Throwing device and throwing method

By designing a throwing device including a launch energy storage unit and a rotating unit, the problem of difficulty in studying the angular velocity and linear velocity of an aircraft or rocket when releasing a flying object in the prior art is solved, and the effect of the throwing object having a linear velocity and angular velocity when throwing is achieved.

CN119503125APending Publication Date: 2025-02-25BEIJING INST OF ENVIRONMENTAL FEATURES
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Patent Information

Application Number
CN202411705397.4
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-11-26
Publication Date
2025-02-25

AI Technical Summary

Technical Problem

The prior art is difficult to effectively study the angular velocity and linear velocity of aircraft or rockets when releasing companions during flight, which affects the study of micro-movement phenomena.

Method used

A throwing device is designed, including a emitting energy storage unit and a rotating unit. By applying a force along the axis of the cylinder, the cover body carries the throwing object and obtains an angular velocity.

Benefits of technology

It realizes that the throwing object has linear and angular velocity when throwing, and can more effectively study the micro motion of an aircraft or rocket.

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Abstract

The invention relates to the technical field of aerospace, in particular to a throwing device and a throwing method. The embodiment of the invention provides a throwing device. The throwing device comprises a launching energy storage unit and a rotating unit. The rotating unit comprises a barrel and a wrapping body, the inner wall of the barrel is provided with a spiral groove which is spirally distributed around the axis of the barrel, the inner wall of the wrapping body comprises a cavity matched with the shape of a thrown object, the shape size of the wrapping body is matched with the size of the inner wall of the barrel, the wrapping body is provided with a protrusion, and the protrusion is matched with the inner wall of the barrel. The bulge is matched with the spiral groove and is inserted into the spiral groove; the launching energy storage unit is used for applying force in the axis direction of the barrel to the wrapping body in the barrel. The embodiment of the invention provides a throwing device and a throwing method. The throwing device and the throwing method can enable a thrown object to have an angular velocity and a linear velocity when the thrown object is thrown.
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Description

Technical Field

[0001] The present invention relates to the field of aerospace technology, and in particular to a throwing device and a throwing method. Background Art

[0002] Aircraft, rockets and other products will release accompanying objects during flight due to mission requirements. When the accompanying objects are thrown out at different speeds and angular velocities, the rocket or aircraft will produce micromotion. By studying the speed and angular velocity of the accompanying objects when they are released, we can study the micromotion boundary conditions of the aircraft or rocket. Therefore, it is of great significance to study the angular velocity and linear velocity of heavy ejected objects when they are released. Summary of the invention

[0003] The embodiment of the present invention provides a throwing device and a throwing method, which can make the thrown object have angular velocity and linear velocity when thrown.

[0004] In a first aspect, an embodiment of the present invention provides a throwing device, including a launching energy storage unit and a rotating unit;

[0005] The rotating unit comprises a cylinder and a covering body, the inner wall of the cylinder is provided with spiral grooves spirally distributed around its axis, the inner wall of the covering body comprises a cavity matching the outer shape of the ejected object, the outer dimensions of the covering body match the dimensions of the inner wall of the cylinder, the covering body is provided with a protrusion, the protrusion matches the spiral groove and is inserted into the spiral groove;

[0006] The launch energy storage unit is used to apply a force along the axis direction of the cylinder to the coating in the cylinder;

[0007] When throwing out a projectile, the launching energy storage unit applies a force along the axis direction of the cylinder to the coating in the cylinder, so that it is launched to the outside of the cylinder. In the process of the coating carrying the projectile moving in the cylinder, the spiral groove and the protrusion cooperate to make the coating carry the projectile to rotate and obtain an angular velocity.

[0008] In a possible design, the launch energy storage unit includes a first spring and a locking release device, wherein the locking release device controls the first spring to maintain a compressed state and is used to release the first spring from the compressed state to provide power.

[0009] In a possible design, the locking release device includes a cam, a first column, a second column, a locking release column, and a second spring. The cam is connected to a steering gear through a rotating shaft, and the steering gear is used to rotate the cam. The first column is fixedly installed on the bottom plate of the cylinder. The first column is provided with a through hole, and the second column is provided with a limiting hole. The locking release column passes through the through hole and enters the limiting hole. The cam, the locking release column, the through hole and the limiting hole are located in the same plane. The locking support column sleeve is provided with a second spring. A power disk is installed at one end of the second column, and the first spring is between the power disk and the bottom plate.

[0010] When the ejected object is not released, the raised part of the cam abuts against one end of the locking release column, and the second spring sleeved on the locking release column is in a compressed state. When the ejected object is released, the servo engine rotates the cam, and one end of the locking release column abuts against the recessed part of the cam under the elastic force of the second spring, and the other end of the locking release column pops out from the limiting hole, releasing the connection between the first column and the second column. The second column and the power disk are displaced and exerted force under the elastic force of the first spring, so that the coated body on one side of the power disk coated with the ejected object is ejected.

[0011] In a possible design, a guide piece is disposed outside the first spring.

[0012] In a possible design, the power disc is provided with a spring groove to connect the first spring.

[0013] In a possible design, a roller is installed on one end of the locking support column for abutting against the cam.

[0014] In a possible design, the cam includes four raised portions and four recessed portions, and includes four groups of the first column, the second column, the locking release column, and the second spring that are evenly distributed around the cam.

[0015] In a possible design, the enveloping body includes a first half enveloping body, a second half enveloping body and an annular hoop, the annular hoop is provided with the protrusion, and the annular hoop is used to tighten the first half enveloping body and the second half enveloping body.

[0016] In a possible design, four evenly distributed first springs are included.

[0017] In a second aspect, an embodiment of the present invention further provides a method for throwing a thrown object, based on any of the throwing devices described above, the throwing method comprising:

[0018] Using the launch energy storage unit to apply a force along the axis direction of the cylinder to the covering body in the cylinder, so that it is launched toward the outside of the cylinder;

[0019] In the process that the covering body carries the ejecta and moves in the cylinder, the spiral groove and the protrusion cooperate to make the covering body carry the ejecta and rotate to obtain an angular velocity.

[0020] Compared with the prior art, the present invention has at least the following beneficial effects:

[0021] In this embodiment, a launch energy storage unit is used to provide power for the coating of the built-in ejecta, that is, to provide a linear velocity along the axis direction of the cylinder. The launch energy storage unit can be powered by a spring, by gas expansion, or by an electromagnetic. When the coating of the built-in ejecta moves in the cylinder, the protrusion controls the rotation of the coating of the built-in ejecta under the action of the spiral groove to obtain an angular velocity. In summary, the device provided in this application can be used to throw ejecta with a linear velocity and an angular velocity. BRIEF DESCRIPTION OF THE DRAWINGS

[0022] In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some embodiments of the present invention. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.

[0023] Figure 1 is a schematic cross-sectional structure diagram of a throwing device provided by an embodiment of the present invention;

[0024] Figure 2 It is a structural schematic diagram of a throwing device provided by an embodiment of the present invention;

[0025] Figure 3 It is a structural schematic diagram of a locking and releasing device provided in an embodiment of the present invention.

[0026] In the figure:

[0027] 1-Cylinder;

[0028] 11- spiral groove;

[0029] 12- bottom plate;

[0030] 2-encapsulation body;

[0031] 21- convex;

[0032] 3-Throwaways;

[0033] 4- first spring;

[0034] 41- guide member;

[0035] 5-Lock release device;

[0036] 51- Cam;

[0037] 52- first column;

[0038] 53- second column;

[0039] 54-lock release column;

[0040] 55 - second spring;

[0041] 56-Servo;

[0042] 57-power plate;

[0043] 58-Roller. DETAILED DESCRIPTION

[0044] In order to make the purpose, technical solutions and advantages of the embodiments of the present invention clearer, the technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the drawings in the embodiments of the present invention. Obviously, the described embodiments are part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments in the present invention, all other embodiments obtained by ordinary technicians in this field without making creative work are within the scope of protection of the present invention.

[0045] In the description of the embodiments of the present invention, unless otherwise clearly specified and limited, the terms "first" and "second" are used for descriptive purposes only and cannot be understood as indicating or implying relative importance; unless otherwise specified or explained, the term "multiple" refers to two or more; the terms "connected" and "fixed" should be understood in a broad sense, for example, "connected" can be a fixed connection, a detachable connection, an integral connection, or an electrical connection; it can be directly connected or indirectly connected through an intermediate medium. For ordinary technicians in this field, the specific meanings of the above terms in the present invention can be understood according to specific circumstances.

[0046] In the description of this specification, it should be understood that the directional words such as "upper" and "lower" described in the embodiments of the present invention are described at the angles shown in the drawings and should not be understood as limiting the embodiments of the present invention. In addition, in the context, it should also be understood that when it is mentioned that an element is connected to another element "upper" or "lower", it can not only be directly connected to another element "upper" or "lower", but also indirectly connected to another element "upper" or "lower" through an intermediate element.

[0047] Please refer to Figure 1 and Figure 2, an embodiment of the present invention provides a throwing device, including a launching energy storage unit and a rotating unit;

[0048] The rotating unit includes a cylinder 1 and a covering body 2. The inner wall of the cylinder 1 is provided with a spiral groove 11 spirally distributed around its axis. The inner wall of the covering body 2 includes a cavity matching the shape of the ejection 3. The outer dimensions of the covering body 2 match the dimensions of the inner wall of the cylinder 1. The covering body 2 is provided with a protrusion 21, which matches the spiral groove 11 and is inserted into the spiral groove 11.

[0049] The launch energy storage unit is used to apply a force along the axis direction of the cylinder 1 to the covering body 2 in the cylinder 1;

[0050] When throwing out the ejecta 3, the launching energy storage unit applies a force along the axial direction of the cylinder 1 to the coating 2 in the cylinder 1, so that it is launched to the outside of the cylinder 1. In the process of the coating 2 carrying the ejecta 3 moving in the cylinder 1, the spiral groove 11 and the protrusion 21 cooperate to make the coating 2 carrying the ejecta 3 rotate and obtain an angular velocity.

[0051] In this embodiment, a launching energy storage unit is used to provide power for the coating 2 with the built-in ejecta 3, that is, to provide a linear velocity along the axial direction of the cylinder 1. The launching energy storage unit can be powered by a spring, by gas expansion, or by electromagnetic power. When the coating 2 with the built-in ejecta 3 moves in the cylinder 1, the protrusion 21 will control the rotation of the coating 2 with the built-in ejecta 3 under the action of the spiral groove 11 to obtain an angular velocity. In summary, the device provided in this application can be used to throw an ejecta 3 with a linear velocity and an angular velocity.

[0052] In this embodiment, the protrusion 21 is cylindrical, and the cylindrical protrusion and the spiral groove 11 are matched by grinding.

[0053] In some embodiments of the present invention, the launch energy storage unit includes a first spring 4 and a locking release device 5. The locking release device 5 controls the first spring 4 to maintain a compressed state and is used to release the first spring 4 from a compressed state to provide power.

[0054] In this embodiment, using a spring to provide power has the advantage of being low-cost and reproducible.

[0055] Please refer to Figure 3In some embodiments of the present invention, the locking release device 5 includes a cam 51, a first column 52, a second column 53, a locking release column 54, and a second spring 55. The cam 51 is connected to a steering gear 56 through a rotating shaft. The steering gear 56 is used to rotate the cam 51. The first column 52 is fixedly installed on the bottom plate 12 of the cylinder 1. The first column 52 is provided with a through hole, and the second column 53 is provided with a limiting hole. The locking release column 54 passes through the through hole and enters the limiting hole. The cam 51, the locking release column 54, the through hole and the limiting hole are located in the same plane. The locking support column sleeve is provided with a second spring 55. A power disk 57 is installed at one end of the second column 53. The first spring 4 is between the power disk 57 and the bottom plate 12;

[0056] When the ejected object 3 is not released, the protrusion 21 of the cam 51 abuts against one end of the locking release column 54, and the second spring 55 sleeved on the locking release column 54 is in a compressed state. When the ejected object 3 is released, the servo 56 rotates the cam 51, and one end of the locking release column 54 abuts against the recessed part of the cam 51 under the elastic force of the second spring 55, and the other end of the locking release column 54 pops out from the limiting hole, releasing the connection between the first column 52 and the second column 53. The second column 53 and the power disk 57 are displaced and exerted force under the elastic force of the first spring 4, so that the covering body 2 coated with the ejected object 3 on one side of the power disk 57 is thrown out.

[0057] In this embodiment, the locking and releasing device 5 can be used to lock and release the first spring 4, so that the ejection can be controlled.

[0058] In some embodiments of the present invention, a guide member 41 is disposed outside the first spring 4 .

[0059] In this embodiment, the guide member 41 can release the elastic force of the first spring 4 in the guiding direction.

[0060] In some embodiments of the present invention, the power disk 57 is provided with a spring groove to connect the first spring 4 .

[0061] In some embodiments of the present invention, a roller 58 is installed at one end of the locking support column for abutting against the cam 51 .

[0062] In this embodiment, the friction between the locking support column and the cam 51 can be replaced by rolling friction instead of sliding friction through the roller 58 .

[0063] In some embodiments of the present invention, the cam 51 includes four protrusions 21 and four recesses, including four groups of first columns 52 , second columns 53 , locking release columns 54 , and second springs 55 evenly distributed around the cam 51 .

[0064] In this embodiment, the four groups of components that are evenly distributed can make the overall structure and force generation more uniform.

[0065] In some embodiments of the present invention, the enclosure 2 includes a first half enclosure 2 , a second half enclosure 2 and an annular hoop, on which a protrusion 21 is provided, and the annular hoop is used to tighten the first half enclosure 2 and the second half enclosure 2 .

[0066] In this embodiment, the enclosure 2 consisting of the first half enclosure 2 and the second half enclosure 2 is fastened by an annular hoop, which facilitates the installation and removal of the heavy ejecta 3 .

[0067] In some embodiments of the present invention, four evenly distributed first springs 4 are included.

[0068] In this embodiment, the four first springs 4 can provide sufficient elastic force and are evenly distributed, so that the points of action of the elastic force are more even and the force on the covering body 2 is more evenly distributed.

[0069] The embodiment of the present invention further provides a method for throwing a throwable object 3. Based on any of the above throwing devices, the throwing method includes:

[0070] The launching energy storage unit is used to apply a force along the axis direction of the cylinder 1 to the covering body 2 in the cylinder 1, so that it is launched toward the outside of the cylinder 1;

[0071] When the covering body 2 carries the ejecta 3 and moves in the cylinder 1, the spiral groove 11 and the protrusion 21 cooperate to make the covering body 2 carry the ejecta 3 and rotate to obtain an angular velocity.

[0072] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present invention, rather than to limit it. Although the present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that they can still modify the technical solutions described in the aforementioned embodiments, or make equivalent replacements for some of the technical features therein. However, these modifications or replacements do not deviate the essence of the corresponding technical solutions from the spirit and scope of the technical solutions of the embodiments of the present invention.

Claims

1. A throwing device, characterized in that: It includes a launching energy storage unit and a rotating unit; The rotating unit comprises a cylinder and a covering body, the inner wall of the cylinder is provided with spiral grooves spirally distributed around its axis, the inner wall of the covering body comprises a cavity matching the outer shape of the ejected object, the outer dimensions of the covering body match the dimensions of the inner wall of the cylinder, the covering body is provided with a protrusion, the protrusion matches the spiral groove and is inserted into the spiral groove; The launch energy storage unit is used to apply a force along the axis direction of the cylinder to the coating in the cylinder; When throwing out a projectile, the launching energy storage unit applies a force along the axis direction of the cylinder to the coating in the cylinder, so that it is launched to the outside of the cylinder. In the process of the coating carrying the projectile moving in the cylinder, the spiral groove and the protrusion cooperate to make the coating carry the projectile to rotate and obtain an angular velocity.

2. The ejection device according to claim 1, characterized in that: The launch energy storage unit includes a first spring and a locking and releasing device. The locking and releasing device controls the first spring to maintain a compressed state and is used to release the first spring from a compressed state to provide power.

3. The ejection device according to claim 2, characterized in that: The locking release device comprises a cam, a first column, a second column, a locking release column, and a second spring. The cam is connected to the steering gear through a rotating shaft. The steering gear is used to rotate the cam. The first column is fixedly installed on the bottom plate of the cylinder. The first column is provided with a through hole. The second column is provided with a limiting hole. The locking release column passes through the through hole and enters the limiting hole. The cam, the locking release column, the through hole and the limiting hole are located in the same plane. The locking support column sleeve is provided with a second spring. A power disk is installed at one end of the second column. The first spring is between the power disk and the bottom plate. When the ejected object is not released, the raised part of the cam abuts against one end of the locking release column, and the second spring sleeved on the locking release column is in a compressed state. When the ejected object is released, the servo engine rotates the cam, and one end of the locking release column abuts against the recessed part of the cam under the elastic force of the second spring, and the other end of the locking release column pops out from the limiting hole, releasing the connection between the first column and the second column. The second column and the power disk are displaced and exerted force under the elastic force of the first spring, so that the coated body on one side of the power disk coated with the ejected object is ejected.

4. The ejection device according to claim 3, characterized in that: A guide piece is arranged outside the first spring.

5. The ejection device according to claim 3, characterized in that: The power disc is provided with a spring slot to connect the first spring.

6. The ejection device according to claim 3, characterized in that: A roller is installed on one end of the locking support column for abutting against the cam.

7. The ejection device according to claim 3, characterized in that: The cam includes four raised parts and four recessed parts, and includes four groups of the first column, the second column, the locking and releasing column, and the second spring uniformly distributed around the cam.

8. The ejection device according to claim 1, characterized in that: The enveloping body comprises a first half enveloping body, a second half enveloping body and an annular hoop, the annular hoop is provided with the protrusion, and the annular hoop is used to tighten the first half enveloping body and the second half enveloping body.

9. The ejection device according to claim 2, characterized in that: The first springs include four evenly distributed ones.

10. A method for throwing an object, characterized in that: Based on the throwing device described in any one of claims 1 to 9, the throwing method includes: Using the launch energy storage unit to apply a force along the axis direction of the cylinder to the covering body in the cylinder, so that it is launched toward the outside of the cylinder; In the process that the covering body carries the ejecta and moves in the cylinder, the spiral groove and the protrusion cooperate to make the covering body carry the ejecta and rotate to obtain an angular velocity.