CN209364429U - Aircraft engine maintenance supporting member - Google Patents
Aircraft engine maintenance supporting member Download PDFInfo
- Publication number
- CN209364429U CN209364429U CN201821883593.0U CN201821883593U CN209364429U CN 209364429 U CN209364429 U CN 209364429U CN 201821883593 U CN201821883593 U CN 201821883593U CN 209364429 U CN209364429 U CN 209364429U
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- hydraulic telescopic
- telescopic rod
- groups
- fixedly connected
- sliding
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Abstract
The utility model discloses aircraft engine maintenance supporting members, including pedestal, base top is provided with two groups of sliding slots, two group of first sliding block is equipped in two groups of sliding slots, four group of first sliding block top is fixedly connected with support rod, threaded hole is provided on support rod, sliding sleeve is cased on support rod, there is fixing bolt to pass through on sliding sleeve, fixing bolt and screw hole, the first hydraulic telescopic rod is connected on the inside of sliding sleeve, first hydraulic telescopic rod telescopic end is connected with clamping piece, the second sliding block is equipped in the middle part of sliding slot, the second hydraulic telescopic rod is fixedly connected on two group of second sliding block, second hydraulic telescopic rod top is fixedly connected with support plate, support plate top middle portion is fixedly connected with supporting element, base top is equipped with control panel；The utility model not only structure novel under the double action by clamping piece and supporting element, to the good fixing effect of engine, while can as needed be adjusted convenient for the maintenance to engine the position of clamping piece, use extremely convenient.
Description
Technical field
The utility model relates to aircraft engine maintenance fields, and in particular to aircraft engine maintenance supporting member.
Background technique
Aero-engine (aero-engine), which refers to, provides the engine for the required power that flies for aircraft.Mainly have three
Seed type: piston aviation engine, gas-turbine unit, punching engine.
Aero-engine generally when needing repairing, needs to separate the connection of engine and aircraft/helicopter, then passes through
Aero-engine is removed from piggyback pod, then carries out maintenance work, operation is more troublesome, and cost by lifting or lifting device
It is higher, it is time-consuming and laborious.
Utility model content
The purpose of the utility model is to overcome the above-mentioned problems in the prior art, provide aircraft engine maintenance branch
Component is supportted, not only structure novel, under the double action by clamping piece and supporting element, to the good fixing effect of engine, simultaneously
The position of clamping piece can be adjusted convenient for the maintenance to engine as needed, be used extremely convenient.
To realize above-mentioned technical purpose and the technique effect, the utility model is achieved through the following technical solutions:
Aircraft engine maintenance supporting member, including pedestal, the base top are provided with two groups of sliding slots, sliding slot described in two groups
It is inside equipped with two group of first sliding block, the first sliding block top described in four groups is fixedly connected with support rod, is provided with spiral shell on the support rod
Pit is cased with sliding sleeve on the support rod, is slidably connected between the sliding sleeve and support rod, has fixing bolt to wear on the sliding sleeve
It crosses, the fixing bolt and screw hole, is fixedly connected with the first hydraulic telescopic rod on the inside of the sliding sleeve, described first is hydraulic
Telescopic rod telescopic end is fixedly connected with clamping piece, is equipped with the second sliding block in the middle part of sliding slot described in two groups, the second sliding block described in two groups
On be fixedly connected to the second hydraulic telescopic rod, second hydraulic telescopic rod top is fixedly connected with support plate, the support
Plate top middle portion is fixedly connected with supporting element, and the base top is equipped with control panel.
Further, the base bottom is equipped with idler wheel, has self-locking mechanism on the idler wheel.
Further, the control panel electrically connects between the first hydraulic telescopic rod and the second hydraulic telescopic rod respectively
It connects.
Further, the clamping piece is arc clamping piece.
Further, the supporting element is curved support part, and the inner arc of the curved support part faces upward.
Further, six groups of threaded holes are provided on support rod described in every group.
The income effect of the utility model is:
The utility model not only structure novel, the fixation under the double action by clamping piece and supporting element, to engine
Effect is good, while can as needed be adjusted the position of clamping piece convenient for the maintenance to engine, uses extremely
It is convenient.
Detailed description of the invention
In order to illustrate more clearly of the technical solution of the utility model embodiment, make required for being described below to embodiment
Attached drawing is briefly described, it should be apparent that, the drawings in the following description are merely some embodiments of the present invention,
For those of ordinary skill in the art, without creative efforts, it can also be obtained according to these attached drawings
Other attached drawings.
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model structure diagram；
Fig. 3 is the utility model structure diagram.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without creative efforts
All other embodiment obtained, fall within the protection scope of the utility model.
As shown in Figure 1-3, the utility model is aircraft engine maintenance supporting member, including pedestal 1, opened at the top of pedestal 1
There are two groups of sliding slots 12, two group of first sliding block 14 is equipped in two groups of sliding slots 12, four group of first 14 top of sliding block is fixedly connected with branch
Strut 2 is provided with threaded hole 4 on support rod 2, sliding sleeve 3 is cased on support rod 2, is slidably connected between sliding sleeve 3 and support rod 2, sliding sleeve
There is fixing bolt 5 to pass through on 3, fixing bolt 5 and threaded hole 4 are spirally connected, the first hydraulic telescopic rod 6 is fixedly connected on the inside of sliding sleeve 3,
First hydraulic telescopic rod, 6 telescopic end is fixedly connected with clamping piece 7, is equipped with the second sliding block 15 in the middle part of two groups of sliding slots 12, and two group
The second hydraulic telescopic rod 13 is fixedly connected on two sliding blocks 15,13 top of the second hydraulic telescopic rod is fixedly connected with support plate 8,
8 top middle portion of support plate is fixedly connected with supporting element 10, is equipped with control panel 9 at the top of pedestal 1.
Wherein, 1 bottom of pedestal is equipped with idler wheel 11, self-locking mechanism is had on idler wheel 11, convenient for the movement and fixation of device.
Wherein, control panel 9 is electrically connected between the first hydraulic telescopic rod 6 and the second hydraulic telescopic rod 13 respectively.
Wherein, clamping piece 7 is arc clamping piece 7, and it is more preferable to grip effect.
Wherein, supporting element 10 is curved support part 10, and the inner arc of curved support part 10 faces upward, and support effect is more preferable.
Wherein, six groups of threaded holes 4 are provided on every group of support rod 2, convenient for adjusting the height of clamping piece 7.
One concrete application of the present embodiment are as follows: in use, the height according to locating for engine is different, loosen fixing bolt
5, sliding sleeve 3 can be moved up and down along support rod 2, sliding sleeve 3 drives clamping piece 7 to move up and down by the first hydraulic telescopic rod 6, can
The height of clamping piece 7 is adjusted, after the completion of the height adjustment of clamping piece 7, sliding sleeve 3 is fixed by fixing bolt 5,
The first hydraulic telescopic rod 6 is controlled by control panel 9 to shrink, and increases the distance between corresponding clamping piece 7, by four groups of folders
Gripping member 7 is located at the two sides of engine, and mobile support rod 2 slides the first sliding block 14 in sliding slot 12, and support rod 2 drives
Clamping piece 7 moves together, and clamping piece 7 is avoided to coincide with maintenance position, controls the first hydraulic telescopic rod 6 by control panel 9
Elongation, clamps clamping piece 7 by engine, controls the elongation of the second hydraulic telescopic rod 13 by control panel 9, second hydraulic stretches
Contracting bar 13 drives support plate 8 to move upwards, and supporting element 10 is moved upwardly together with support plate 8, when supporting element 10 and engine
After contact, the second hydraulic telescopic rod 13 of control is no longer moved upwards, and supporting element 10 can play the role of supporting engine, convenient
Maintenance to engine.
To sum up, the utility model not only structure novel, under the double action by clamping piece and supporting element, to engine
Good fixing effect, while the position of clamping piece can be adjusted convenient for the maintenance to engine as needed, it uses
It is extremely convenient.
In the description of this specification, the description of reference term " one embodiment ", " example ", " specific example " etc. means
Specific features described in conjunction with this embodiment or example, structure, material live feature be contained in the utility model at least one
In embodiment or example.In the present specification, schematic expression of the above terms be not necessarily referring to identical embodiment or
Example.Moreover, particular features, structures, materials, or characteristics described can be in any one or more embodiment or examples
In can be combined in any suitable manner.
The preferred embodiment in the utility model disclosed above is only intended to help to illustrate the utility model.Preferred embodiment is simultaneously
There is no the details that detailed descriptionthe is all, also not limiting the utility model is only the specific embodiment.Obviously, according to this theory
The content of bright book can make many modifications and variations.These embodiments are chosen and specifically described to this specification, is in order to preferably
The principles of the present invention and practical application are explained, so that skilled artisan be enable to better understand and utilize this
Utility model.The utility model is limited only by the claims and their full scope and equivalents.
Claims (6)
1. aircraft engine maintenance supporting member, it is characterised in that: including pedestal (1), be provided with two groups of cunnings at the top of the pedestal (1)
Slot (12), sliding slot described in two groups (12) is interior to be equipped with two group of first sliding block (14), and the first sliding block (14) top described in four groups is fixed
It is connected with support rod (2), is provided with threaded hole (4) on the support rod (2), is cased with sliding sleeve (3) on the support rod (2), it is described
It is slidably connected between sliding sleeve (3) and support rod (2), there is fixing bolt (5) to pass through on the sliding sleeve (3), the fixing bolt (5)
It is spirally connected, is fixedly connected with the first hydraulic telescopic rod (6) on the inside of the sliding sleeve (3), first hydraulic telescopic rod with threaded hole (4)
(6) telescopic end is fixedly connected with clamping piece (7), the second sliding block (15) is equipped in the middle part of sliding slot described in two groups (12), described in two groups
It is fixedly connected on second sliding block (15) the second hydraulic telescopic rod (13), the second hydraulic telescopic rod (13) top is fixed to be connected
It is connected to support plate (8), support plate (8) top middle portion is fixedly connected with supporting element (10), and control is equipped at the top of the pedestal (1)
Panel (9) processed.
2. aircraft engine maintenance supporting member according to claim 1, it is characterised in that: pedestal (1) bottom is set
Have idler wheel (11), self-locking mechanism is had on the idler wheel (11).
3. aircraft engine maintenance supporting member according to claim 1, it is characterised in that: the control panel (9) point
It is not electrically connected between the first hydraulic telescopic rod (6) and the second hydraulic telescopic rod (13).
4. aircraft engine maintenance supporting member according to claim 1, it is characterised in that: the clamping piece (7) is arc
Clevis gripping member (7).
5. aircraft engine maintenance supporting member according to claim 1, it is characterised in that: the supporting element (10) is arc
The inner arc of shape supporting element (10), the curved support part (10) faces upward.
6. aircraft engine maintenance supporting member according to claim 1, it is characterised in that: support rod described in every group (2)
On be provided with six groups of threaded holes (4).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821883593.0U CN209364429U (en) | 2018-11-15 | 2018-11-15 | Aircraft engine maintenance supporting member |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201821883593.0U CN209364429U (en) | 2018-11-15 | 2018-11-15 | Aircraft engine maintenance supporting member |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209364429U true CN209364429U (en) | 2019-09-10 |
Family
ID=67837056
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201821883593.0U Active CN209364429U (en) | 2018-11-15 | 2018-11-15 | Aircraft engine maintenance supporting member |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209364429U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114673883A (en) * | 2022-03-22 | 2022-06-28 | 广东电力通信科技有限公司 | Overcurrent monitoring device |
-
2018
- 2018-11-15 CN CN201821883593.0U patent/CN209364429U/en active Active
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114673883A (en) * | 2022-03-22 | 2022-06-28 | 广东电力通信科技有限公司 | Overcurrent monitoring device |
| CN114673883B (en) * | 2022-03-22 | 2023-12-01 | 广东电力通信科技有限公司 | Overcurrent monitoring device |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: No. 30, development avenue, new industrial park, high tech Zone, Xi'an, Shaanxi 710000 Patentee after: Shaanxi Xintai Aviation Technology Co.,Ltd. Address before: No. 30, development avenue, new industrial park, high tech Zone, Xi'an, Shaanxi 710000 Patentee before: SHAANXI SINTEK AVIATION TECHNOLOGIES CO.,LTD. |
|
| CP01 | Change in the name or title of a patent holder |