Light and small airborne suspension release device
By adopting a combination design of connecting rod mechanism and elastic components in the airborne suspension device, the problems of large size and heavy weight in the existing technology are solved, and the lightweight and flexible configuration is achieved, adapting to the needs of narrow spaces, and reducing the Air resistance and maintenance costs.
Patent Information
- Application Number
- CN202411531442.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2024-10-30
- Publication Date
- 2024-12-31
AI Technical Summary
The existing air-mounted suspension devices are large in size and heavy in weight, making them difficult to meet the needs of narrow spaces, and the suspension point position cannot be flexibly adjusted.
Adopting a structural design based on linkage mechanism and elastic components to realize passive driving lightweight and miniaturized airborne suspension release device, including a load bearing mechanism and unlocking mechanism, and realize suspension through linkage components, locking latch assembly and unlocking slide rod and other components. The device is small in size, light in weight and flexible in configuration.
The suspension device is small in size and light in weight, and can be flexibly configured according to the number and position of the lifting points, reducing the impact of air resistance and simplifying the maintenance and installation process.
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Figure CN119218418A_ABST
Abstract
Description
Technical Field
[0001] The invention belongs to the technical field of aviation and weapon equipment connection and separation mechanisms, and in particular relates to a light and miniaturized airborne suspension release device. Background Art
[0002] The airborne suspension device mainly adopts catapult launch, push-off catapult launch, and rail launch, and each launch method has specific requirements for the hook of the suspension. Most of the existing suspension devices are pneumatic or hydraulic, and the front and rear suspension points are designed as an integrated type. For medium and large suspensions, the existing suspension devices weigh from tens of kilograms to hundreds of kilograms, have large dimensions (height dimension is not less than 10 cm), have high requirements for installation space and aircraft carrying capacity, and cannot be flexibly adjusted according to the front and rear suspension point positions of the suspension.
[0003] As the weight of onboard suspension objects gradually increases, the onboard suspension devices are required to occupy small space, be light, and occupy less system resources, due to the constraints of factors such as body size design and weight indicators. Therefore, there is an urgent need for lightweight and miniaturized suspension release devices. Summary of the invention
[0004] The technology of the present invention solves the problem: overcomes the shortcomings of the prior art, provides a lightweight and miniaturized airborne suspension release device, and realizes passive drive of the suspension device based on the structural design combining a connecting rod mechanism and an elastic element. The entire device has the characteristics of small size and light weight, and the device can be flexibly configured according to the number and position of the suspension points; it solves the problem that the existing airborne suspension device has large external dimensions and heavy weight, and is difficult to adapt to the requirements of the airborne suspension device in a small space.
[0005] In order to solve the above technical problems, the present invention discloses a lightweight and miniaturized airborne suspension release device, comprising: a bearing mechanism and an unlocking mechanism;
[0006] The bearing mechanism is provided with a mechanical interface fixedly connected to the mounting platform, and a mounting interface connected to the load hook;
[0007] The unlocking mechanism is installed on the supporting mechanism; wherein, when the unlocking mechanism and the supporting mechanism are installed, the unlocking mechanism conical hole on the unlocking mechanism and the supporting mechanism conical hole on the supporting mechanism are positioned and matched, and are fixedly connected by screws after being installed in place.
[0008] In the above-mentioned lightweight and miniaturized airborne suspension release device, the bearing mechanism includes: a mounting assembly, a connecting rod assembly, a locking latch assembly, an unlocking slide rod, an in-place feedback assembly and an electrical connector; wherein the connecting rod assembly is installed on the mounting column of the mounting assembly to form a rotating pair connection; the locking latch assembly is connected to the mounting assembly by a screw to limit the movement of the connecting rod assembly; the unlocking slide rod passes through the mounting assembly and is connected to the locking latch assembly by a nut, and can slide in the mounting assembly; the in-place feedback assembly and the electrical connector are respectively installed on the mounting assembly through brackets.
[0009] In the above-mentioned lightweight and miniaturized airborne suspension release device, the mounting assembly includes: gripper I, gripper II, mounting base, side mounting plate I, gripper torsion spring, side mounting plate II and mounting column; wherein, gripper I and gripper II are respectively mounted with the mounting base through shaft holes; gripper torsion spring is installed on gripper I and gripper II; side mounting plate I and side mounting plate II are respectively fixedly connected with the mounting base through screws to form gripper I, gripper II and gripper torsion spring with the mounting base as a whole.
[0010] In the above-mentioned lightweight and miniaturized airborne suspension release device, in the initial state, grasping claws I and II are in an open state under the action of grasping claw torsion springs; when mounting, the load hook is installed upward, and the load hook acts on the locking tongues of grasping claws I and II, so that grasping claws I and II overcome the spring force of the grasping claw torsion springs and retract toward the middle, thereby locking the load hook.
[0011] In the above-mentioned light and miniaturized airborne suspension release device, the connecting rod assembly includes: a catch, a connecting rod I, a swing arm, a connecting rod II, a center turntable I, a connecting rod III, a center turntable II, a rocker torsion spring, a rocker, a rocker support and a connecting rod IV; wherein, the catch, the connecting rod I, the swing arm, the connecting rod II and the center turntable I are connected by pins to form a rotation pair I at the connection; the catch, the connecting rod I, the swing arm, the connecting rod III and the center turntable II are connected by pins to form a rotation pair II at the connection; the center turntable I is installed on the center turntable II for a fixed connection; the rocker torsion spring and the rocker are installed on the rocker support by pins; the rocker and the swing arm are connected by connecting rod IV to form a rotation pair connection; the rocker support is fixed to the mounting base by screws.
[0012] In the above-mentioned lightweight and miniaturized airborne suspension release device, in the initial state, under the action of the rocker torsion spring, gripper I and gripper II, the gripper is in an open state; when gripper I and gripper II are folded into place, the rocker is rotated to drive the gripper to close through connecting rods I, II, III and IV, contacting the side planes of gripper I and II, and clamping gripper I and II.
[0013] In the above-mentioned lightweight and miniaturized airborne suspension release device, the locking latch assembly includes: a latch spring, a spring sleeve, a locking latch and a latch connecting plate; wherein the latch spring and the spring sleeve are installed on the locking latch to generate pre-compression on the latch spring, the locking latch can move axially on the spring sleeve, and the latch connecting plate is fixed to the locking latch by a nut; the locking latch assembly is fixedly connected to the mounting base by the spring sleeve, and after the connection is completed, the locking latch can move axially.
[0014] In the above-mentioned lightweight and miniaturized airborne suspension release device, in the initial state, the latch spring is in a compressed state, the latch end of the locking latch contacts the side of the center turntable II, and forms a sliding pair; when the rocker is rotated, the connecting rods I, II, III and IV drive the center turntables I and II to rotate, and a latch locking groove is provided on the center turntable II. After the center turntables I and II are rotated into place, the locking latch is inserted into the latch locking groove on the center turntable II under the action of the latch spring to achieve locking.
[0015] In the above-mentioned lightweight and miniaturized airborne suspension release device, the unlocking slide rod passes through the mounting base and is connected to the pin connecting plate by a nut; a safety pin hole and a manual unlocking groove are provided on the unlocking slide rod; when the load hook is locked by the bearing mechanism, the safety pin is inserted into the safety pin hole on the unlocking slide rod to ensure that the locking pin will not accidentally fall out of the pin locking groove on the center turntable II, causing accidental unlocking of the bearing mechanism; when manual unlocking is required, one end of the safety pin is inserted into the manual unlocking groove of the unlocking slide rod, and the rocker support is used as a lever fulcrum to pry the unlocking slide rod to move in the mounting base, thereby driving the locking pin to unlock the connecting rod assembly; a status indication feature is provided on the unlocking slide rod to indicate whether the locking pin is locked in place.
[0016] In the above-mentioned lightweight and miniaturized airborne suspension release device, the unlocking mechanism includes: a mounting bracket, an unlocking slider, an unlocking spring, a spring guide column, a locking push rod, a pressure plate, a cushion block, an unlocker, a clamping rod, a pull rod spring and a capture cap; wherein, the unlocking slider and the unlocking spring are mounted on the mounting bracket through the spring guide column, and the unlocking slider can move axially along the spring guide column; the locking push rod is fixed to the unlocking slider through a nut; the unlocker, the cushion block and the capture cap are fixed to the mounting bracket through screws; when locking, the clamping rod passes through the pressure plate and is screwed into the unlocker, and one end of the locking push rod is compressed through the pressure plate, so that the unlocking spring is in a compressed state; the pull rod spring is installed between the pressure plate and the cushion block, and passes through the clamping rod and is in a compressed state.
[0017] The present invention has the following advantages:
[0018] (1) The present invention discloses a lightweight and miniaturized airborne suspension release device. Based on the structural design combining a connecting rod mechanism and an elastic element, the suspension device is passively driven. The entire device has the characteristics of small size and light weight, and the device can be flexibly configured according to the number and position of suspension points. The problem that the existing airborne suspension device is large in size and heavy in weight, and is difficult to adapt to the requirements of the airborne suspension device in a small space is solved.
[0019] (2) The present invention discloses a lightweight and miniaturized airborne suspension release device, which places the connecting rod assembly horizontally and utilizes the force-increasing effect of the dead point position of the connecting rod assembly to achieve a small size and large load-bearing effect. Compared with traditional airborne suspension devices, under the same load level, its height dimension is only 1 / 3 of that of traditional suspension devices, which can effectively reduce the impact of air resistance during flight.
[0020] (3) The present invention discloses a lightweight and miniaturized airborne suspension release device, which uses a spring to realize the unlocking drive of the airborne suspension device, so the suspension device does not need to carry an additional cylinder or oil cylinder, which effectively reduces the weight of the airborne suspension device. At the same time, a small unlocker is used as a trigger source, which reduces the requirements for platform resources.
[0021] (4) The present invention discloses a lightweight and miniaturized airborne suspension release device. Compared with the integrated design of the front and rear suspension points of the traditional suspension device, the present invention adopts a design concept in which the front and rear suspension points are completely independent. A single set of the lightweight and miniaturized airborne suspension release device described in the present invention can meet the independent mounting of one suspension point and can be flexibly configured according to different suspension point positions and quantities.
[0022] (5) The present invention discloses a lightweight and miniaturized airborne suspension release device, in which the bearing mechanism and the unlocking mechanism are modularly split in design. When the unlocking is completed, only the unlocking mechanism needs to be removed for resetting, so that the resetting and maintenance of the device are convenient and quick. When the unlocking device uses pyrotechnics, it can be installed before the airborne suspension device is used, which reduces the maintenance cost on the ground. BRIEF DESCRIPTION OF THE DRAWINGS
[0023] Figure 1 It is a structural schematic diagram of a lightweight and miniaturized airborne suspension release device in an embodiment of the present invention;
[0024] Figure 2 is a structural schematic diagram of a bearing mechanism in an embodiment of the present invention;
[0025] Figure 3 is a structural schematic diagram of a mounting component in an embodiment of the present invention;
[0026] Figure 4 is a structural schematic diagram of a connecting rod assembly in an embodiment of the present invention;
[0027] Figure 5 is a structural schematic diagram of a locking latch assembly in an embodiment of the present invention;
[0028] Figure 6 is a schematic structural diagram of an unlocking slide bar in an embodiment of the present invention;
[0029] Figure 7 This is a schematic diagram of a structure of a grabbing method according to an embodiment of the present invention;
[0030] Figure 8 It is a structural schematic diagram of an unlocking mechanism in an embodiment of the present invention. DETAILED DESCRIPTION
[0031] In order to make the objectives, technical solutions and advantages of the present invention more clear, the embodiments disclosed in the present invention will be further described in detail below with reference to the accompanying drawings.
[0032] In order to adapt to the requirements of narrow space, rapid response and flattening of airborne suspension devices in some application scenarios, the present invention proposes a lightweight and miniaturized airborne suspension release device that can realize passive drive and adopts a horizontally placed connecting rod mechanism to solve the problems of large size and weight of existing devices. The suspension device is divided into two independent front and rear devices, which can flexibly adapt to suspension points with different spacings.
[0033] Reference Figures 1 to 8 In this embodiment, the light and miniaturized airborne suspension release device includes: a bearing mechanism 100 and an unlocking mechanism 200. The bearing mechanism 100 is provided with a mechanical interface fixedly connected to the mounting platform and a mounting interface connected to the load hook. The unlocking mechanism 200 is installed on the bearing mechanism 100; when the unlocking mechanism 200 is installed with the bearing mechanism 100, the unlocking mechanism conical hole on the unlocking mechanism 200 is positioned and matched with the bearing mechanism conical hole on the bearing mechanism 100, and is fixedly connected by screws after being installed in place.
[0034] Carrying mechanism
[0035] In this embodiment, the bearing mechanism 100 mainly includes: a mounting assembly, a connecting rod assembly, a locking latch assembly, an unlocking slide bar 19, an in-position feedback assembly 14 and an electrical connector 13. Among them, the connecting rod assembly is installed on the mounting column 25 of the mounting assembly to form a revolving pair connection; the locking latch assembly is connected to the mounting assembly by screws to limit the movement of the connecting rod assembly; the unlocking slide bar 19 passes through the mounting assembly and is connected to the locking latch assembly by nuts, and can slide in the mounting assembly; the in-position feedback assembly 14 and the electrical connector 13 are respectively installed on the mounting assembly through brackets.
[0036] Mounting Components
[0037] In this embodiment, the mounting assembly mainly includes: gripper I1, gripper II2, mounting base 10, side mounting plate I11, gripper torsion spring 12, side mounting plate II20 and mounting column 25. Among them, gripper I1 and gripper II2 are respectively mounted with mounting base 10 through shaft holes; gripper torsion spring 12 is mounted on gripper I1 and gripper II2; side mounting plate I11 and side mounting plate II20 are respectively fixedly connected with mounting base 10 through screws, so that gripper I1, gripper II2 and gripper torsion spring 12 are integrated with mounting base 10.
[0038] In the initial state, the grabber Ⅰ1 and the grabber Ⅱ2 are in an open state under the action of the grabber torsion spring 12; when mounting, the load hook is installed upward, and the load hook acts on the locking tongues of the grabber Ⅰ1 and the grabber Ⅱ2, so that the grabber Ⅰ1 and the grabber Ⅱ2 overcome the spring force of the grabber torsion spring 12 and retract to the middle, thereby locking the load hook.
[0039] Connecting rod assembly
[0040] In this embodiment, the connecting rod assembly mainly includes: a clamping grip 3, a connecting rod I4, a swing arm 5, a connecting rod II6, a center turntable I7, a connecting rod III8, a center turntable II9, a rocker torsion spring 21, a rocker 22, a rocker support 23 and a connecting rod IV24. Among them, the clamping grip 3, the connecting rod I4, the swing arm 5, the connecting rod II6 and the center turntable I7 are connected by pins to form a rotation pair I at the connection; the clamping grip 3, the connecting rod I4, the swing arm 5, the connecting rod III8 and the center turntable II9 are connected by pins to form a rotation pair II at the connection; the center turntable I7 is installed on the center turntable II9, which is a fixed connection. When the center turntable I7 and the center turntable II9 rotate in step, the clamping grip 3 can be driven to expand or close; the rocker torsion spring 21 and the rocker 22 are installed on the rocker support 23 by pins; the rocker 22 is connected to the swing arm 5 by the connecting rod IV24 to form a rotation pair connection, and the clamping grip 3 can be driven to expand or close by rotating the rocker 22. The connecting rod assembly is installed on the mounting column 25 of the mounting assembly through the clamp 3, the swing arm 5, the center turntable I7 and the center turntable II9, and is fixed by the shaft end retaining ring to form a rotating pair; the rocker support 23 is fixed on the mounting base 10 by screws.
[0041] In the initial state, under the action of the rocker torsion spring 21, gripper Ⅰ1 and gripper Ⅱ2, the clamping claw 3 is in an open state; when gripper Ⅰ1 and gripper Ⅱ2 are folded into place, the rocker 22 is rotated to drive the clamping claw 3 to close through the connecting rod Ⅰ4, connecting rod Ⅱ6, connecting rod Ⅲ8 and connecting rod Ⅳ24, contacting with the side planes of gripper Ⅰ1 and gripper Ⅱ2, and clamping gripper Ⅰ1 and gripper Ⅱ2.
[0042] Locking pin assembly
[0043] In this embodiment, the locking latch assembly mainly includes: a latch spring 15, a spring sleeve 16, a locking latch 17 and a latch connecting plate 18. The latch spring 15 and the spring sleeve 16 are installed on the locking latch 17 to generate pre-compression on the latch spring 15, and the locking latch 17 can move axially on the spring sleeve 16. The latch connecting plate 18 is fixed to the locking latch 17 by a nut; the locking latch assembly is fixedly connected to the mounting base 10 through the spring sleeve 16, and after the connection is completed, the locking latch 17 can move axially.
[0044] In the initial state, the latch spring 15 is in a compressed state, and the latch end of the locking latch 17 contacts the side of the center turntable Ⅱ9 to form a sliding pair; when the rocker 22 is rotated, the connecting rods Ⅰ4, Ⅱ6, Ⅲ8 and Ⅳ24 drive the center turntable Ⅰ7 and the center turntable Ⅱ9 to rotate, and a latch locking groove is provided on the center turntable Ⅱ9. After the center turntable Ⅰ7 and the center turntable Ⅱ9 are rotated into place, the locking latch 17 is inserted into the latch locking groove on the center turntable Ⅱ9 under the action of the latch spring 15 to achieve locking.
[0045] Unlock Slide
[0046] In this embodiment, the unlocking slide bar 19 passes through the mounting base 10 and is connected to the latch connecting plate 18 by a nut; a safety pin socket and a manual unlocking groove are provided on the unlocking slide bar 19; when the load hook is locked by the bearing mechanism 100, the safety pin 300 is inserted into the safety pin socket on the unlocking slide bar 19 to ensure that the locking latch 17 will not accidentally fall out of the latch locking groove on the center turntable II9, causing the bearing mechanism 100 to be accidentally unlocked; when manual unlocking is required, one end of the safety pin 300 is inserted into the manual unlocking groove of the unlocking slide bar 19, and the rocker support 23 is used as a lever fulcrum to pry the unlocking slide bar 19 to move in the mounting base 10, thereby driving the locking latch 17 to unlock the connecting rod assembly; a status indication feature is provided on the unlocking slide bar 19 to indicate whether the locking latch 17 is locked in place.
[0047] Unlocking mechanism
[0048] In this embodiment, the unlocking mechanism 200 mainly includes: a mounting bracket 36, an unlocking slider 26, an unlocking spring 27, a spring guide column 28, a locking push rod 29, a pressure plate 30, a cushion block 31, an unlocker 32, a clamping rod 33, a pull rod spring 34 and a capture cap 35. Among them, the unlocking slider 26 and the unlocking spring 27 are mounted on the mounting bracket 36 through the spring guide column 28, and the unlocking slider 26 can move in the axial direction along the spring guide column 28; the locking push rod 29 is fixed on the unlocking slider 26 through a nut; the unlocker 32, the cushion block 31 and the capture cap 35 are fixed on the mounting bracket 36 through screws; when locking, the clamping rod 33 passes through the pressure plate 30 and is screwed into the unlocker 32, and one end of the locking push rod 29 is compressed through the pressure plate 30, so that the unlocking spring 27 is in a compressed state; the pull rod spring 34 is installed between the pressure plate 30 and the cushion block 31, and passes through the clamping rod 33 in a compressed state.
[0049] It should be noted that the unlocker can be a pyrotechnic unlocker or a non-pyrotechnic unlocker according to actual needs, and only the unlocking interface of the unlocker on the mounting bracket needs to be adjusted.
[0050] In this embodiment, after the unlocking mechanism 200 is installed on the bearing mechanism 100, the notch of the unlocking slider 26 passes through the locking pin 17 and hooks the locking pin 17 through the nut. In the locked state, the pressing rod 33 presses the locking push rod 29 with the cushion block 31 through the pressing plate 30, and the locking push rod 29 is fixedly connected to the unlocking slider 26 to compress the unlocking spring 27. When unlocking, the unlocker 32 unlocks and releases the pressing rod 33, and the pressing plate 30 is separated from the cushion block 31 under the action of the pull rod spring 34 and the locking push rod 29. The locking push rod 29 and the unlocking slider 26 move under the action of the unlocking spring 27, driving the locking pin 17 to be pulled out and contacting the connecting rod assembly to limit the position.
[0051] Based on the above embodiment, the working process of the light and small-sized airborne suspension release device is briefly described below. In this embodiment, the working process of the light and small-sized airborne suspension release device is as follows:
[0052] 1) Device installation. First, connect the carrying mechanism to the aircraft or other carrier platform through screws, and then install the unlocking mechanism on the carrying mechanism. At this time, the carrying mechanism is in the initial state, the unlocking mechanism is in the locked state, and the unlocking slider of the unlocking mechanism is limited by the nut on the locking pin of the carrying mechanism to achieve connection.
[0053] 2) Load suspension. The light and small airborne suspension release device includes three steps from the initial state to the load mounting locking: First, the load hook contacts the locking tongues of the gripper I and the gripper II and continues to move, and the gripper I and the gripper II begin to close together until the gripper I and the gripper II are closed in place. Next, manually turn the rocker to clamp the gripper I and the gripper II, and insert the locking pin into the pin space of the center turntable II to complete the mechanism locking. Finally, observe whether the status indicator of the unlocking slide bar shows that it is locked in place. If it shows that it is in place, insert the safety pin into the safety pin socket of the unlocking slide bar.
[0054] 3) Load delivery. Load delivery is divided into two modes: manual unlocking and power-on automatic delivery. Manual unlocking is mainly for ground testing, device maintenance or other situations, and power-on automatic delivery is for load airdrop scenarios. Among them, manual unlocking and delivery includes two steps: first, pull out the safety pin, and insert the safety pin (or other tools) into the manual unlocking groove of the unlocking slide bar, use the rocker support as a fulcrum, pry the unlocking slide bar to move in the mounting base, and drive the locking pin out of the pin hole of the center turntable II; then, the connecting rod mechanism and the gripper are opened under the action of the gripper torsion spring and the gravity of the load to realize manual load delivery; after manual unlocking and delivery, the load-bearing mechanism is in the initial state, and the unlocking mechanism is in the locked state. Automatic release upon power-on includes three steps: first, pull out the safety pin; then, after reaching the specified position, the unlocker is powered on to unlock, the limit on the clamping rod is released, the pressure plate is lifted up by the pull rod spring and the locking push rod, and the unlocking slider pulls the locking pin out of the pin hole of the center turntable II under the action of the unlocking spring; finally, the connecting rod assembly and the gripper are opened under the action of the gripper torsion spring and the gravity of the load, realizing automatic release of the load upon power-on. After automatic release upon power-on, the load-bearing mechanism is in the initial state and the unlocking mechanism is in the unlocked state.
[0055] It should be noted that the above is only one embodiment of the technical solution of the present invention, and the structural dimensions can be changed according to actual needs to achieve load locking pre-release under different bearing capacities.
[0056] Although the present invention has been disclosed as above in the form of a preferred embodiment, it is not intended to limit the present invention. Any person skilled in the art may make possible changes and modifications to the technical solution of the present invention by using the methods and technical contents disclosed above without departing from the spirit and scope of the present invention. Therefore, any simple modifications, equivalent changes and modifications made to the above embodiments based on the technical essence of the present invention without departing from the content of the technical solution of the present invention shall fall within the protection scope of the technical solution of the present invention.
[0057] The contents not described in detail in the specification of the present invention belong to the common knowledge of the professionals in this field.
Claims
1. A lightweight and miniaturized airborne suspension release device, characterized in that: include: A carrying mechanism (100) and an unlocking mechanism (200); The bearing mechanism (100) is provided with a mechanical interface fixedly connected to the mounting platform, and a mounting interface connected to the load hook; The unlocking mechanism (200) is installed on the supporting mechanism (100); wherein, when the unlocking mechanism (200) and the supporting mechanism (100) are installed, the unlocking mechanism conical hole on the unlocking mechanism (200) is positioned and matched with the supporting mechanism conical hole on the supporting mechanism (100), and after being installed in place, they are fixedly connected by screws.
2. The light and miniaturized airborne suspension release device according to claim 1, characterized in that: The bearing mechanism (100) comprises: a mounting assembly, a connecting rod assembly, a locking latch assembly, an unlocking slide bar (19), an in-position feedback assembly (14) and an electrical connector (13); wherein the connecting rod assembly is mounted on a mounting column (25) of the mounting assembly to form a rotating pair connection; the locking latch assembly is connected to the mounting assembly via a screw to limit the movement of the connecting rod assembly; the unlocking slide bar (19) passes through the mounting assembly and is connected to the locking latch assembly via a nut to slide in the mounting assembly; the in-position feedback assembly (14) and the electrical connector (13) are respectively mounted on the mounting assembly via brackets.
3. The light and miniaturized airborne suspension release device according to claim 2 is characterized in that: The mounting assembly comprises: a gripper I (1), a gripper II (2), a mounting base (10), a side mounting plate I (11), a gripper torsion spring (12), a side mounting plate II (20) and a mounting column (25); wherein the gripper I (1) and the gripper II (2) are respectively mounted on the mounting base (10) through shaft holes; the gripper torsion spring (12) is mounted on the gripper I (1) and the gripper II (2); the side mounting plate I (11) and the side mounting plate II (20) are respectively fixedly connected to the mounting base (10) through screws, so that the gripper I (1), the gripper II (2) and the gripper torsion spring (12) are integrated with the mounting base (10).
4. The light and miniaturized airborne suspension release device according to claim 3 is characterized in that: In the initial state, the gripper I (1) and the gripper II (2) are in an open state under the action of the gripper torsion spring (12); when loading, the load hook is installed upward, and the load hook acts on the locking tongues of the gripper I (1) and the gripper II (2), so that the gripper I (1) and the gripper II (2) overcome the spring force of the gripper torsion spring (12) and retract toward the middle, thereby locking the load hook.
5. The light and small-sized airborne suspension release device according to claim 3 is characterized in that: The connecting rod assembly comprises: a clamping grip (3), a connecting rod I (4), a swing arm (5), a connecting rod II (6), a center rotating disk I (7), a connecting rod III (8), a center rotating disk II (9), a rocker torsion spring (21), a rocker (22), a rocker support (23) and a connecting rod IV (24); wherein the clamping grip (3), the connecting rod I (4), the swing arm (5), the connecting rod II (6) and the center rotating disk I (7) are connected by a pin, and a rotating pair I is formed at the connection; the clamping grip (3), the connecting rod I ( 4), the swing arm (5), the connecting rod III (8) and the center turntable II (9) are connected by pins, and a rotation pair II is formed at the connection; the center turntable I (7) is installed on the center turntable II (9) for fixed connection; the rocker torsion spring (21) and the rocker (22) are installed on the rocker support (23) by pins; the rocker (22) and the swing arm (5) are connected by connecting rod IV (24) to form a rotation pair connection; the rocker support (23) is fixed on the mounting base (10) by screws.
6. The light and miniaturized airborne suspension release device according to claim 5, characterized in that: In the initial state, under the action of the rocker torsion spring (21), the gripper I (1) and the gripper II (2), the gripper (3) is in an open state; when the gripper I (1) and the gripper II (2) are retracted into place, the rocker (22) is rotated to drive the gripper (3) to close through the connecting rod I (4), the connecting rod II (6), the connecting rod III (8) and the connecting rod IV (24), and the gripper (3) contacts the side planes of the gripper I (1) and the gripper II (2), thereby clamping the gripper I (1) and the gripper II (2).
7. The light and small-sized airborne suspension release device according to claim 5, characterized in that: The locking bolt assembly comprises: a bolt spring (15), a spring sleeve (16), a locking bolt (17) and a bolt connecting plate (18); wherein the bolt spring (15) and the spring sleeve (16) are mounted on the locking bolt (17) to generate pre-compression on the bolt spring (15); the locking bolt (17) can move axially on the spring sleeve (16); the bolt connecting plate (18) is fixed to the locking bolt (17) by a nut; the locking bolt assembly is fixedly connected to a mounting base (10) by the spring sleeve (16); after the connection is completed, the locking bolt (17) can move axially.
8. The light and miniaturized airborne suspension release device according to claim 7, characterized in that: In the initial state, the latch spring (15) is in a compressed state, and the latch end of the locking latch (17) contacts the side of the center turntable II (9) to form a sliding pair; when the rocker (22) is rotated, the connecting rods I (4), II (6), III (8) and IV (24) drive the center turntable I (7) and the center turntable II (9) to rotate, and a latch locking groove is provided on the center turntable II (9). After the center turntable I (7) and the center turntable II (9) are rotated to the right position, the locking latch (17) is inserted into the latch locking groove on the center turntable II (9) under the action of the latch spring (15) to achieve locking.
9. The light and small-sized airborne suspension release device according to claim 7, characterized in that: The unlocking slide bar (19) passes through the mounting base (10) and is connected to the latch connecting plate (18) through a nut; a safety pin insertion hole and a manual unlocking groove are provided on the unlocking slide bar (19); when the load hook is locked by the bearing mechanism (100), the safety pin (300) is inserted into the safety pin insertion hole on the unlocking slide bar (19) to ensure that the locking latch (17) will not accidentally fall out of the latch locking groove on the central rotating disk II (9), causing the bearing mechanism (100) to be accidentally unlocked; when manual unlocking is required, one end of the safety pin (300) is inserted into the manual unlocking groove of the unlocking slide bar (19), and the rocker support (23) is used as a lever fulcrum to pry the unlocking slide bar (19) to move in the mounting base (10), thereby driving the locking latch (17) to unlock the connecting rod assembly; a status indication feature is provided on the unlocking slide bar (19) to indicate whether the locking latch (17) is locked in place.
10. The light and miniaturized airborne suspension release device according to claim 9, characterized in that: The unlocking mechanism (200) comprises: a mounting bracket (36), an unlocking slider (26), an unlocking spring (27), a spring guide column (28), a locking push rod (29), a pressure plate (30), a cushion block (31), an unlocker (32), a pressing rod (33), a rod pulling spring (34) and a capture cap (35); wherein the unlocking slider (26) and the unlocking spring (27) are mounted on the mounting bracket (36) via the spring guide column (28), and the unlocking slider (26) can move in an axial direction along the spring guide column (28); The locking push rod (29) is fixed to the unlocking slider (26) by a nut; the unlocker (32), the cushion block (31) and the capture cap (35) are fixed to the mounting bracket (36) by screws; when locking, the pressing rod (33) passes through the pressure plate (30) and is screwed into the unlocker (32), and one end of the locking push rod (29) is pressed by the pressure plate (30), so that the unlocking spring (27) is in a compressed state; the pull rod spring (34) is installed between the pressure plate (30) and the cushion block (31), and passes through the pressing rod (33) and is in a compressed state.
Citation Information
Patent Citations
A locking and releasing mechanism
CN105474775B
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FR3146460A1