CN110645467A

CN110645467A - Novel aircraft bonnet that can slide and turn to

Info

Publication number: CN110645467A
Application number: CN201911035528.1A
Authority: CN
Inventors: 余立冬
Original assignee: Jiangsu Pengfei Automation Machinery Co Ltd
Current assignee: Jiangsu Pengfei Automation Machinery Co Ltd
Priority date: 2019-10-29
Filing date: 2019-10-29
Publication date: 2020-01-03
Anticipated expiration: 2039-10-29
Also published as: CN110645467B

Abstract

The invention discloses a novel engine cover capable of sliding and steering, which comprises an equipment main body and a guide rail arranged on the upper surface of the equipment main body, wherein a split engine cover is connected on the guide rail in a sliding manner, the split engine covers are connected with each other through a connecting mechanism, the connecting mechanism comprises a connecting rod, a sliding groove and a sliding column, one end of the connecting rod is fixedly connected with one end of the split engine cover, the sliding groove is formed in the other end of the connecting rod, the sliding column is fixed on the side surface of one end of the split engine cover, and the sliding column is arranged in the sliding groove in a sliding manner; the invention divides the hood into a plurality of split hoods, which are connected through the connecting mechanism, when the hood is opened, the raised hood can be turned to be attached to the surface of one end of the equipment, and the phenomenon that the opening and the surrounding movement of the hood are influenced because the hood is too much projected is prevented.

Description

Novel aircraft bonnet that can slide and turn to

Technical Field

The invention belongs to the technical field of hoods, and particularly relates to a novel hood capable of sliding and steering.

Background

The machine cover is used for protecting internal parts of the machine from being corroded and damaged by the outside, and the machine tool cover is divided into an inner protection part and an outer protection part. The steel plate and the stainless steel protective cover have the characteristics of good sealing, iron filings prevention, cooling liquid prevention, tool accident prevention, firmness, durability, attractive appearance and the like.

When an existing hood is used, the problem that the hood is inconvenient to open or the surrounding walking is affected due to the fact that the protruding part of the hood occupies space when the hood is opened is solved, and therefore a novel hood capable of sliding and steering is provided.

Disclosure of Invention

The invention aims to provide a novel hood capable of sliding and steering, and aims to solve the problem that when the existing hood proposed in the background art is used, the hood is opened, the protruding part of the hood occupies space, so that the hood is inconvenient to open or the surrounding walking is influenced.

In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides a novel aircraft bonnet that can slide and turn to, includes the equipment main part and installs the guide rail at the equipment main part upper surface, sliding connection has the components of a whole that can function independently aircraft bonnet on the guide rail, connect through coupling mechanism between the components of a whole that can function independently aircraft bonnet, coupling mechanism includes connecting rod, sliding tray and sliding column, the one end of connecting rod and the one end fixed connection of components of a whole that can function independently aircraft bonnet, the other end at the connecting rod is seted up to the sliding tray, the sliding column is fixed in the one end side of components of a whole that can function independently aircraft bonnet.

Preferably, the inside buffer gear that is provided with of components of a whole that can function independently aircraft bonnet, buffer gear includes spring A, dashpot, catch plate, spring B and diversion slider, the dashpot is seted up in the inside of components of a whole that can function independently aircraft bonnet, catch plate fixed mounting is at the inboard top of dashpot, the downside at the catch plate is installed to spring B, spring B's both ends respectively with catch plate and the inboard bottom fixed connection of dashpot, spring A fixed mounting is on the both ends inner wall of dashpot, diversion slider fixed mounting is in spring A's one end, and diversion slider and dashpot sliding connection.

Preferably, the contact surfaces of the turning sliding block and the two ends of the pushing plate are both inclined surfaces.

Preferably, a reinforcing rod is fixedly connected to the inner side of the split hood, the position of the reinforcing rod corresponds to that of the pushing plate, and two ends of the reinforcing rod are inserted into the split hood.

Preferably, the two ends of the upper surface of the equipment main body are provided with limiting rods corresponding to the positions of the guide rails, and the lower ends of the limiting rods are rotatably connected with the equipment main body through damping rotating shafts.

Preferably, a protrusion is arranged at one end of the split hood, a groove is formed in the other end of the split hood, and the split hoods are clamped through the protrusion and the groove.

Preferably, a pulling handle is provided on an upper surface of an end portion of the split hood.

Compared with the prior art, the invention has the beneficial effects that: (1) the invention divides the hood into a plurality of split hoods, which are connected through the connecting mechanism, when the hood is opened, the raised hood can be turned to be attached to the surface of one end of the equipment, and the phenomenon that the opening and the surrounding movement of the hood are influenced because the hood is too much projected is prevented. (2) Through the buffer gear who designs, when the aircraft bonnet received external force and assaulted, components of a whole that can function independently aircraft bonnet both ends supported the buffering through equipment main part, and the unsettled position in components of a whole that can function independently aircraft bonnet middle part is through buffer gear's spring buffering, makes the better impact that bears of aircraft bonnet prevent damaging.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic view of the hood opening configuration of the present invention;

FIG. 3 is a cross-sectional view of the hood of the present invention;

in the figure: 1. an apparatus main body; 2. a guide rail; 3. a split hood; 4. a connecting rod; 5. a sliding groove; 6. a sliding post; 7. a limiting rod; 8. a spring A; 9. a buffer tank; 10. a push plate; 11. a spring B; 12. a reinforcing bar; 13. a direction-changing slide block.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides a technical solution: a novel engine cover capable of sliding and steering comprises an equipment main body 1 and a guide rail 2 arranged on the upper surface of the equipment main body 1, wherein a split engine cover 3 is connected on the guide rail 2 in a sliding way, the split engine covers 3 are connected through a connecting mechanism, the connecting mechanism comprises a connecting rod 4, a sliding groove 5 and a sliding column 6, one end of the connecting rod 4 is fixedly connected with one end of the split engine cover 3, the sliding groove 5 is arranged at the other end of the connecting rod 4, the sliding column 6 is fixed on one end side surface of the split engine cover 3, and the sliding column 6 is arranged in the sliding groove 5 in a sliding way, when the split hood 3 is opened, the split hood 3 is pushed to slide on the guide rails 2, and when one end of the split hood 3 protrudes out of the equipment main body 1, the convex split hood 3 is rotated through the connection of the connecting rod 4 and the sliding column 6, so that the convex split hood 3 is turned to be attached to the equipment main body 1, and the situation that the hood is opened and personnel are influenced to walk due to the excessive convex influence of the split hood 3 is prevented.

In this embodiment, preferably, a buffering mechanism is disposed inside the split hood 3, the buffering mechanism includes a spring A8, a buffering slot 9, a pushing plate 10, a spring B11 and a direction-changing slider 13, the buffering slot 9 is disposed inside the split hood 3, the pushing plate 10 is fixedly mounted at the top of the inner side of the buffering slot 9, a spring B11 is mounted at the lower side of the pushing plate 10, two ends of a spring B11 are fixedly connected with the pushing plate 10 and the bottom of the inner side of the buffering slot 9, a spring A8 is fixedly mounted on the inner walls of two ends of the buffering slot 9, the direction-changing slider 13 is fixedly mounted at one end of the spring A8, the direction-changing slider 13 is slidably connected with the buffering slot 9, the pushing plate 10 moves down to compress a spring B11 when the split hood 3 is stressed, a certain buffering is performed by the elastic force of the spring B11, and the direction-changing slider 13 is pushed by two ends of the pushing plate 10 to slide, so that, the buffering effect of the buffering mechanism is better.

In this embodiment, preferably, the contact surfaces of the direction-changing slider 13 and the two ends of the pushing plate 10 are both provided with inclined surfaces, so that the direction-changing slider 13 is conveniently pushed to slide and press the spring A8 when the pushing plate 10 moves downwards under force.

In this embodiment, preferably, the reinforcing rod 12 is fixedly connected to the inner side of the split hood 3, the position of the reinforcing rod 12 corresponds to the position of the pushing plate 10, and the two ends of the reinforcing rod 12 are inserted into the split hood 3, so that the supporting strength of the split hood 3 is higher, and the buffer mechanism is convenient to replace and buffer.

In this embodiment, preferably, the two ends of the upper surface of the device main body 1 are provided with the limiting rods 7 corresponding to the positions of the guide rails 2, the lower ends of the limiting rods 7 are rotatably connected with the device main body 1 through the damping rotating shafts, and the split hood 3 is conveniently positioned when being opened and closed by the blocking of the limiting rods 7.

In this embodiment, preferably, a protrusion is disposed at one end of the split hood 3, a groove is disposed at the other end of the split hood 3, and the split hood 3 is engaged with the protrusion and the groove, so that the split hood 3 is more conveniently connected.

In this embodiment, preferably, a pulling handle is disposed on an upper surface of an end portion of the split hood 3, so as to facilitate the pulling of the split hood 3 to slide on the guide rail 2.

The working principle and the using process of the invention are as follows: after the split hood 3 is installed, firstly, the installation fixing and the safety protection of the split hood are checked, then the split hood can be used, when the split hood 3 is opened, the split hood 3 is pushed to slide on the guide rail 2, when one end of the split hood 3 protrudes out of the equipment main body 1, the protruded split hood 3 is rotated through the connection of the connecting rod 4 and the sliding column 6, the protruded split hood 3 is enabled to be turned to be attached to the equipment main body 1, the split hood 3 is prevented from being protruded too much to influence the opening of the hood and influence the walking of personnel, when the split hood 3 is stressed, the edge is supported and buffered through the guide rail 2 and the equipment main body 1, the middle part is buffered through the buffering mechanism, when the split hood 3 is stressed, the push plate 10 moves downwards to compress the spring B11, certain buffering is performed through the elastic force of the spring B11, meanwhile, the two ends of the push plate 10 push the direction-changing slide block 13 to slide, the buffering effect of the buffering mechanism is better through the elastic force auxiliary buffering of the spring A8, so that the use process of the invention is completed.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a novel aircraft bonnet that can slide and turn to, includes equipment main part (1) and installs guide rail (2) at equipment main part (1) upper surface, its characterized in that: sliding connection has components of a whole that can function independently aircraft bonnet (3) on guide rail (2), connect through coupling mechanism between components of a whole that can function independently aircraft bonnet (3), coupling mechanism includes connecting rod (4), sliding tray (5) and sliding column (6), the one end of connecting rod (4) and the one end fixed connection of components of a whole that can function independently aircraft bonnet (3), the other end at connecting rod (4) is seted up in sliding tray (5), the one end side at components of a whole that can function independently aircraft bonnet (3) is fixed in sliding column (6), and sliding column (6) slidable mounting is in sliding tray (5).

2. The novel slip steerable hood according to claim 1, characterized in that: the utility model discloses a novel engine, including components of a whole that can function independently aircraft bonnet (3), components of a whole that can function independently aircraft bonnet (3) inside is provided with buffer gear, buffer gear includes spring A (8), dashpot (9), catch plate (10), spring B (11) and diversion slider (13), the inside in components of a whole that can function independently aircraft bonnet (3) is seted up in dashpot (9), catch plate (10) fixed mounting is at the inboard top of dashpot (9), the downside at catch plate (10) is installed in spring B (11), the both ends of spring B (11) respectively with catch plate (10) and the inboard bottom fixed connection of dashpot (9), spring A (8) fixed mounting is on the both ends inner wall of dashpot (9), diversion slider (13) fixed mounting is in the one end of spring A (8), and diversion slider (13) and dashpot (9) sliding connection.

3. A novel slip steerable hood as in claim 2 wherein: the contact surfaces of the turning sliding block (13) and the two ends of the pushing plate (10) are both inclined surfaces.

4. A novel slip steerable hood as in claim 2 wherein: the inner side of the split hood (3) is fixedly connected with a reinforcing rod (12), the position of the reinforcing rod (12) corresponds to the position of the pushing plate (10), and two ends of the reinforcing rod (12) are inserted into the split hood (3).

5. The novel slip steerable hood according to claim 1, characterized in that: the device is characterized in that limiting rods (7) are arranged at the two ends of the upper surface of the device body (1) corresponding to the positions of the guide rails (2), and the lower ends of the limiting rods (7) are rotatably connected with the device body (1) through damping rotating shafts.

6. The novel slip steerable hood according to claim 1, characterized in that: the novel engine is characterized in that a protrusion is arranged at one end of the split engine cover (3), a groove is formed in the other end of the split engine cover (3), and the split engine cover (3) is clamped through the protrusion and the groove.

7. The novel slip steerable hood according to claim 1, characterized in that: and a pulling handle is arranged on the upper surface of the end part of the split hood (3).