Automatic parachute ejection device
By designing an automatic ejection parachute device, using components such as the parachute box and torsion servo, the problems of high adaptability and cost of existing devices are solved, and the rapid, reliable ejection and simplified operation of the parachute is achieved.
Patent Information
- Application Number
- CN202422225354.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-09-11
- Publication Date
- 2025-07-08
- Estimated Expiration
- 2034-09-11
AI Technical Summary
The existing parachute ejection device has low appearance and assembly properties, high cost, prone to quality problems, and poor adaptability to the products used.
An automatic ejection parachute device is designed, including a umbrella cabin box, ejection base, large torsion servo, tab limit seat and locking spring. The large torsion servo is triggered through the power control interface to achieve high-speed ejection and slow fall of the parachute.
The rapid and reliable pop-up of the parachute is achieved, reducing assembly difficulty and cost, improving adaptability to the loading platform, and simplifying operations.
Smart Images
Figure CN223072753U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of ejection devices, in particular to an automatic ejection parachute device. Background Art
[0002] A parachute is a device that uses the principle of air resistance to safely land a person or an object from a high altitude. Generally, a parachute consists of a parachute canopy, suspension lines, a harness system, etc.
[0003] The existing parachute ejection devices have relatively low appearance and assembly adaptability, require high requirements for the loading platform, usually need to add reinforcement devices for installation, are very inconvenient to operate, and have very high costs. The shapes of the existing parachute ejection devices are relatively rough, with low adaptability to the products used, affecting the experience, and the processing method is relatively simple, prone to quality problems. Moreover, for the existing parachute ejection devices, the actual products often have excessive strength and weight.
[0004] Therefore, an automatic ejection parachute device is proposed. Summary of the Utility Model
[0005] The purpose of the utility model is to provide an automatic ejection parachute device to solve the problems mentioned in the above background art.
[0006] The utility model specifically adopts the following technical solutions to achieve the above purpose:
[0007] The automatic ejection parachute device includes a parachute cabin box. Inside the parachute cabin box, an ejection base is fixedly installed. At the inner bottom of the parachute cabin box, a large-torque servo is fixedly installed, and a metal servo arm is fixedly installed at the output end of the large-torque servo. At the bottom surface of the ejection base, a tongue limiting seat is fixedly installed. Inside the tongue limiting seat, a tongue plate is movably inserted. The tongue plate and the metal servo arm are hinged and installed. Small-diameter through grooves and large-diameter through grooves are formed on the surface of the tongue plate. At the top surface of the tongue plate, a spring base is fixedly installed, and a locking spring is fixedly installed between the end face of the spring base and the end face of the tongue limiting seat. A spring limiting rod is inserted into the ejection base, the tongue limiting seat, and the tongue plate. A snap ring is clamped on the surface of the spring limiting rod. The top end of the spring limiting rod is fixedly installed with a parachute cabin bottom plate, and a main spring is sleeved on the surface of the spring limiting rod.
[0008] Further, a power control interface is arranged on the surface of the parachute cabin box, and the power control interface is connected to the large-torque servo. The top surface of the parachute cabin box is covered with a parachute cabin cover.
[0009] Further, the parachute cabin box includes a cylinder body. Multiple installation bumps are fixedly installed on the surface of the cylinder body. A stepped portion is arranged on the inner wall of the cylinder body. The ejection base is fixedly installed inside the cylinder body and at the top end of the stepped portion.
[0010] Further, the spring limiting rod includes a rod body, and the rod body is movably inserted into the ejection base, the tongue limiting seat and the tongue plate. Notches are formed on the surface of the rod body, and a mounting disc is fixedly installed at the top end of the rod body, and a parachute cabin bottom plate is fixedly installed on the top surface of the mounting disc.
[0011] Further, the diameters of the small-diameter through groove and the notch on the surface of the tongue plate are equal, and the diameter of the rod body is equal to the diameter of the large-diameter through groove.
[0012] Further, convex strips are arranged on the inner wall of the cylinder body, and notches are formed on the surface of the parachute cabin bottom plate. The notches on the surface of the parachute cabin bottom plate and the convex strips on the inner wall of the cylinder body are arranged in correspondence.
[0013] The beneficial effects of the present utility model are as follows:
[0014] After folding the parachute and installing it on the parachute cabin bottom plate, pressing the parachute cabin bottom plate to the limit position, at this time the locking spring pushes the tongue plate to clamp the limiting part of the spring limiting rod. When it is necessary to eject the parachute, a trigger command is sent through the power control interface, and the large-torque servo motor drives the metal servo arm to pull the tongue plate to move outwards to disengage from the limiting part of the spring limiting rod. At this time, the main spring releases elastic force to push the parachute cabin bottom plate, realizing the high-speed ejection of the parachute from the parachute cabin box. After pushing out a sufficient stroke, the snap ring at the bottom of the spring limiting rod is limited by the tongue limiting seat to keep the parachute connected to the ejection device to realize the slow-falling process of the parachute throwing. The device has a simple structure, low accessory cost, low assembly difficulty, modular design of its core components, high adaptability with arbitrary modification of the appearance, and low requirements for the loading platform. Description of the Drawings
[0015] Figure 1 is a three-dimensional structural schematic diagram of the present utility model;
[0016] Figure 2 is a partial front sectional view of the present utility model;
[0017] Figure 3 is a schematic diagram of a partial structure of the present utility model;
[0018] Figure 4 is a schematic diagram of another partial structure of the present utility model;
[0019] Figure 5 is an exploded view of a partial structure of the present utility model;
[0020] Reference numerals: 1, umbrella cabin box; 101, cylinder body; 102, mounting bump; 103, stepped portion; 2, umbrella cabin cover; 3, power control interface; 4, ejection base; 5, large-torque servo; 6, metal servo arm; 7, tongue limiting seat; 8, tongue plate; 81, small-diameter through slot; 82, large-diameter through slot; 9, spring base; 10, locking spring; 11, spring limiting rod; 1101, rod body; 1102, notch; 1103, mounting disc; 12, snap ring; 13, umbrella cabin bottom plate; 14, main spring. Detailed implementation manners
[0021] To make the objectives, technical solutions and advantages of the embodiments of the present utility model clearer, the technical solutions in the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model. Apparently, the described embodiments are some but not all of the embodiments of the present utility model. Usually, the components of the embodiments of the present utility model described and illustrated in the accompanying drawings here can be arranged and designed in various different configurations.
[0022] Therefore, the following detailed description of the embodiments of the present utility model provided in the accompanying drawings is not intended to limit the scope of the claimed present utility model, but merely represents selected embodiments of the present utility model. All other embodiments obtained by those of ordinary skill in the art based on the embodiments of the present utility model without creative efforts shall fall within the scope of protection of the present utility model.
[0023] It should be noted that: similar reference numerals and letters denote similar items in the following drawings. Therefore, once an item is defined in one drawing, it does not need to be further defined and explained in subsequent drawings. In addition, the terms "first", "second", etc. are only used for descriptive distinction and cannot be construed as indicating or implying relative importance.
[0024] In the description of the embodiments of the present utility model, it should be noted that the orientation or positional relationship indicated by terms such as "inner", "outer", "upper", etc. is based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship in which the product of this utility model is usually placed during use. It is only for the convenience of describing the present utility model and simplifying the description, rather than indicating or implying that the device or element referred to must have a specific orientation, be constructed and operated in a specific orientation, and therefore cannot be construed as a limitation of the present utility model.
[0025] Such as Figures 1 to 5As shown in the figure, the automatic ejection parachute device includes a parachute cabin box 1. Inside the parachute cabin box 1, an ejection base 4 is fixedly installed. At the inner bottom of the parachute cabin box 1, a large-torque servo 5 is fixedly installed, and the output end of the large-torque servo 5 is fixedly installed with a metal servo arm 6. At the bottom surface of the ejection base 4, a tongue limiting seat 7 is fixedly installed. Inside the tongue limiting seat 7, a tongue plate 8 is movably inserted. The tongue plate 8 and the metal servo arm 6 are hinged. On the surface of the tongue plate 8, a small-diameter through groove 81 and a large-diameter through groove 82 are opened. On the top surface of the tongue plate 8, a spring base 9 is fixedly installed, and a locking spring 10 is fixedly installed between the end surface of the spring base 9 and the end surface of the tongue limiting seat 7. A spring limiting rod 11 is inserted into the ejection base 4, the tongue limiting seat 7, and the tongue plate 8. A snap ring 12 is clamped on the surface of the spring limiting rod 11. The top end of the spring limiting rod 11 is fixedly installed with a parachute cabin bottom plate 13, and a main spring 14 is sleeved on the surface of the spring limiting rod 11. More specifically, after the parachute is folded, it is installed on the parachute cabin bottom plate 13. Press the parachute cabin bottom plate 13 to the limit position. At this time, the locking spring 10 pushes the tongue plate 8 to clamp the limiting part of the spring limiting rod 11. When it is necessary to eject the parachute, a trigger command is sent through the power control interface 3. The large-torque servo 5 drives the metal servo arm 6 to pull the tongue plate 8 to move outwards so that it disengages from the limiting part of the spring limiting rod 11. At this time, the main spring 14 releases its elastic force to push the parachute cabin bottom plate 13, realizing the high-speed ejection of the parachute from the parachute cabin box 1. After pushing out a sufficient stroke, the snap ring 12 at the bottom of the spring limiting rod 11 is limited by the tongue limiting seat 7 to keep the parachute connected to the ejection device to realize the process of slow falling of the parachute after throwing.
[0026] On the surface of the parachute cabin box 1, a power control interface 3 is provided, and the power control interface 3 is connected to the large-torque servo 5. The top surface of the parachute cabin box 1 is covered with a parachute cabin cover 2. More specifically, through the power control interface 3, a trigger command can be triggered. Through the power control interface 3, the large-torque servo 5 can be triggered to rotate. By covering the parachute cabin cover 2 on the top surface of the parachute cabin box 1, the parachute cabin cover 2 can be pushed open when the parachute is ejected.
[0027] The parachute cabin box 1 includes a cylinder body 101. On the surface of the cylinder body 101, multiple groups of installation bumps 102 are fixedly installed. On the inner wall of the cylinder body 101, a stepped part 103 is provided. Inside the cylinder body 101 and at the top of the stepped part 103, the ejection base 4 is fixedly installed. More specifically, through the installation bumps 102 on the surface of the cylinder body 101, it is convenient to fix the ejection device. Through the stepped part 103, the ejection base 4 can be fixedly installed.
[0028] The spring limit rod 11 includes a rod body 1101. The rod body 1101 is movably inserted into the ejection base 4, the tongue limit seat 7, and the tongue plate 8. A notch 1102 is formed on the surface of the rod body 1101. An installation disk 1103 is fixedly installed at the top end of the rod body 1101, and a parachute compartment bottom plate 13 is fixedly installed on the top surface of the installation disk 1103. More specifically, when in the limit position, the small-diameter through groove 81 on the surface of the tongue plate 8 and the notch 1102 on the surface of the rod body 1101 are clamped to limit the rod body 1101. When the large-torque servo 5 drives the metal servo arm 6 to pull the tongue plate 8 outward, the large-diameter through groove 82 on the surface of the tongue plate 8 corresponds to the rod body 1101, enabling the vertical movement of the rod body 1101.
[0029] The diameter of the small-diameter through groove 81 on the surface of the tongue plate 8 is equal to the diameter of the notch 1102, and the diameter of the rod body 1101 is equal to the diameter of the large-diameter through groove 82. More specifically, due to the equal diameters of the small-diameter through groove 81 and the notch 1102, the rod body 1101 can be limited, and due to the equal diameters of the rod body 1101 and the large-diameter through groove 82, the relative movement between the rod body 1101 and the tongue plate 8 can be realized.
[0030] Convex strips are provided on the inner wall of the cylinder body 101, and notches are formed on the surface of the parachute compartment bottom plate 13. The notches on the surface of the parachute compartment bottom plate 13 and the convex strips on the inner wall of the cylinder body 101 are correspondingly arranged. More specifically, by meshing the notches on the surface of the parachute compartment bottom plate 13 with the convex strips on the inner wall of the cylinder body 101, the vertical movement of the parachute compartment bottom plate 13 can be limited and guided.
[0031] In summary: After folding the parachute, it is installed on the parachute compartment bottom plate 13. When the parachute compartment bottom plate 13 reaches the limit position, the locking spring 10 pushes the tongue plate 8 to clamp the limit part of the spring limit rod 11. When the parachute needs to be ejected, a trigger command is sent through the power control interface 3. The large-torque servo 5 drives the metal servo arm 6 to pull the tongue plate 8 outward to disengage it from the limit part of the spring limit rod 11. At this time, the main spring 14 releases its elastic force to push the parachute compartment bottom plate 13, realizing the high-speed ejection of the parachute from the parachute compartment box 1. After pushing out a sufficient stroke, the snap ring 12 at the bottom of the spring limit rod 11 is limited by the tongue limit seat 7 to keep the parachute connected to the ejection device and realize the process of slow falling of the parachute.
[0032] The above shows and describes the basic principles, main features, and advantages of the present invention. Those skilled in the art should understand that the present invention is not limited by the above embodiments. What is described in the above embodiments and the specification is only the principle of the present invention. Without departing from the spirit and scope of the present invention, the present invention will have various changes and improvements, and these changes and improvements all fall within the scope of the present invention claimed. The scope of protection required by the present invention is defined by the appended claims and their equivalents.
Claims
1. Automatic ejection parachute device, characterized in that, It includes an umbrella cabin box (1), inside which an ejection base (4) is fixedly installed. At the inner bottom of the umbrella cabin box (1), a large-torque servo (5) is fixedly installed, and a metal servo arm (6) is fixedly installed at the output end of the large-torque servo (5). At the bottom surface of the ejection base (4), a tongue limiting seat (7) is fixedly installed. Inside the tongue limiting seat (7), a tongue plate (8) is movably inserted. The tongue plate (8) and the metal servo arm (6) are hinged. On the surface of the tongue plate (8), a small-diameter through groove (81) and a large-diameter through groove (82) are provided. On the top surface of the tongue plate (8), a spring base (9) is fixedly installed, and a locking spring (10) is fixedly installed between the end face of the spring base (9) and the end face of the tongue limiting seat (7). A spring limiting rod (11) is inserted into the ejection base (4), the tongue limiting seat (7), and the tongue plate (8). A snap spring (12) is clamped on the surface of the spring limiting rod (11). The top end of the spring limiting rod (11) is fixedly installed with an umbrella cabin bottom plate (13), and a main spring (14) is sleeved on the surface of the spring limiting rod (11).
2. The automatic ejection parachute device according to claim 1, wherein On the surface of the umbrella cabin box (1), a power control interface (3) is provided, and the power control interface (3) is connected to the large-torque servo (5). The top surface of the umbrella cabin box (1) is covered with an umbrella cabin cover (2).
3. The automatic ejection parachute device according to claim 1, characterized in that, The umbrella cabin box (1) includes a cylinder body (101). On the surface of the cylinder body (101), multiple installation bumps (102) are fixedly installed. On the inner wall of the cylinder body (101), a stepped portion (103) is provided. Inside the cylinder body (101) and at the top of the stepped portion (103), an ejection base (4) is fixedly installed.
4. The automatic ejection parachute device according to claim 1, characterized in that, The spring limiting rod (11) includes a rod body (1101). The rod body (1101) is movably inserted into the ejection base (4), the tongue limiting seat (7), and the tongue plate (8). On the surface of the rod body (1101), a notch (1102) is provided. The top end of the rod body (1101) is fixedly installed with an installation disk (1103), and the umbrella cabin bottom plate (13) is fixedly installed on the top surface of the installation disk (1103).
5. The automatic ejection parachute device according to claim 4, characterized in that, The diameter of the small-diameter through groove (81) on the surface of the tongue plate (8) is equal to the diameter of the notch (1102), and the diameter of the rod body (1101) is equal to the diameter of the large-diameter through groove (82).
6. The automatic ejection parachute device according to claim 3, wherein On the inner wall of the cylinder body (101), a rib is provided. On the surface of the umbrella cabin bottom plate (13), a notch is provided. The notch on the surface of the umbrella cabin bottom plate (13) and the rib on the inner wall of the cylinder body (101) are correspondingly arranged.