CN217201742U - Light-duty hard arm guiding mechanism of aeroengine single track - Google Patents
Light-duty hard arm guiding mechanism of aeroengine single track Download PDFInfo
- Publication number
- CN217201742U CN217201742U CN202220920838.2U CN202220920838U CN217201742U CN 217201742 U CN217201742 U CN 217201742U CN 202220920838 U CN202220920838 U CN 202220920838U CN 217201742 U CN217201742 U CN 217201742U
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- connecting plate
- fixedly connected
- light
- clamp
- aeroengine
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T30/00—Transportation of goods or passengers via railways, e.g. energy recovery or reducing air resistance
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- Carriers, Traveling Bodies, And Overhead Traveling Cranes (AREA)
Abstract
The utility model discloses a single-rail light hard arm guiding mechanism of an aeroengine, which comprises a clamp and a connecting plate; two at least guide bars of vertical fixedly connected with on the connecting plate, vertical swing joint has the direction bearing on the guide bar, fixedly connected with movable plate on the direction bearing, anchor clamps rotate the below of connecting at the movable plate, the utility model discloses a promote the direction, solve the pure steel wire of intelligent lifting machine and lift by crane the free problem of rocking of this type of soft cable structure, the better operation position of article is transplanted to the control below.
Description
Technical Field
The utility model relates to an aeroengine technical field specifically is a single track light-duty hard arm guiding mechanism of aeroengine.
Background
An aircraft engine is a highly complex and precise thermal machine that provides the power required for flight of an aircraft. The heart of the airplane is known as 'industrial flower', which directly affects the performance, reliability and economy of the airplane and is an important embodiment of national science and technology, industry and national defense strength.
However, the workpiece is lifted by the steel wire rope or the ring chain hoist of the traditional lifting equipment, and the soft rope type shaking is large; or the guide mechanism is larger, and the running resistance of the fixed rail of the equipment is increased.
SUMMERY OF THE UTILITY MODEL
An object of the utility model is to provide a single-rail light-duty hard arm guiding mechanism of aeroengine to solve the problem that proposes in the above-mentioned background art.
In order to achieve the above purpose, the utility model provides a following technical scheme:
a monorail light hard arm guide mechanism of an aircraft engine comprises a clamp and a connecting plate;
the clamp is characterized in that at least two guide rods are vertically and fixedly connected to the connecting plate, guide bearings are vertically and movably connected to the guide rods, a moving plate is fixedly connected to the guide bearings, and the clamp is rotatably connected to the lower portion of the moving plate.
As a further aspect of the present invention: the lower surface of the movable plate is rotatably connected with a turntable, and the turntable is fixedly connected with the clamp.
As a further aspect of the present invention: the lifting machine is fixedly connected to the connecting plate, a soft rope is fixedly connected to the output end of the lifting machine, and the lower end of the soft rope is fixedly connected with the moving plate.
As a further aspect of the present invention: the connecting plate is movably connected below the horizontal section of the bracket.
As a further aspect of the present invention: the horizontal section fixedly connected with track of support, swing joint has the track coaster in the track, the track coaster is installed on the top of connecting plate.
Compared with the prior art, the beneficial effects of the utility model are that: the utility model is mainly used for solving the problem that the flexible cable lifting appliance is difficult to handle and control due to large shaking in the using process; the double-track guide hard arm is heavy in self and high in pushing resistance, is suitable for carrying and lifting workpieces in 50kg, and achieves the functions of easy push-pull and small stable shaking.
The utility model discloses a two track coasters walk in the track, and inside the equipment focus was changeed the wheel, bottom join in marriage R and support so that connect relevant anchor clamps to the gyration carousel.
Through the promotion direction, solve the free problem of rocking of the soft cable structure of intelligent lifting machine pure wire lifting type, the operation position of article is transplanted to better control below.
Drawings
FIG. 1 is a schematic view of a monorail light-weight hard arm guide mechanism of an aircraft engine;
FIG. 2 is a schematic diagram of a connecting plate, a clamp and a track pulley in a monorail light-weight hard-arm guide mechanism of an aircraft engine;
FIG. 3 is a schematic diagram I of a connecting plate and a track pulley in a monorail light-weight hard arm guide mechanism of an aero-engine;
FIG. 4 is a schematic diagram II of a connecting plate and a track pulley in a monorail light-weight hard arm guide mechanism of an aero-engine;
in the figure: 1. a clamp; 2. a connecting plate; 3. a guide bar; 4. a guide bearing; 5. moving the plate; 6. a turntable; 7. a hoist; 8. soft cables; 9. a support; 10. a track; 11. a track pulley.
Detailed Description
The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.
Referring to fig. 1-4, in an embodiment of the present invention, a single-rail light hard arm guiding mechanism for an aircraft engine includes a clamp 1 and a connecting plate 2;
at least two guide rods 3 are vertically and fixedly connected to the connecting plate 2, guide bearings 4 are vertically and movably connected to the guide rods 3, a moving plate 5 is fixedly connected to the guide bearings 4, and the clamp 1 is rotatably connected to the lower portion of the moving plate 5.
The lower surface of the moving plate 5 is rotatably connected with a turntable 6, the turntable 6 is fixedly connected with the clamp 1, the clamp 1 is conveniently rotated below the connecting plate 2 through the turntable 6, so that the direction of the clamp 1 is adjusted, and the clamp 1 is conveniently clamped with an aero-engine.
Fixedly connected with lifting machine 7 on connecting plate 2, the output fixedly connected with soft cable 8 of lifting machine 7, the lower extreme and the movable plate 5 fixed connection of soft cable 8, lifting machine 7 work realizes soft cable 8 rebound, realize movable plate 5 rebound at the in-process of soft cable 8 rebound, because connecting plate 5 and guide bearing 4 fixed connection, and guide bearing 4 swing joint is in the outside of guide bar 3, consequently, realize the direction limiting displacement to connecting plate 5 through the effect of guide bearing 4 and guide bar 3, only allow connecting plate 5 rebound promptly, also prevent simultaneously that connecting plate 5 from rocking, further guarantee that anchor clamps 1 only allows connecting plate 5 rebound, also prevent simultaneously that anchor clamps 1 from rocking.
The device also comprises a bracket 9, and the connecting plate 2 is movably connected below the horizontal section of the bracket 9.
Support 9's horizontal segment fixedly connected with track 10, swing joint has track coaster 11 in the track 10, and track coaster 11 is installed on the top of connecting plate 2, realizes through track coaster 11 and track 10's cooperation that connecting plate 2 removes in support 9 horizontal segment below, when pressing from both sides aeroengine tightly through anchor clamps 1, track coaster 11 removes on track 10 to realize aeroengine and remove at the horizontal direction, reach the purpose of carrying aeroengine.
The utility model discloses when using, be convenient for realize through setting up of carousel 6 that anchor clamps 1 rotates in 2 below of connecting plate to adjusted anchor clamps 1's direction, be convenient for press from both sides aeroengine with anchor clamps 1 tight.
The hoist 7 works to realize the upward movement of the soft rope 8, the upward movement of the movable plate 5 is realized in the upward movement process of the soft rope 8, the connecting plate 5 is fixedly connected with the guide bearing 4, and the guide bearing 4 is movably connected to the outer side of the guide rod 3, so that the guide limiting effect on the connecting plate 5 is realized through the action of the guide bearing 4 and the guide rod 3, namely, only the connecting plate 5 is allowed to move upwards, meanwhile, the connecting plate 5 is prevented from shaking, the fixture 1 is further ensured to only allow the connecting plate 5 to move upwards, and meanwhile, the fixture 1 is prevented from shaking.
The scheme is mainly used for solving the problems that the soft cable lifting appliance is difficult to handle and control due to large shaking in the using process; the double-track guide hard arm is heavy in self and high in pushing resistance, is suitable for carrying and lifting workpieces in 50kg, and achieves the functions of easy push-pull and small stable shaking.
The connection plate 2 moves below the horizontal section of the support 9 through the matching of the rail pulley 11 and the rail 10, and when the aero-engine is clamped through the clamp 1, the rail pulley 11 moves on the rail 10, so that the aero-engine moves in the horizontal direction, and the purpose of carrying the aero-engine is achieved.
"fixedly connected" as described in the present invention means that two parts connected to each other are fixed together, typically by welding, screwing or gluing; "rotationally coupled" means that two components are coupled together and capable of relative motion.
Although the present description is described in terms of embodiments, not every embodiment includes only a single embodiment, and such description is for clarity only, and those skilled in the art should be able to integrate the description as a whole, and the embodiments can be appropriately combined to form other embodiments as will be understood by those skilled in the art.
Therefore, the above description is only a preferred embodiment of the present application, and is not intended to limit the scope of the present application; all changes which come within the meaning and range of equivalency of the claims are to be embraced within their scope.
Claims (5)
1. A monorail light hard arm guide mechanism of an aircraft engine comprises a clamp (1) and is characterized by further comprising a connecting plate (2);
the clamp is characterized in that at least two guide rods (3) are vertically and fixedly connected to the connecting plate (2), guide bearings (4) are vertically and movably connected to the guide rods (3), a movable plate (5) is fixedly connected to the guide bearings (4), and the clamp (1) is rotatably connected to the lower portion of the movable plate (5).
2. The light-weight hard arm guide mechanism of the monorail of the claim 1 is characterized in that a rotary table (6) is rotatably connected to the lower surface of the moving plate (5), and the rotary table (6) is fixedly connected with the clamp (1).
3. The light-weight hard arm guide mechanism of the monorail of claim 1, characterized in that a hoisting machine (7) is fixedly connected to the connecting plate (2), a soft rope (8) is fixedly connected to the output end of the hoisting machine (7), and the lower end of the soft rope (8) is fixedly connected to the moving plate (5).
4. A light-weight stiff arm guide mechanism for an aircraft engine monorail according to claim 1, characterized in that it further comprises a bracket (9), said connecting plate (2) being articulated below the horizontal section of the bracket (9).
5. A light-weight hard arm guide mechanism of an aircraft engine monorail, as defined in claim 4, characterized in that the horizontal section of the bracket (9) is fixedly connected with a rail (10), a rail trolley (11) is movably connected in the rail (10), and the rail trolley (11) is installed on the top end of the connecting plate (2).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202220920838.2U CN217201742U (en) | 2022-04-20 | 2022-04-20 | Light-duty hard arm guiding mechanism of aeroengine single track |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN202220920838.2U CN217201742U (en) | 2022-04-20 | 2022-04-20 | Light-duty hard arm guiding mechanism of aeroengine single track |
Publications (1)
Publication Number | Publication Date |
---|---|
CN217201742U true CN217201742U (en) | 2022-08-16 |
Family
ID=82774462
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN202220920838.2U Active CN217201742U (en) | 2022-04-20 | 2022-04-20 | Light-duty hard arm guiding mechanism of aeroengine single track |
Country Status (1)
Country | Link |
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CN (1) | CN217201742U (en) |
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2022
- 2022-04-20 CN CN202220920838.2U patent/CN217201742U/en active Active
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