Folding wing unlocking device and system

By designing a folding wing unlocking device for missile launching system, the locking and unlocking of the bullet body and the folding wing is achieved by using mechanical structural state switching, the problems of parts damage of the fireworks separation device and air leakage of the pneumatic separation device in the prior art are solved, and the reliability and durability of the system are improved.

CN116007447BActive Publication Date: 2025-04-22BEIJING LINGKONG TIANXING TECH CO LTD
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Patent Information

Application Number
CN202310134433.5
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2023-02-10
Publication Date
2025-04-22
Estimated Expiration
2043-02-10

AI Technical Summary

Technical Problem

In the existing missile launch system, the pyrotechnic separation device has problems of parts damage and high test costs, while the pneumatic separation device is prone to air leakage in vibration and high temperature environments, resulting in insufficient separation power.

Method used

A folding wing unlocking device is designed, including a hoop assembly, a connecting assembly and a driving assembly. Through mechanical structural state switching, the locking and unlocking of the projectile body and the folding wing is achieved, avoiding the installation needs of gas cylinders and pipelines.

Benefits of technology

It realizes simple installation, locking and unlocking of the projectile and folding wing, improves the reliability and durability of the device, and avoids the air leakage problem of the pneumatic separation device in vibration and high temperature environments.

✦ Generated by Eureka AI based on patent content.

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Abstract

The present application provides a folding wing unlocking device and system, wherein the folding wing unlocking device includes a clamp assembly, a connecting assembly and a driving assembly; the clamp assembly includes a first clamp body and a second clamp body, and an embracing space for embracing a projectile is formed between the two; a mounting portion for mounting the folding wing is provided on the first clamp body or the second clamp body; the connecting assembly is installed between the first clamp body and the second clamp body, and when the connecting assembly is in a first state, the first clamp body and the second clamp body are locked; when the connecting assembly is in a second state, the first clamp body and the second clamp body are unlocked to separate the folding wing from the projectile; the driving assembly is connected to the connecting assembly and is used to switch the first state and the second state of the connecting assembly. The installation, locking and unlocking process of the above structure is relatively simple, and there is no need to reserve space for gas cylinders and pipelines. The switching of the connection assembly state is driven by the driving assembly in a mechanical manner, thereby realizing the locking and unlocking of the projectile and the folding wing, and improving the reliability of the device.
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Description

Technical Field

[0001] The present disclosure generally relates to the field of missile launch, and more particularly to a folding wing unlocking device. Background Art

[0002] The unlocking and separation device is to reliably connect the two parts of the structure before the combination is separated, and when the separation signal is received, it can quickly and reliably achieve unlocking and separation;

[0003] In the prior art, pyrotechnic separation or pneumatic separation is usually used to separate the two-part structure. However, the pyrotechnic separation device is a controlled item, and parts are often damaged during the test, thereby increasing the test cost and placing particularly high demands on the professionalism and requirements of the installers. Most pneumatic separations are installed in conjunction with gas cylinders and pipelines, so it is necessary to reserve installation space for gas cylinders and pipelines inside the equipment. At the same time, pneumatic separation is prone to leakage under vibration and high temperature environments, which can easily cause insufficient separation power. Summary of the invention

[0004] In view of the above defects or deficiencies in the prior art, it is desired to provide a folding wing unlocking device that can solve the above technical problems.

[0005] A first aspect of the present application provides a folding wing unlocking device, comprising:

[0006] A hoop assembly, the hoop assembly comprising a first hoop body and a second hoop body, an embracing space for embracing the elastic body is formed between the first hoop body and the second hoop body; a mounting portion for mounting the folding wing is provided on the first hoop body or the second hoop body;

[0007] A connecting assembly, the connecting assembly is installed between the first hoop body and the second hoop body, the connecting assembly has a first state and a second state; when the connecting assembly is in the first state, the first hoop body and the second hoop body are locked; when the connecting assembly is in the second state, the first hoop body and the second hoop body are unlocked, so that the folding wing is separated from the projectile body;

[0008] A driving component is connected to the connecting component and is used to switch the connecting component between a first state and a second state.

[0009] According to the technical solution provided in the embodiment of the present application, two connecting assemblies are provided, and are respectively arranged between the first end of the first hoop body and the first end of the second hoop body and between the second end of the first hoop body and the second end of the second hoop body.

[0010] According to the technical solution provided in the embodiment of the present application, the connection component includes:

[0011] A locking body, the locking body being mounted on the end of the first hoop body, the locking body being provided with an insertion groove, the end of the second hoop body being insertable into the insertion groove;

[0012] A wedge-shaped stopper, the wedge-shaped stopper being rotatably mounted in the insertion groove, and a clamping groove being provided at the end of the second hoop body corresponding to the wedge-shaped stopper;

[0013] Wherein, when the connecting assembly is in the first state, the wedge-shaped stopper rotates into the snap-fit ​​groove to lock the first hoop body and the second hoop body; when the connecting assembly is in the second state, the wedge-shaped stopper moves in a direction away from the snap-fit ​​groove to separate the first hoop body and the second hoop body.

[0014] According to the technical solution provided in the embodiment of the present application, the insertion groove is arranged on the side of the locking body close to each other; a first inclined surface is arranged in the insertion groove and close to the side of the second hoop body; along the direction away from the center line of the clamp assembly, the distance from the first inclined surface to the side of the insertion groove away from the second hoop body gradually decreases;

[0015] The first inclined surface is provided with an installation groove, and the wedge-shaped stopper can be installed in the installation groove rotatably along a second direction, and the second direction is parallel to the center line of the clamp assembly;

[0016] A second inclined surface is provided at the end of the second hoop body corresponding to the first inclined surface, and the clamping groove is provided on the second inclined surface.

[0017] According to the technical solution provided in the embodiment of the present application, the first hoop body includes a first sub-hoop body and a second sub-hoop body arranged at both ends of the first sub-hoop body; the first sub-hoop body and the second sub-hoop body are hinged along a first hinge axis; the first hinge axis is parallel to the center line of the clamp assembly.

[0018] According to the technical solution provided in the embodiment of the present application, an elastic member is provided between the insertion groove, which is away from the side of the wedge-shaped stopper, and the end portion of the second hoop body.

[0019] According to the technical solution provided in the embodiment of the present application, a spring pressure plate is provided between the installation groove and the wedge-shaped stopper, and the spring pressure plate is used to provide a pre-tightening force to the wedge-shaped stopper in a direction pointing to the clamping groove.

[0020] According to the technical solution provided in the embodiment of the present application, the driving component includes:

[0021] A rotating shaft, the rotating shaft is rotatably mounted in the inserting groove, and the wedge-shaped stopper is fixedly mounted on the rotating shaft;

[0022] A driving motor, wherein the output end of the driving motor is connected to the rotating shaft through a gear set, and is used to drive the rotating shaft to rotate along its axis.

[0023] According to the technical solution provided in the embodiment of the present application, the folding-wing unlocking device also includes: a control unit; the control unit is configured to receive control instructions and control the action of the driving component to switch the first state and the second state of the connecting component.

[0024] A second aspect of the present application provides a folding-wing unlocking system, comprising a folding wing, a body and a plurality of folding-wing unlocking devices as described above; each of the folding-wing unlocking devices is arranged along the axial direction of the body; the body is clamped into the clamping space of each clamping assembly, and the folding wing is connected to the mounting portion of each clamping assembly.

[0025] The beneficial effects of this application are:

[0026] When in use, the projectile is clamped in the embracing space formed by the first hoop body and the second hoop body, and the driving assembly is controlled to lock the first hoop body and the second hoop body. When the projectile needs to be launched, the combined structure of the projectile, folding wings and folding wing unlocking device is launched as a whole; during the flight, the combined structure can control the folding wings to unfold so that the folding wings assist the projectile in flying; when the folding wings and the projectile need to be separated from each other, the driving assembly is controlled to switch the connecting assembly to the second state, so that the first hoop body and the second hoop body are unlocked, thereby separating the folding wings from the projectile. The installation, locking and unlocking process of the above structure is relatively simple, and there is no need to reserve installation space for gas cylinders and pipelines. The locking and unlocking of the projectile and the folding wings are achieved by switching the mechanical structure state, thereby improving the reliability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0027] Other features, objects and advantages of the present application will become more apparent by reading the detailed description of non-limiting embodiments made with reference to the following drawings:

[0028] Figure 1 A schematic cross-sectional view of a folding wing unlocking device provided in the present application;

[0029] Figure 2 for Figure 1 A partial enlarged view of part A shown;

[0030] Figure 3 for Figure 1 A schematic diagram showing the connecting component 4 in a second state;

[0031] Figure 4 for Figure 3 A partial enlarged view of portion B shown;

[0032] Figure 5 for Figure 1 The front view structural diagram of the connecting component 4 when it is in the first state;

[0033] Figure 6 for Figure 1 The front view structural diagram of the connecting component 4 when it is in the second state;

[0034] Figure 7 for Figure 1 An exploded view of a drive assembly connected to the connecting assembly 4 shown;

[0035] Figure 8 for Figure 1 A schematic structural diagram of the connecting component 4 is shown.

[0036] Fig. 9 for Figure 1 A schematic side view of the structure of the folding wing unlocking device shown;

[0037] Fig.10 for Figure 1 A schematic diagram of the three-dimensional structure of the first hoop body 1 is shown;

[0038] Fig.11 for Figure 1 A schematic diagram of the three-dimensional structure of the second hoop body 2 is shown;

[0039] Fig.12 A schematic diagram of the structure of a folding wing unlocking system provided in this application;

[0040] Numbers in the figure:

[0041] 1. First hoop body; 11. First sub-hoop body; 12. Second sub-hoop body; 2. Second hoop body; 21. Second inclined surface; 22. Clamping groove; 3. Mounting portion; 4. Connecting assembly; 41. Locking body; 42. Inserting groove; 43. Wedge-shaped stopper; 44. First inclined surface; 45. Mounting groove; 46. Elastic member; 47. Spring pressure plate; 48. Flat key; 49. Bearing; 5. Rotating shaft; 6. Driving motor; 7. Driving gear; 8. Driven gear; 9. Folding wing. DETAILED DESCRIPTION

[0042] The present application is further described in detail below in conjunction with the accompanying drawings and embodiments. It is to be understood that the specific embodiments described herein are only used to explain the relevant invention, rather than to limit the invention. It is also necessary to explain that, for ease of description, only the parts related to the invention are shown in the accompanying drawings.

[0043] It should be noted that, in the absence of conflict, the embodiments and features in the embodiments of the present application can be combined with each other. The present application will be described in detail below with reference to the accompanying drawings and in combination with the embodiments.

[0044] Example 1

[0045] Please refer to Figure 1-Figure 11 A schematic diagram of a folding wing unlocking device provided in this application includes:

[0046] A hoop assembly, the hoop assembly comprising a first hoop body 1 and a second hoop body 2, wherein an embracing space for embracing the elastic body is formed between the first hoop body 1 and the second hoop body 2; a mounting portion 3 for mounting the folding wing is provided on the first hoop body 1 or the second hoop body 2;

[0047] A connecting assembly 4, wherein the connecting assembly 4 is installed between the first hoop body 1 and the second hoop body 2, and the connecting assembly 4 has a first state and a second state; when the connecting assembly 4 is in the first state, the first hoop body 1 and the second hoop body 2 are locked; when the connecting assembly 4 is in the second state, the first hoop body 1 and the second hoop body 2 are unlocked, so that the folding wing is separated from the projectile body;

[0048] A driving component, wherein the driving component is connected to the connecting component 4 and is used for switching the connecting component 4 between a first state and a second state.

[0049] Specifically, the first hoop body 1 and the second hoop body 2 are semicircular ring structures, thereby forming a circular embracing space between the first hoop body 1 and the second hoop body 2 to support the elastic body.

[0050] In some embodiments, the mounting parts 3 are provided at both ends of the first hoop body 1, and two folding wings are provided, which are respectively installed on the mounting parts 3; in other embodiments, the mounting parts 3 can also be provided at both ends of the second hoop body 2;

[0051] It needs to be further explained that, in the actual operation process, the elastic body needs to be clamped in the embracing space formed by the first hoop body 1 and the second hoop body 2, the first hoop body 1 is relatively arranged above the second hoop body 2, the elastic body and the second hoop body 2 are fixed together by fasteners, adhesives, etc., and the action of the driving component is controlled to lock the first hoop body 1 and the second hoop body 2.

[0052] When it is necessary to launch the projectile, the combined structure of the projectile, the folding wings and the folding wing unlocking device is launched as a whole; during the flight, the combined structure can control the folding wings to unfold so that the folding wings assist the projectile in flying; when the folding wings and the projectile need to be separated from each other, the driving assembly is controlled to switch to the second state, so that the first hoop body 1 and the second hoop body 2 are unlocked, thereby completing the separation of the folding wings from the projectile.

[0053] The installation, locking and unlocking process of the above structure is relatively simple, and there is no need to reserve installation space for gas cylinders and pipelines. The locking and unlocking of the projectile body and the folding wings are achieved by switching the mechanical structure state, thereby improving the reliability of the device.

[0054] In some embodiments, two connecting assemblies 4 are provided, and are respectively disposed between the first end of the first hoop body 1 and the first end of the second hoop body 2 and between the second end of the first hoop body 1 and the second end of the second hoop body 2 .

[0055] When the two connecting components 4 are in the second state, the two ends of the first hoop body 1 lose connection with the two ends of the second hoop body 2, that is, separation is achieved.

[0056] In some embodiments, the connection component 4 includes:

[0057] A locking body 41, wherein the locking body 41 is mounted on the end of the first hoop body 1, and an insertion groove 42 is formed on the locking body 41, and the end of the second hoop body 2 can be inserted into the insertion groove 42;

[0058] A wedge-shaped stopper 43, wherein the wedge-shaped stopper 43 is rotatably mounted in the insertion groove 42, and a clamping groove 22 is provided at the end of the second hoop body 2 corresponding to the wedge-shaped stopper 43;

[0059] When the connecting assembly 4 is in the first state, the wedge-shaped stopper 43 rotates into the clamping groove 22 to lock the first hoop body 1 and the second hoop body 2. Figure 1 and Figure 2 When the connecting assembly 4 is in the second state, the wedge-shaped stopper 43 moves in a direction away from the snap-fit ​​groove 22 to separate the first hoop body 1 and the second hoop body 2, as shown Figure 3 and Figure 4 shown.

[0060] Specifically, the locking body 41 and both ends of the first hoop body 1 may be an integrated structure or a split structure.

[0061] Specifically, the driving assembly is connected to the wedge-shaped stopper 43 to drive the wedge-shaped stopper 43 to rotate.

[0062] During installation, the end of the second hoop body 2 is inserted into the insertion groove 42 on the locking body 41, and the driving component drives the wedge-shaped stopper 43 to move, so that the wedge-shaped stopper 43 rotates into the clamping groove 22, thereby realizing the locking between the second hoop body 2 and the first hoop body 1; when unlocking is required, the driving component drives the wedge-shaped stopper 43 to move in the opposite direction, so that the wedge-shaped stopper 43 moves in the opposite direction away from the clamping groove 22, thereby realizing the unlocking between the second hoop body 2 and the first hoop body 1.

[0063] In some embodiments, the insertion groove 42 is arranged on the side of the locking body 41 close to each other; a first inclined surface 44 is arranged in the insertion groove 42 and close to the second hoop body 2; along the direction away from the center line of the clamp assembly, the distance from the first inclined surface 44 to the side of the insertion groove 42 away from the second hoop body 2 gradually decreases;

[0064] The first inclined surface 44 is provided with a mounting groove 45, and the wedge-shaped stopper 43 is rotatably mounted in the mounting groove 45 along a second direction, wherein the second direction is parallel to the center line of the clamp assembly;

[0065] A second inclined surface 21 is disposed at the end of the second hoop body 2 corresponding to the first inclined surface 44 , and the engaging groove 22 is disposed on the second inclined surface 21 .

[0066] Specifically, the locking body 41 is installed at both ends of the first hoop body 1, and the insertion groove 42 is installed on the side of the locking body 41 close to each other;

[0067] Since a first inclined surface 44 is provided in the insertion groove 42 and a second inclined surface 21 is provided at the end of the second hoop body 2 corresponding to the first inclined surface 44, in the unlocked state (i.e., the second state), relative movement between the second inclined surface 21 at the end of the second hoop body 2 and the first inclined surface 44 of the first hoop body 1 is facilitated, thereby facilitating disengagement.

[0068] In some embodiments, the first hoop body 1 includes a first sub-hoop body 11 and a second sub-hoop body 12 arranged at both ends of the first sub-hoop body 11; the first sub-hoop body 11 and the second sub-hoop body 12 are hinged along a first hinge axis; the first hinge axis is parallel to the center line of the clamp assembly.

[0069] Specifically, the locking body 41 is installed at the end of the second sub-hoop body 12; in the above structure, the second sub-hoop body 12 can rotate along the hinge axis, so when the connecting component 4 is in the unlocked state (ie, the second state), it is convenient for the second inclined surface 21 and the first inclined surface 44 to disengage from each other.

[0070] Furthermore, the first inclined surface 44 is an arc-shaped inclined surface, and the normal direction of the first inclined surface 44 intersects with the first hinge axis, so that the second sub-hoop body 12 can rotate along the first hinge axis and ensure that the separation can slide along the mechanical path to achieve mutual separation from the first hoop body 1.

[0071] Furthermore, graphite powder is coated between the first inclined surface 44 and the second inclined surface 21 to prevent adhesion or jamming between the two.

[0072] In some embodiments, an elastic member 46 is provided between the insertion groove 42 on a side away from the wedge-shaped stopper 43 and the end of the second hoop body 2 .

[0073] Furthermore, the elastic member 46 is a circular compression spring; when the connecting component 4 is in the first state, the elastic member 46 is in a compressed state; when the connecting component 4 is switched to the second state, the first hoop body 1 and the second hoop body 2 are unlocked, and at this time, under the elastic force of the elastic member 46, the first hoop body 1 and the second hoop body 2 are separated from each other; therefore, by setting the elastic member 46, a separation pushing force is provided, which is conducive to rapid separation.

[0074] In some embodiments, a spring pressure plate 47 is provided between the mounting groove 45 and the wedge-shaped stopper 43 , and the spring pressure plate 47 is used to provide a pre-tightening force to the wedge-shaped stopper 43 in a direction pointing to the clamping groove 22 .

[0075] Specifically, the spring pressure plate 47 is distributed in an S shape as a whole, and the bottom is a mounting flange surface. The mounting flange surface is provided with a mounting hole for fixing to the bottom of the mounting groove 45.

[0076] The spring pressure plate 47 is provided to provide a pre-tightening force for the wedge-shaped stopper 43 to prevent the wedge-shaped stopper 43 from vibrating off during the vibration process.

[0077] In some embodiments, the drive assembly comprises:

[0078] A rotating shaft 5, wherein the rotating shaft 5 is rotatably mounted in the inserting groove 42, and the wedge-shaped stopper 43 is fixedly mounted on the rotating shaft 5;

[0079] A driving motor 6, wherein an output end of the driving motor 6 is connected to the rotating shaft 5 through a gear set, and is used for driving the rotating shaft 5 to rotate along its axis.

[0080] Furthermore, the gear set includes a driving gear 7 and a driven gear 8 meshing with each other; the driving gear 7 is mounted on the driving motor 6, and the driven gear 8 is mounted on the rotating shaft 5;

[0081] Furthermore, the driving gear 7 and the driving motor 6 can be designed as an integrated structure to reduce the installation space and improve the transmission accuracy and structural strength;

[0082] Furthermore, the driven gear 8 and the rotating shaft 5 are an integrated structure, and the driven gear 8 is a standard spur gear, and the hardness of the tooth surface after quenching and tempering is RHC25-32; combining the driven gear 8 with the rotating shaft 5 can improve the structural strength and reduce the transmission error caused by the clearance fit;

[0083] Furthermore, the rotating shaft 5 is a stepped shaft, which can be circumferentially limited and installed with bearings; the rotating shaft 5 is rotatably installed in the insertion groove 42 by installing bearings 49 .

[0084] Furthermore, the wedge-shaped stopper 43 is fixed to the rotating shaft 5 via a flat key 48 .

[0085] In some embodiments, the folding-wing unlocking device further includes: a control unit; the control unit is configured to receive control instructions and control the action of the driving component to switch the first state and the second state of the connecting component.

[0086] Specifically, the control unit may receive the information in a wireless manner. For example, when the control unit receives a first control instruction, the control unit controls the driving component to operate, and the driving component drives the connecting component to switch to the first state; when the control unit receives a second control instruction, the control unit controls the driving component to operate, and the driving component drives the connecting component to switch to the second state.

[0087] Example 2

[0088] The present embodiment provides a folding wing unlocking system, comprising a folding wing 9, a body and a plurality of folding wing unlocking devices as described above; each of the folding wing unlocking devices is arranged along the axial direction of the body; the body is clamped into the clamping space of each clamping assembly, and the folding wing 9 is connected to the mounting portion 3 of each clamping assembly.

[0089] Specifically, the folding wings 9 are respectively arranged on both sides of the projectile body (i.e., the folding wing unlocking device), wherein the folding wings 9 on one side of the projectile body are as follows: Fig.12 shown.

[0090] The above description is only a preferred embodiment of the present application and an explanation of the technical principles used. Those skilled in the art should understand that the scope of the invention involved in the present application is not limited to the technical solution formed by a specific combination of the above technical features, but should also cover other technical solutions formed by any combination of the above technical features or their equivalent features without departing from the inventive concept. For example, the above features are replaced with (but not limited to) technical features with similar functions disclosed in the present application.

Claims

1. A folding wing unlocking device, characterized in that: include: A hoop assembly, the hoop assembly comprising a first hoop body (1) and a second hoop body (2), wherein an embracing space for embracing an elastic body is formed between the first hoop body (1) and the second hoop body (2); a mounting portion (3) for mounting the folding wing is provided on the first hoop body (1) or the second hoop body (2); A connecting assembly (4), the connecting assembly (4) being installed between the first hoop body (1) and the second hoop body (2), the connecting assembly (4) having a first state and a second state; when the connecting assembly (4) is in the first state, the first hoop body (1) and the second hoop body (2) are locked; when the connecting assembly (4) is in the second state, the first hoop body (1) and the second hoop body (2) are unlocked, so that the folding wing is separated from the projectile body; a driving component, the driving component being connected to the connecting component (4) and being used to switch the connecting component (4) between a first state and a second state; The connection component (4) comprises: A locking body (41), the locking body (41) being mounted on the end of the first hoop body (1), the locking body (41) being provided with an insertion groove (42), the end of the second hoop body (2) being insertable into the insertion groove (42); A wedge-shaped stopper (43), the wedge-shaped stopper (43) being rotatably mounted in the insertion groove (42), and a clamping groove (22) being provided at the end of the second hoop body (2) corresponding to the wedge-shaped stopper (43); Wherein, when the connecting assembly (4) is in a first state, the wedge-shaped stopper (43) rotates into the clamping groove (22) to lock the first hoop body (1) and the second hoop body (2); when the connecting assembly (4) is in a second state, the wedge-shaped stopper (43) moves in a direction away from the clamping groove (22) to separate the first hoop body (1) and the second hoop body (2); The insertion groove (42) is arranged on a side of the locking body (41) close to each other; a first inclined surface (44) is arranged in the insertion groove (42) and close to the second hoop body (2); along the direction away from the center line of the clamp assembly, the distance from the first inclined surface (44) to the side of the insertion groove (42) away from the second hoop body (2) gradually decreases; The first inclined surface (44) is provided with a mounting groove (45), and the wedge-shaped stopper (43) is mounted in the mounting groove (45) so as to be rotatable along a second direction, wherein the second direction is parallel to the center line of the clamp assembly; The end of the second hoop body (2) is provided with a second inclined surface (21) corresponding to the first inclined surface (44), and the clamping groove (22) is arranged on the second inclined surface (21).

2. The folding wing unlocking device according to claim 1, characterized in that: The connecting components (4) are provided in two pieces and are respectively arranged between the first end of the first hoop body (1) and the first end of the second hoop body (2), and between the second end of the first hoop body (1) and the second end of the second hoop body (2).

3. The folding wing unlocking device according to claim 1, characterized in that: The first hoop body (1) comprises a first sub-hoop body (11) and a second sub-hoop body (12) arranged at two ends of the first sub-hoop body (11); the first sub-hoop body (11) and the second sub-hoop body (12) are hinged along a first hinge axis; the first hinge axis is parallel to the center line of the clamp assembly.

4. The folding wing unlocking device according to claim 1, characterized in that: An elastic member (46) is provided between the insertion groove (42) and the end of the second hoop body (2), on a side away from the wedge-shaped stopper (43).

5. The folding wing unlocking device according to claim 1, characterized in that: A spring pressure plate (47) is provided between the installation groove (45) and the wedge-shaped stopper (43), and the spring pressure plate (47) is used to provide a pre-tightening force to the wedge-shaped stopper (43) in a direction pointing toward the clamping groove (22).

6. The folding wing unlocking device according to claim 1, characterized in that: The drive assembly comprises: A rotating shaft (5), the rotating shaft (5) being rotatably mounted in the insertion groove (42), and the wedge-shaped stopper (43) being fixedly mounted on the rotating shaft (5); A drive motor (6), wherein an output end of the drive motor (6) is connected to the rotating shaft (5) via a gear set, and is used to drive the rotating shaft (5) to rotate along its axis.

7. The folding wing unlocking device according to any one of claims 1 to 6, characterized in that: Also includes: A control unit; the control unit is configured to receive control instructions and control the action of the drive component to switch the first state and the second state of the connection component.

8. A folding wing unlocking system, comprising a folding wing, a body and a plurality of folding wing unlocking devices as described in any one of claims 1 to 7; each of the folding wing unlocking devices is arranged along the axial direction of the body; the body is snapped into the clamping space of each clamping hoop assembly, and the folding wing is connected to the mounting portion (3) of each clamping hoop assembly.

Citation Information

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