Magnetic attraction control satellite unlocking and separating device

Abstract

The utility model relates to the technical field of spaceflight, in particular to a magnetic attraction control satellite unlocking and separating device which comprises a mounting frame, a plurality of bases are arranged at the upper end of the mounting frame, and the bases are distributed along the upper end of the mounting frame in an array mode. The separating mechanism is arranged at the upper end of the base; wherein the separation mechanism comprises an outer frame fixedly connected to the upper end of the base, a positioning assembly is arranged in the outer frame, and the surface of the positioning assembly penetrates through the outer part of the outer frame; according to the device, a double-limiting effect can be formed under the action of a separating mechanism, when a limiting clamping pipe is reset, an upper limiting plate can be driven to move along with the limiting clamping pipe, at the moment, the limiting clamping pipe can relieve limiting on a second clamping block, meanwhile, the limiting clamping pipe can drive the upper limiting plate to move, the upper limiting plate makes contact with limiting of a first clamping block, and therefore the device is convenient to use. And therefore, the separation pipe can perform separation operation, and the separation effect of the device is guaranteed.

Description

Technical Field

[0001] The utility model relates to the field of aerospace technology, in particular to a magnetic attraction control satellite unlocking and separation device. Background Art

[0002] Spacecraft separation and release is a key link in the success of a space mission. The key mechanism for achieving satellite release and separation after entering orbit is related to the success or failure of the satellite launch mission. Common separation and release drive methods include: pyrotechnics explosion drive, memory alloy drive, electric thermal fuse drive, polymer drive, motor drive, etc.

[0003] After searching the prior art, it was found that "a satellite-rocket separation device unlocked by low-impact explosive bolts" has a publication number of "CN114476144B". This device improves the impact environment during the explosion of pyrotechnics to avoid affecting the spacecraft after separation. However, the explosive bolts may cause residual fragments to be embedded in surrounding parts, thereby affecting the separation effect of the device.

[0004] Therefore, a magnetically controlled satellite unlocking and separation device is proposed to solve the above problems. Utility Model Content

[0005] The purpose of the utility model is to provide a magnetically controlled satellite unlocking and separation device in order to solve the above-mentioned problem, thereby improving the problem that the explosive bolts may cause residual fragments to be embedded in the surrounding parts, thereby affecting the separation effect of the device.

[0006] The utility model achieves the above-mentioned purpose through the following technical solutions, a magnetically controlled satellite unlocking and separation device, comprising: a mounting frame, a plurality of bases are arranged on the upper end of the mounting frame, and the plurality of bases are distributed in an array along the upper end of the mounting frame; a separation mechanism, the separation mechanism is arranged on the upper end of the base; wherein, the separation mechanism comprises an outer frame fixedly connected to the upper end of the base, a positioning assembly is arranged inside the outer frame, the surface of the positioning assembly passes through the outside of the outer frame, and limited separation assemblies are arranged on both sides of the outer frame, the limited separation assemblies are located inside the outer frame, and the upper end of the limited separation assembly passes through the top of the outer frame.

[0007] Preferably, the positioning assembly includes a mounting platform fixedly connected to the inner bottom wall of the outer frame and two mounting tubes fixedly connected to the side surfaces of the outer frame. An electromagnet is embedded and installed inside the mounting platform. Limit clamping tubes are provided on both sides of the electromagnet. The limit clamping tubes are slidably connected to the inner walls of the mounting tubes. The electromagnet is controlled so that it can generate magnetic force when power is supplied.

[0008] Preferably, the limiting separation assembly includes an outer tube fixedly connected to the inner bottom wall of the outer frame, the inner wall of the outer tube is slidably connected with a separation tube, the upper end of the separation tube passes through the top of the outer frame, the surface of the separation tube is fixedly connected with a first clamping block, the first clamping block is slidably connected to the inner wall of the outer frame, and the upper end arc surface of the first clamping block assists the separation operation.

[0009] Preferably, a middle cross column is fixedly connected to the inner wall of the mounting tube, a first spring is sleeved on the surface of the middle cross column, the other end of the first spring is fixedly connected to the inner wall of the position limiting clamping tube, and the middle cross column cooperates with the position limiting clamping tube to achieve a positioning effect.

[0010] Preferably, the end of the limit clamp tube away from the electromagnet is fixedly connected with an upper limit plate, and the upper end of the upper limit plate is provided with two rectangular grooves, and the two upper limit plates can assist in the separation of the electromagnet.

[0011] Preferably, the interior of the outer tube is provided with a middle sliding rod fixedly connected to the inner bottom wall of the outer frame, the surface of the middle sliding rod is sleeved with a second spring, the second spring is fixedly connected to the lower end of the separation tube, and the second spring is used to assist the electromagnet in the separation operation.

[0012] Preferably, a slide groove is provided on one side of the outer tube, a second clamping block is fixedly connected to one side of the separation tube, the second clamping block passes through the slide groove, and the second clamping block and the limiting clamping tube form a secondary limiting function.

[0013] The beneficial effects of the utility model are:

[0014] 1. The above-mentioned magnetically controlled satellite unlocking and separation device can form a double limit effect under the action of the separation mechanism. When the limit clamp tube is reset, the device will drive the upper limit plate to move with it. At this time, the limit clamp tube will release the limit on the second clamp block. At the same time, the limit clamp tube will drive the upper limit plate to move, so that the upper limit plate contacts the limit on the first clamp block, so that the separation tube can be separated, thereby ensuring the separation effect of the device;

[0015] 2. By setting up a separation tube, it can cooperate with the positioning component to form a secondary limiting effect under the action of the separation tube. The first clamping block fixedly connected to the surface of the separation tube on one side will cooperate with the upper limiting plate. At the same time, the arc surface of the upper limiting plate cooperates with the arc surface of the first clamping block, which will ensure the stability of separation and reduce the situation of poor separation. BRIEF DESCRIPTION OF THE DRAWINGS

[0016] Figure 1 It is a structural schematic diagram of the utility model;

[0017] Figure 2 This is a schematic diagram of the separation mechanism structure of the utility model;

[0018] Figure 3 This is an internal cross-sectional view of the separation mechanism of the utility model;

[0019] Figure 4 This is a schematic diagram of the explosion structure of the limit separation component of the utility model;

[0020] Figure 5 It is a schematic diagram of the structure of the positioning component of the utility model.

[0021] In the figure: 1. mounting frame; 2. base; 3. separation mechanism; 31. outer frame; 32. positioning assembly; 321. mounting table; 322. electromagnet; 323. limit clamping tube; 324. mounting tube; 325. middle cross column; 326. first spring; 327. upper limit plate; 33. limit separation assembly; 331. outer tube; 332. separation tube; 333. first clamping block; 334. middle sliding rod; 335. second spring; 336. slide groove; 337. second clamping block. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0023] When implementing: Figure 1-5 As shown, a magnetically controlled satellite unlocking and separation device comprises: a mounting frame 1, a plurality of bases 2 are arranged at the upper end of the mounting frame 1, and the plurality of bases 2 are distributed in an array along the upper end of the mounting frame 1; a separation mechanism 3, the separation mechanism 3 is arranged at the upper end of the base 2; wherein the separation mechanism 3 comprises an outer frame 31 fixedly connected to the upper end of the base 2, a positioning assembly 32 is arranged inside the outer frame 31, the surface of the positioning assembly 32 penetrates to the outside of the outer frame 31, and limited separation assemblies 33 are arranged on both sides of the outer frame 31, the limited separation assembly 33 is located inside the outer frame 31, and the upper end of the limited separation assembly 33 penetrates to the top of the outer frame 31;

[0024] like Figure 2 , Figure 3 and Figure 5As shown, the positioning assembly 32 includes a mounting platform 321 fixedly connected to the inner bottom wall of the outer frame 31 and two mounting tubes 324 fixedly connected to the side surfaces of the outer frame 31. An electromagnet 322 is embedded and installed inside the mounting platform 321. Limit clamping tubes 323 are arranged on both sides of the electromagnet 322. The limit clamping tubes 323 are slidably connected to the inner walls of the mounting tubes 324. A middle cross column 325 is fixedly connected to the inner wall of the mounting tube 324. A first spring 326 is sleeved on the surface of the middle cross column 325. The other end of the first spring 326 is fixedly connected to the inner wall of the limit clamping tube 323. The end of the limit clamping tube 323 away from the electromagnet 322 is fixedly connected to an upper limit plate 327. Two rectangular grooves are provided at the upper end of the upper limit plate 327. The device controls the electromagnet 322 so that the electromagnet 322 generates magnetic force when it is powered on, thereby generating magnetic attraction on the end of the limit clamping tube 323, so that the limit clamping tube 323 is firmly adsorbed on the end surface of the electromagnet 322. When the electromagnet 322 is no longer powered on, the magnetic attraction effect on the limit clamping tube 323 is released. At this time, the limit clamping tube 323 moves toward the direction of the middle cross column 325 under the action of the first spring 326. At this time, when the limit clamping tube 323 moves, the upper limit plate 327 is driven to move with it.

[0025] like Figure 1 , Figure 2 and Figure 4 As shown, the limiting separation component 33 includes an outer tube 331 fixedly connected to the inner bottom wall of the outer frame 31, the inner wall of the outer tube 331 is slidably connected with a separation tube 332, the upper end of the separation tube 332 passes through the top of the outer frame 31, the surface of the separation tube 332 is fixedly connected with a first clamping block 333, the first clamping block 333 is slidably connected to the inner wall of the outer frame 31, the interior of the outer tube 331 is provided with a middle sliding rod 334 fixedly connected to the inner bottom wall of the outer frame 31, the surface of the middle sliding rod 334 is sleeved with a second spring 335, the second spring 335 is fixedly connected to the lower end of the separation tube 332, a sliding groove 336 is opened on one side of the outer tube 331, and a second clamping block 337 is fixedly connected to one side of the separation tube 332, and the second clamping block 337 passes through the sliding groove 336. When the limit clamp tube 323 remains adsorbed, the position of the separation tube 332 is limited by the limit clamp tube 323 and the cooperation with the second clamp block 337, and the upper limit plate 327 synchronously limits the first clamp block 333, thereby achieving a double limit effect. When the limit clamp tube 323 moves, the limit clamp tube 323 releases the restriction on the second clamp block 337, and the upper limit plate 327 also releases the restriction on the first clamp block 333, thereby allowing the separation tube 332 to be separated.

[0026] When the utility model is in use, the device controls the electromagnet 322. The electromagnet 322 generates magnetic force when it is energized, thereby generating magnetic attraction on the end of the limit clamping tube 323. The limit clamping tube 323 is firmly adsorbed on the end surface of the electromagnet 322. When the limit clamping tube 323 remains adsorbed, the position of the separation tube 332 is limited under the action of the limit clamping tube 323 and the cooperation of the second clamping block 337. At the same time, the upper limit plate 327 synchronously limits the first clamping block 333. When the electromagnet 322 is no longer energized, the magnetic attraction effect on the limit clamping tube 323 is released. At this time, the limit clamping tube 323 moves toward the direction of the middle cross column 325 under the action of the first spring 326. At this time, when the limit clamping tube 323 moves, the upper limit plate 327 is driven to move with it. At this time, the limit clamping tube 323 releases the restriction on the second clamping block 337, and the upper limit plate 327 also releases the restriction on the first clamping block 333, thereby separating the separation tube 332.

[0027] In addition, it should be understood that although the present specification is described according to implementation modes, not every implementation mode contains only one independent technical solution. This description of the specification is only for the sake of clarity. Those skilled in the art should regard the specification as a whole. The technical solutions in each embodiment may also be appropriately combined to form other implementation modes that can be understood by those skilled in the art.

Claims

1. A magnetically controlled satellite unlocking and separation device, characterized in that: include: A mounting frame (1), wherein a plurality of bases (2) are arranged at the upper end of the mounting frame (1), and the plurality of bases (2) are distributed in an array along the upper end of the mounting frame (1); A separation mechanism (3), wherein the separation mechanism (3) is arranged at the upper end of the base (2); The separation mechanism (3) comprises an outer frame (31) fixedly connected to the upper end of the base (2); a positioning assembly (32) is arranged inside the outer frame (31); the surface of the positioning assembly (32) extends to the outside of the outer frame (31); and limited separation assemblies (33) are arranged on both sides of the outer frame (31); the limited separation assembly (33) is located inside the outer frame (31); and the upper end of the limited separation assembly (33) extends to the top of the outer frame (31).

2. The magnetically controlled satellite unlocking and separation device according to claim 1, characterized in that: The positioning assembly (32) comprises a mounting platform (321) fixedly connected to the inner bottom wall of the outer frame (31) and two mounting tubes (324) fixedly connected to the side surfaces of the outer frame (31); an electromagnet (322) is embedded and installed inside the mounting platform (321); both sides of the electromagnet (322) are provided with limit clamping tubes (323); the limit clamping tubes (323) are slidably connected to the inner walls of the mounting tubes (324).

3. The magnetically controlled satellite unlocking and separation device according to claim 1, characterized in that: The position limiting separation component (33) comprises an outer tube (331) fixedly connected to the inner bottom wall of the outer frame (31); a separation tube (332) is slidably connected to the inner wall of the outer tube (331); the upper end of the separation tube (332) passes through the upper part of the outer frame (31); a first clamping block (333) is fixedly connected to the surface of the separation tube (332); and the first clamping block (333) is slidably connected to the inner wall of the outer frame (31).

4. The magnetically controlled satellite unlocking and separation device according to claim 2, characterized in that: The inner wall of the mounting tube (324) is fixedly connected with a middle cross column (325), the surface of the middle cross column (325) is sleeved with a first spring (326), and the other end of the first spring (326) is fixedly connected to the inner wall of the limit clamping tube (323).

5. The magnetically controlled satellite unlocking and separation device according to claim 4 is characterized in that: An upper limit plate (327) is fixedly connected to the end of the limit clamping tube (323) away from the electromagnet (322), and two rectangular grooves are formed at the upper end of the upper limit plate (327).

6. The magnetically controlled satellite unlocking and separation device according to claim 3 is characterized in that: The outer tube (331) is provided with a middle sliding rod (334) fixedly connected to the inner bottom wall of the outer frame (31), and the surface of the middle sliding rod (334) is sleeved with a second spring (335), and the second spring (335) is fixedly connected to the lower end of the separation tube (332).

7. The magnetically controlled satellite unlocking and separation device according to claim 6 is characterized in that: A slide groove (336) is provided on one side of the outer tube (331), and a second clamping block (337) is fixedly connected to one side of the separation tube (332), and the second clamping block (337) passes through the slide groove (336).

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