Small-thrust high-stability closed turbine

Abstract

The utility model discloses a low-thrust high-stability closed turbine which comprises a turbine body, a protection assembly is movably installed on the front face of the turbine body, a dust cover is movably installed on the surface of the protection assembly, the protection assembly comprises a protection cover, a center block is arranged in the center of the protection cover, and a dust cover is movably installed on the surface of the protection assembly. A plurality of sets of connecting rods are arranged on the inner wall of the protective cover, the ends of the connecting rods are connected with the side face of the center block, a plurality of sets of butt joint holes are formed in the edges of the two faces of a shell of the turbine body, a plurality of sets of connecting columns are fixedly connected to the edge of the back face of the protective cover, and connecting plates are arranged at the ends of the connecting columns. Strong magnets are arranged in the connecting plates and the butt joint holes. Through the arrangement of the protection assembly, adsorption and butt joint are achieved through a powerful magnet, stability is high, when the turbine body is impacted by external force, the protection cover can make contact with a sponge strip, and the turbine body can be well protected in cooperation with energy absorption and shock absorption of a buffer spring.

Description

Technical Field

[0001] The utility model relates to the technical field of closed turbines, in particular to a closed turbine with low thrust and high stability. Background Art

[0002] A closed turbine, usually refers to a closed turbocharger system, which is a fan in a car or aircraft engine. It is a power machine that converts fluid energy into mechanical energy to generate thrust. It has better operating stability and higher work efficiency.

[0003] The existing technology has the following problems:

[0004] In the prior art, there are generally no protective facilities on the outside of the closed turbine, which means that if some birds or other objects accidentally enter the inside and cause damage to it, it will bring certain safety hazards to the flight of the aircraft. Utility Model Content

[0005] In view of the problems in the related technology, the utility model proposes a small thrust and high stability closed turbine to overcome the above technical problems existing in the existing related technology.

[0006] To this end, the specific technical solutions adopted by the utility model are as follows:

[0007] A small-thrust, high-stability closed turbine comprises a turbine body, a protective assembly is movably mounted on the front of the turbine body, a dust cover is movably mounted on the surface of the protective assembly, the protective assembly comprises a protective cover, a center block is arranged at the center of the protective cover, a plurality of groups of connecting rods are arranged on the inner wall of the protective cover, and the ends of the connecting rods are interconnected with the sides of the center block.

[0008] Preferably, a plurality of docking holes are provided at the edges of both sides of the shell of the turbine body, a plurality of connecting columns are fixedly connected at the back edge of the protective cover, connecting plates are provided at the ends of the connecting columns, strong magnets are provided inside the connecting plates and the docking holes, and the connecting columns are inserted into the docking holes and installed by adsorption of strong magnets, thereby ensuring the installation stability of the protective cover.

[0009] Preferably, a buffer spring is fixedly connected to the top of the connecting plate, and the top of the buffer spring is connected to the bottom of the connecting column. The buffer spring can achieve a good energy absorption effect when the protective cover is subjected to external impact, thereby helping to protect the turbine body.

[0010] Preferably, an insertion rod is fixedly connected to the back edge of the dust cover, and a socket is provided at the front edge of the protective cover. The dust cover and the protective cover can be movably connected to each other through the provided insertion rod and socket, and are convenient for assembly and disassembly.

[0011] Preferably, handles are fixedly connected to both sides of the protective cover, and a protrusion is provided on the front side of the dust cover. The handles and the protrusion make it easy for people to disassemble the protective cover and the dust cover.

[0012] Preferably, sponge strips are bonded to the front edge of the turbine body. There are six groups of sponge strips, which are arranged in a circular array on the surface of the turbine body. Through the provision of sponge strips, the protective cover will preferentially contact the sponge strips after being subjected to external impact force, and combined with the energy absorption and shock absorption of the buffer spring, it can provide further protection for the turbine body.

[0013] Preferably, the bottom of the turbine body is fixedly connected to a box body, the inner wall of the box body is provided with a damping shaft, the end of the damping shaft is fixedly connected to a rectangular block, the surface of the rectangular block is fixedly connected to a support plate, the surface of the support plate is bonded with an anti-slip pad, and the rectangular block is driven to flip into a vertical state through the damping shaft through the provided support plate, so that the turbine body is placed vertically, which is convenient for people to inspect and maintain the interior of the turbine body, and also avoids wear and tear caused by direct contact with the ground when the turbine body is not in use.

[0014] The beneficial effects of the utility model are:

[0015] 1. This small-thrust, high-stability closed turbine has a protective component that is adsorbed and docked by a strong magnet, and has high stability. When the turbine body is impacted by external force, the protective cover will first contact the sponge strip, and cooperate with the energy absorption and shock absorption of the buffer spring to provide good protection for the turbine body.

[0016] 2. The small-thrust, high-stability closed turbine drives the rectangular block to flip into a vertical state through the damping shaft through the support plate, so that the turbine body can be placed vertically, which is convenient for people to inspect the inside of the turbine body and also avoids the turbine body from directly contacting the ground when not in use, which may cause wear. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] In order to more clearly illustrate the embodiments of the utility model or the technical solutions in the prior art, the drawings required for use in the embodiments will be briefly introduced below. Obviously, the drawings described below are only some embodiments of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0018] Figure 1 It is a schematic diagram of the connection structure between the turbine body, the protection assembly and the dust cover of the utility model;

[0019] Figure 2 This is a schematic diagram of the overall structure of the protection component of the utility model;

[0020] Figure 3 This is a schematic diagram of the bottom structure of the turbine body of the utility model;

[0021] Figure 4 This is a schematic diagram of the front structure of the turbine body of the utility model.

[0022] In the figure: 1. turbine body; 2. protection assembly; 201. protection cover; 202. connecting column; 203. buffer spring; 204. connecting plate; 205. handle; 206. socket; 3. dust cover; 4. box body; 5. damping shaft; 6. rectangular block; 7. support plate; 8. sponge strip; 9. docking hole; 10. strong magnet; 11. bump; 12. plug rod. DETAILED DESCRIPTION

[0023] To further illustrate each embodiment, the present invention provides drawings, which are part of the disclosure of the present invention and are mainly used to illustrate the embodiments. They can be used in conjunction with the relevant descriptions in the specification to explain the operating principles of the embodiments. With reference to these contents, ordinary technicians in the field should be able to understand other possible implementation methods and advantages of the present invention. The components in the figures are not drawn to scale, and similar component symbols are generally used to represent similar components.

[0024] According to an embodiment of the utility model, a closed turbine with low thrust and high stability is provided.

[0025] Embodiment 1;

[0026] like Figure 1-Figure 4 As shown, a small-thrust, high-stability closed turbine according to an embodiment of the utility model includes a turbine body 1, a protective component 2 is movably installed on the front of the turbine body 1, a dust cover 3 is movably installed on the surface of the protective component 2, the protective component 2 includes a protective cover 201, a center block is arranged at the center of the protective cover 201, a plurality of connecting rods are arranged on the inner wall of the protective cover 201, and the ends of the connecting rods are connected to the sides of the center block.

[0027] In this embodiment, a plurality of docking holes 9 are provided at the edges of both sides of the shell of the turbine body 1, a plurality of connecting columns 202 are fixedly connected to the back edge of the protective cover 201, a connecting plate 204 is provided at the end of the connecting column 202, and a strong magnet 10 is provided inside the connecting plate 204 and the docking hole 9. The connecting column 202 is inserted into the docking hole 9 and installed by adsorption by the strong magnet 10, thereby ensuring the installation stability of the protective cover 201.

[0028] In this embodiment, a buffer spring 203 is fixedly connected to the top of the connecting plate 204, and the top of the buffer spring 203 is interconnected with the bottom of the connecting column 202. The buffer spring 203 can achieve a good energy absorption effect when the protective cover 201 is subjected to external impact, thereby helping to protect the turbine body 1.

[0029] In this embodiment, an insertion rod 12 is fixedly connected to the back edge of the dust cover 3, and a socket 206 is opened at the front edge of the protective cover 201. Through the provided insertion rod 12 and socket 206, the dust cover 3 and the protective cover 201 can be movably connected, and disassembly and assembly are convenient.

[0030] In this embodiment, handles 205 are fixedly connected to both sides of the protective cover 201, and a protrusion 11 is provided on the front of the dust cover 3. The handles 205 and the protrusion 11 make it easy for people to disassemble the protective cover 201 and the dust cover 3.

[0031] Embodiment 2:

[0032] On the basis of the first embodiment, the preferred embodiment of the small thrust and high stability closed turbine provided by the utility model is as follows: Figures 1 to 4 As shown:

[0033] In this embodiment, a sponge strip 8 is bonded to the front edge of the turbine body 1. There are six groups of sponge strips 8, which are arranged in a circular array on the surface of the turbine body 1. Through the provision of the sponge strips 8, the protective cover 201 will preferentially contact the sponge strips 8 after being subjected to external impact force. Combined with the energy absorption and shock absorption of the buffer spring 203, it can provide further protection for the turbine body 1.

[0034] In this embodiment, the bottom of the turbine body 1 is fixedly connected to a box body 4, the inner wall of the box body 4 is provided with a damping shaft 5, the end of the damping shaft 5 is fixedly connected to a rectangular block 6, the surface of the rectangular block 6 is fixedly connected to a support plate 7, and the surface of the support plate 7 is bonded with an anti-slip pad. Through the support plate 7, the rectangular block 6 is driven by the damping shaft 5 to flip into a vertical state, so that the turbine body 1 is placed vertically, which is convenient for people to inspect and maintain the interior of the turbine body 1, and also avoids the turbine body 1 from directly contacting the ground when not in use, which may cause wear.

[0035] In order to facilitate understanding of the above technical solution of the present invention, the working principle or operation method of the present invention in the actual process is described in detail below.

[0036] In actual application, the protective cover 201 is inserted into the docking hole 9 on the surface of the turbine body 1 through the connecting column 202 on the back thereof, and the installation is completed by adsorption and docking between the connecting plate 204 and the strong magnet 10 inside the docking hole 9. When an external bird accidentally hits it or it is affected by high wind pressure and vibrates, the protective cover 201 will be pressed down, and the back of the protective cover 201 will first contact the sponge strip 8, which, in conjunction with the energy absorption and shock reduction of the buffer spring 203, can provide a good protective effect on the turbine body 1. When the turbine body 1 is not in use, the dust cover 3 is inserted into the socket 206 on the surface of the protective cover 201 through the insertion rod 12 on the back thereof to complete the installation and docking. When the turbine body 1 needs to be inspected and repaired, the support plate 7 drives the rectangular block 6 to flip into a vertical state through the damping shaft 5, so that the turbine body 1 is placed vertically, which is convenient for people to inspect and repair the interior of the turbine body 1, and also avoids the wear and tear caused by direct contact with the ground when the turbine body 1 is not in use.

[0037] In summary, with the aid of the above-mentioned technical scheme of the utility model, through the setting of the protective component 2, the strong magnet 10 is adsorbed and docked, and the stability is relatively high. When the turbine body 1 is impacted by external force, the protective cover 201 will preferentially contact the sponge strip 8, and cooperate with the energy absorption and shock reduction of the buffer spring 203, which can play a good protective effect on the turbine body 1. The support plate 7 drives the rectangular block 6 to flip into a vertical state through the damping shaft 5, so that the turbine body 1 is placed vertically, which is convenient for people to inspect and repair the interior of the turbine body 1, and also avoids the turbine body 1 from directly contacting the ground when not in use, which will cause wear.

[0038] The above description is only a preferred embodiment of the present invention and is not intended to limit the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. A low-thrust, high-stability closed turbine, comprising a turbine body (1), characterized in that: A protective component (2) is movably mounted on the front of the turbine body (1), a dust cover (3) is movably mounted on the surface of the protective component (2), the protective component (2) comprises a protective cover (201), a center block is arranged at the center of the protective cover (201), and a plurality of groups of connecting rods are arranged on the inner wall of the protective cover (201), and the ends of the connecting rods are connected to the side surfaces of the center block.

2. A low-thrust, high-stability closed turbine according to claim 1, characterized in that: The turbine body (1) has a plurality of docking holes (9) at the edges of both sides of the shell, and the protective cover (201) has a plurality of connecting columns (202) fixedly connected at the back edge, and connecting plates (204) are provided at the ends of the connecting columns (202). Strong magnets (10) are provided inside the connecting plates (204) and the docking holes (9).

3. A low-thrust, high-stability closed turbine according to claim 2, characterized in that: A buffer spring (203) is fixedly connected to the top of the connecting plate (204), and the top of the buffer spring (203) is connected to the bottom of the connecting column (202).

4. A low-thrust, high-stability closed turbine according to claim 1, characterized in that: An insertion rod (12) is fixedly connected to the back edge of the dust cover (3), and an insertion hole (206) is provided at the front edge of the protective cover (201).

5. A small thrust and high stability closed turbine according to claim 1, characterized in that: Handles (205) are fixedly connected to both sides of the protective cover (201), and a protrusion (11) is provided on the front side of the dust cover (3).

6. A closed turbine with low thrust and high stability according to claim 1, characterized in that: Sponge strips (8) are bonded to the front edge of the turbine body (1), and the number of the sponge strips (8) is six groups, and they are arranged in a circular array on the surface of the turbine body (1).

7. A small thrust and high stability closed turbine according to claim 1, characterized in that: The bottom of the turbine body (1) is fixedly connected to a box body (4), the inner wall of the box body (4) is provided with a damping shaft (5), the end of the damping shaft (5) is fixedly connected to a rectangular block (6), the surface of the rectangular block (6) is fixedly connected to a support plate (7), and the surface of the support plate (7) is bonded with an anti-slip pad.

Images