lower terminal surface of going up the slide rail, the second fluting is located between two first fluting, the inside top swing joint of second fluting has branch, the kerve has been seted up on the right side of branch.

For the convenience is to the battery electric power storage, as the utility model discloses aircraft machine carries intelligent distribution system preferred, the second space has been seted up on the right side in cabin, the second space is located the top in first space, the battery is installed to the inside bottom in second space, the opening has been seted up between first space and the second space.

In order to avoid the bottom plate to drop from the right side in first space, conduct the utility model discloses aircraft machine carries intelligent distribution system preferred, the right side fixedly connected with stopper of slide rail down.

For the lift of convenient control lift, as the utility model discloses aircraft machine carries intelligent distribution system and is preferred, control switch is installed to the up end of bottom plate, control switch is located the rear end of hydraulic stem, be electric connection between control switch and the lift.

For opening and closing of convenient control cylinder, conduct the utility model discloses aircraft machine carries intelligent distribution system preferred, switch is installed to the up end of bottom plate, switch is located the place ahead of first mounting panel, be electric connection between switch and the cylinder.

In order to dismantle the connection with door plant and bottom plate to make things convenient for the door plant to be located the right side activity of bottom plate, as the utility model discloses aircraft machine carries intelligent distribution system preferred, the up end left side of door plant can be dismantled and be connected with the hinge, the door plant passes through the hinge with the bottom plate and can dismantle the connection.

Compared with the prior art, the beneficial effects of the utility model are that:

1. this kind of aircraft machine carries intelligent power distribution system, when needing to look over and maintain the transformer, the right side in first space is pulled out with the bottom plate to the pulling handle, during the pulling, it slides right from the top of slide rail down to go up the slide rail, the height of maintaining as required after that, open the lift, the lift drives the second mounting panel and reachs corresponding height, close the lift, look over and maintain the transformer after that, thereby the height of conveniently adjusting the transformer according to staff's height when maintaining and looking over the transformer, staff's work efficiency and comfort level when maintaining have been improved.

2. This kind of aircraft machine carries intelligent power distribution system, when needs maintenance transformer, start the cylinder, the cylinder drives the hydraulic stem tensile, until door plant and bottom plate parallel placement to block the staff to maintain the transformer in avoiding the maintenance process, and the up end of the door plant of parallel placement makes things convenient for the staff to place repair tools.

3. This kind of aircraft machine carries intelligent power distribution system, when maintaining, with the inside branch of second fluting pull down to being ninety degrees angles, make the lower extreme of branch place subaerial upper end to reached the convenient weight that supports the bottom plate top of maintenance transformer in-process, avoided the bottom plate to lead to the bottom plate to damage because of gravity factor.

Drawings

The accompanying drawings are included to provide a further understanding of the invention, and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention, and together with the description serve to explain the invention and not to limit the invention.

In the drawings:

fig. 1 is a structural diagram of an airplane airborne intelligent power distribution system of the present invention;

FIG. 2 is a structural diagram of a structure of an airplane airborne intelligent power distribution system of the present invention;

FIG. 3 is a cross-sectional view of the aircraft-mounted intelligent power distribution system of the present invention;

fig. 4 is a bottom view of the bottom plate of the present invention;

fig. 5 is a first mounting block structure diagram of the present invention.

In the figure, 1, the nacelle; 101. a first space; 102. a second space; 103. an opening; 2. a lower slide rail; 201. an upper slide rail; 202. a base plate; 2021. a first slot; 2022. a second slot; 203. a first mounting plate; 204. an elevator; 205. a second mounting plate; 206. a transformer; 3. a door panel; 301. a hinge; 302. a handle; 4. a first mounting block; 401. a first rotating shaft; 402. a cylinder; 403. a hydraulic lever; 404. a second rotating shaft; 405. a second mounting block; 5. a control switch; 6. a strut; 601. groove drawing; 7. a power switch; 8. a storage battery; 9. and a limiting block.

Detailed Description

In order to make the objects, technical solutions and advantages of the present invention more clearly understood, the present invention is further described in detail below with reference to the accompanying drawings and embodiments. It should be understood that the specific embodiments described herein are merely illustrative of the invention and are not intended to limit the invention.

In the description of the present invention, it is to be understood that the terms "length", "width", "upper", "lower", "front", "rear", "left", "right", "vertical", "horizontal", "top", "bottom", "inner", "outer", and the like indicate orientations or positional relationships based on those shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. In addition, in the description of the present invention, "a plurality" means two or more unless specifically limited otherwise.

Referring to fig. 1-5, the present invention provides the following technical solutions: aircraft machine carries intelligent power distribution system, including cabin 1, first space 101 has been seted up on cabin 1's right side, the lower slide rail 2 that is connected with two symmetric distributions can be dismantled to the inside bottom in first space 101, the equal sliding connection of up end of two lower slide rail 2 has last slide rail 201, the up end of two last slide rail 201 is provided with bottom plate 202, two symmetric distributions's first fluting 2021 has been seted up to the lower terminal surface of bottom plate 202, the up end of two last slide rail 201 all can be dismantled with the inside top of first fluting 2021 and be connected, the up end of bottom plate 202 can be dismantled and be connected with first mounting panel 203, lift 204 is installed to the up end of first mounting panel 203, second mounting panel 205 is installed to the up end of lift 204, transformer 206 is installed to the up end of second mounting panel 205, door plant 3 is installed on the right side of bottom plate 202, the right side of door plant.

In the examples: need look over and maintain transformer 206, pulling handle 302 pulls out the right side of first space 101 with bottom plate 202, during the pulling, go up slide rail 201 and slide right from the top of lower slide rail 2, height according to the needs maintenance after that, open lift 204, lift 204 drives second mounting panel 203 and reachs corresponding height, close lift 204, look over and maintain transformer 206 after that, thereby the height of conveniently adjusting transformer 206 according to staff's height when maintaining and looking over transformer 206, the comfort level when staff's work efficiency and maintenance has been improved.

Specifically, the up end of bottom plate 202 can be dismantled and be connected with two symmetric distribution's first installation piece 4, two first installation pieces 4 are located both sides around first mounting panel 203, the equal swing joint in up end of two first installation pieces 4 has first pivot 401, the equal swing joint in right side of two first pivot 401 has cylinder 402, hydraulic stem 403 is all installed to the output of two cylinder 402, the equal swing joint in right side of two hydraulic stem 403 has second pivot 404, the equal swing joint in lower terminal surface of two second pivot 404 has second installation piece 405, the lower terminal surface of two second installation pieces 405 all can be dismantled with the up end of door plant 3 and be connected.

In the examples: when needing to maintain transformer 206, start cylinder 402, cylinder 402 drives hydraulic stem 403 and stretches until door plant 3 and bottom plate 202 parallel placement to block the staff to maintain transformer 206 in avoiding the maintenance process, and the up end of the door plant 3 of parallel placement makes things convenient for the staff to place maintenance tool.

Specifically, the lower end surface of the upper slide rail 201 is provided with a second slot 2022, the second slot 2022 is located between the two first slots 2021, the top end of the inside of the second slot 2022 is movably connected with a supporting rod 6, and the right side of the supporting rod 6 is provided with a pull groove 601.

In the examples: when maintenance is carried out, the supporting rod 6 in the second slot 2022 is pulled downwards to form an angle of ninety degrees, so that the lower end of the supporting rod 6 is placed at the upper end of the ground, the weight above the bottom plate 202 is conveniently supported in the process of maintaining the transformer 206, and the bottom plate 202 is prevented from being damaged due to gravity.

Specifically, a second space 102 is formed on the right side of the nacelle 1, the second space 102 is located above the first space 101, the battery 8 is mounted at the bottom end inside the second space 102, and an opening 103 is formed between the first space 101 and the second space 102.

In the examples: after the maintenance is finished, the handle 302 is pulled to push the door panel 3 to the inside of the first space 101, the storage battery 8 is contacted with the transformer 206 below the opening 103 through the opening 103, and the storage battery 8 is stored, so that the effect of conveniently storing the storage battery 8 is achieved.

Specifically, the right side of the lower slide rail 2 is fixedly connected with a limiting block 9.

In the examples: when the bottom plate 202 is pulled to the right side of the lower slide rail 2, the limiting block 9 prevents the bottom plate 202 from being pulled to the right, so that the bottom plate 202 is prevented from falling off from the right side of the first space 101.

Specifically, the control switch 5 is installed on the upper end surface of the bottom plate 202, the control switch 5 is located at the rear end of the hydraulic rod 403, and the control switch 5 is electrically connected to the elevator 204.

In the examples: the control switch 5 is installed on the upper end surface of the bottom plate 202, and the control switch 5 is pressed to control the lifting of the lifter 204.

Specifically, the power switch 7 is mounted on the upper end surface of the bottom plate 202, the power switch 7 is located in front of the first mounting plate 203, and the power switch 7 is electrically connected to the cylinder 402.

In the examples: the power switch 7 is installed through the upper end surface of the base plate 202, and thus the on and off of the cylinder 402 is conveniently controlled by pressing the power switch 7.

Specifically, hinge 301 is detachably connected to the left side of the upper end face of door panel 3, and door panel 3 and bottom plate 202 are detachably connected through hinge 301.

In this embodiment: hinge 301 of connection can be dismantled through the up end left side of door plant 3, and then can dismantle door plant 3 and bottom plate 202 through hinge 301 and be connected to make things convenient for door plant 3 to be located the right side activity of bottom plate 202.

The utility model discloses a theory of operation and use flow: in the using process, when the transformer 206 needs to be checked and maintained, the handle 302 is pulled to pull the bottom plate 202 out of the right side of the first space 101, when the upper sliding rail 201 slides rightwards from the upper side of the lower sliding rail 2, when the bottom plate 202 is pulled to the right side of the lower sliding rail 2, the limiting block 9 prevents the bottom plate 202 from continuously pulling rightwards, then the control switch 5 is pressed to open the elevator 204 according to the height to be maintained, the elevator 204 drives the second mounting plate 203 to reach the corresponding height, the control switch 5 is pressed to close the elevator 204, then the transformer 206 is checked and maintained, when the transformer 206 needs to be maintained, the power switch 7 is pressed to start the air cylinder 402, the air cylinder 402 drives the hydraulic rod 403 to stretch until the door panel 3 and the bottom plate 202 are placed in parallel, the upper end face of the door panel 3 placed in parallel is convenient for a worker to place a maintenance tool, and then the strut 6 in the second slot 2022, the lower end of the support rod 6 is placed on the upper end of the ground, and after the maintenance is finished, the handle 302 is pulled to push the door panel 3 into the first space 101, so that the storage battery 8 is in contact with the transformer 206 below the opening 103 through the opening 103, and the storage battery 8 is charged.

The above description is only exemplary of the present invention and should not be construed as limiting the present invention, and any modifications, equivalents and improvements made within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims

1. Aircraft machine carries intelligent power distribution system, including cabin (1), its characterized in that: the right side of the cabin (1) is provided with a first space (101), the bottom end in the first space (101) is detachably connected with two lower sliding rails (2) which are symmetrically distributed, the upper end faces of the two lower sliding rails (2) are both slidably connected with upper sliding rails (201), the upper end faces of the two upper sliding rails (201) are provided with a bottom plate (202), the lower end face of the bottom plate (202) is provided with two first slots (2021) which are symmetrically distributed, the upper end faces of the two upper sliding rails (201) are both detachably connected with the top end in the first slot (2021), the upper end face of the bottom plate (202) is detachably connected with a first mounting plate (203), the upper end face of the first mounting plate (203) is provided with a lifter (204), the upper end face of the lifter (204) is provided with a second mounting plate (205), the upper end face of the second mounting plate (205) is provided with a transformer (206), the door panel (3) is installed on the right side of the bottom plate (202), and a handle (302) is detachably connected to the right side of the door panel (3).

2. An intelligent power distribution system on-board an aircraft as defined in claim 1, wherein: the up end of bottom plate (202) can be dismantled and be connected with first installation piece (4) of two symmetric distributions, two first installation piece (4) are located both sides around first mounting panel (203), two the equal swing joint in up end of first installation piece (4) has first pivot (401), two the equal swing joint in right side of first pivot (401) has cylinder (402), two hydraulic stem (403) are all installed to the output of cylinder (402), two the equal swing joint in right side of hydraulic stem (403) has second pivot (404), two the equal swing joint in lower terminal surface of second pivot (404) has second installation piece (405), two the lower terminal surface of second installation piece (405) all can be dismantled with the up end of door plant (3) and be connected.

3. An intelligent power distribution system on-board an aircraft as defined in claim 1, wherein: the lower end face of the upper sliding rail (201) is provided with a second open slot (2022), the second open slot (2022) is located between the two first open slots (2021), the top end of the inner part of the second open slot (2022) is movably connected with a supporting rod (6), and the right side of the supporting rod (6) is provided with a pull slot (601).

4. An intelligent power distribution system on-board an aircraft as defined in claim 1, wherein: a second space (102) is formed in the right side of the engine room (1), the second space (102) is located above the first space (101), a storage battery (8) is mounted at the bottom end of the interior of the second space (102), and an opening (103) is formed between the first space (101) and the second space (102).

5. An intelligent power distribution system on-board an aircraft as defined in claim 1, wherein: the right side of the lower sliding rail (2) is fixedly connected with a limiting block (9).

6. An intelligent power distribution system on-board an aircraft as defined in claim 2, wherein: the lifting device is characterized in that a control switch (5) is installed on the upper end face of the bottom plate (202), the control switch (5) is located at the rear end of the hydraulic rod (403), and the control switch (5) is electrically connected with the lifter (204).

7. An intelligent power distribution system on-board an aircraft as defined in claim 2, wherein: power switch (7) are installed to the up end of bottom plate (202), power switch (7) are located the place ahead of first mounting panel (203), be electric connection between power switch (7) and cylinder (402).

8. An intelligent power distribution system on-board an aircraft as defined in claim 1, wherein: hinge (301) can be dismantled and be connected in the up end left side of door plant (3), door plant (3) can be dismantled through hinge (301) with bottom plate (202) and be connected.