Fast-response low-impact large-bearing seeker displacement device

Through the combination of high-pressure energy storage and hoisting cylinder, combined with rolling guide rail sub- and buffering measures, the response speed and impact problems of the seeker positioning device in aerospace environment is solved, and a fast and safe seeker launch and Feedback signal improves testability and reliability.

CN119289775APending Publication Date: 2025-01-10GUIZHOU AEROSPACE TIANMA ELECTRICAL TECH
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Patent Information

Application Number
CN202411544495.4
Authority / Receiving Office
CN · China
Patent Type
Applications(China)
Current Assignee / Owner
Filing Date
2024-10-31
Publication Date
2025-01-10

AI Technical Summary

Technical Problem

The existing seeker positioning device does not respond enough in complex aerospace environments, has a large impact, insufficient testability and reliability, and has a complex structure, making it difficult to meet the problems of fast unlocking, rapid launch, high loads and fast feedback signals. .

Method used

Using high-voltage energy storage as energy, the initial locking mechanism and the hoisting cylinder can be used to quickly unlock and roll out the seeker mechanism. Combined with the rolling guide rail sub and buffering measures, the impact is reduced, and the circuit signal feedback is realized through the in-place feedback mechanism, using high The combination of strength aluminum alloy materials and electronic controls achieves smooth unlocking and rolling process.

Benefits of technology

The seeker mechanism is quickly and safely pushed out in complex environments, reducing forward and reverse impacts, ensuring the safety of the seeker, improving testability and airtightness, able to carry 20,000N external forces, and at 0.3S Complete the rollout process within 1S.

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Abstract

The invention provides a fast-response low-impact large-bearing seeker displacement device. The fast-response low-impact large-bearing seeker displacement device comprises a high-pressure energy storage device. The high-pressure energy storage device is fixed to one side of the body frame and sequentially connected with the initial locking mechanism and the jacking air cylinder, the initial locking mechanism is arranged between the high-pressure energy storage device and the jacking air cylinder, the jacking air cylinder is hinged to the guide head mechanism, and the guide head mechanism is installed and fixed to the other side of the body frame through a large-bearing-capacity rolling guide rail pair. The motion starting point position of the guide head mechanism is fixed by the initial locking mechanism, and a push rod of the jacking air cylinder is connected with the guide head mechanism. When the high-pressure energy accumulator releases energy, the initial locking mechanism is quickly unlocked, so that the jacking air cylinder jacks the seeker mechanism to be pushed out to a set position, sequential control over all-directional locking, unlocking, pushing-out and in-place locking of the seeker mechanism can be achieved, the pushing-out process is high in logicality, and good protectiveness is achieved; and the functions of quick in-place, low impact and large load bearing of the seeker mechanism in an air and space complex environment can be realized.
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Description

Technical Field

[0001] The invention relates to a fast-response, low-impact, large-load seeker displacement device, which is particularly suitable for aircraft terminal precision guidance. Background Art

[0002] With the rapid development of science and technology in my country, the requirements for the use environment and functional performance of the seeker displacement device are becoming higher and higher under the new situation, especially for the seeker displacement device used in the aerospace environment. The seeker displacement device needs to be miniaturized, lightweight, high-strength, and have good air tightness, testability, stability, reliability, etc. Therefore, there is an objective demand: under the premise of the positioning and locking of the seeker mechanism in the aerospace environment, it has the characteristics of fast unlocking, rapid launch, small impact, large load, rapid feedback signal to the collector after it is in place, and good testability in a limited space. Although there are seeker displacement devices that are gradually used in different aircraft, most of them have single functions, complex structures, insufficient reaction speed, large impact, and low testability and reliability. For example, a barrel-launched rotary cruise missile and its working method disclosed in CN116499307A pushes out the propulsion device through a spring and unlocks the mechanical arm through a motor. The unlocking and pushing out of the seeker use two different sets of drive systems respectively, which makes the unlocking and pushing out structure of the seeker complicated, and the use of a spring to push out the seeker requires the reliability of the spring. Summary of the invention

[0003] In order to solve the above technical problems, the present invention provides a fast-response, low-impact, large-load-bearing guide head displacement device, which can meet the requirements of fast unlocking of the guide head mechanism, rapid pushing out, small impact in place, large load bearing, rapid feedback signal, and good testability in a limited space.

[0004] The present invention is achieved through the following technical solutions.

[0005] The present invention provides a fast-response, low-impact, large-load seeker displacement device, comprising a high-pressure accumulator; the high-pressure accumulator is fixed on a main body frame, the high-pressure accumulator serves as the energy source of the seeker displacement device, the high-pressure accumulator pipeline is connected to an initial locking mechanism and a lifting cylinder, the initial locking mechanism is between the high-pressure accumulator and the lifting cylinder, the lifting cylinder is hinged to the seeker mechanism, the seeker mechanism adopts a large-load rolling guide pair as a guide support, the starting position of the seeker mechanism is fixed by the initial locking mechanism, when the high-pressure accumulator releases energy, the initial locking mechanism is quickly unlocked so that the lifting cylinder lifts the seeker mechanism to a set position, at this time, the buffer pad on the main body frame and the buffer ring in the lifting cylinder absorb the large impulse generated by the seeker mechanism, and when in place, an in-place feedback mechanism locks the seeker mechanism and forms a circuit path feedback signal.

[0006] The high-pressure energy storage device can exhaust gas at a constant pressure of a certain ratio within a certain period of time, so that the unlocking and lifting processes are smooth and even.

[0007] The initial locking mechanism is connected to the high-pressure accumulator through the first gas pipeline. After the high-pressure accumulator releases the gas source, the initial locking mechanism is completely unlocked and the gas source enters the lifting cylinder to ensure the safety of the guide head mechanism pushing process.

[0008] The initial locking mechanism is designed with an air source detection interface, which can detect the pressure in the lifting cylinder.

[0009] The lifting cylinder is connected to the initial locking mechanism through the second air pipeline, and a vibration-damping ring is arranged on the internal lever of the lifting cylinder, which can buffer the guide head mechanism and reduce the impact.

[0010] The lifting cylinder is hinged to the guide head mechanism through a lever screw, a vibration-damping pad, and a pin shaft. The vibration-damping pad can provide reverse buffering for the guide head mechanism to reduce reverse impact.

[0011] The rolling guide pair is symmetrically distributed with the lifting cylinder as the center and can bear 20000N in one direction.

[0012] The tops of the left and right sides of the main body frame are provided with limiting steps, and the buffer pads are bonded and fixed to the limiting steps to buffer the guide head mechanism and reduce impact.

[0013] The in-position feedback mechanism can lock the seeker mechanism after it is in position, and form a circuit path to feed back the locking signal to the collector.

[0014] The initial locking mechanism, the lifting cylinder, the body frame, and the in-position feedback mechanism are all made of high-strength aluminum alloy.

[0015] The seeker mechanism can be in place in about 0.1S under no-load conditions and in 0.3S under complex load conditions. ~ 1S in place.

[0016] The beneficial effects of the present invention are: it can realize the release of gas source at a constant pressure of a certain ratio within a certain period of time, so that the unlocking and lifting process is smoother and smoother; it can realize the release of gas source, complete unlocking, rapid lifting, buffering in place, locking in place, and the ejection process of feedback signal through the electric control combination, with strong logic and good protection; it has the limit buffering measures of the lifting cylinder and the main body frame to reduce the forward impact, and has the reverse vibration reduction measures to reduce the reverse impact, and can ensure the safety of the guide head during the ejection process in real time; it can realize the in-cylinder air pressure detection in a complex space, with high air tightness and good testability; it can realize reliable ejection under the external force of 20000N in a complex environment, and the ejection time is 0.3S. ~1S is adjustable; the seeker transformation device is mainly made of high-strength aluminum alloy material, with compact structure layout, high integration, miniaturization and light weight. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 It is a schematic diagram of the structure of the present invention;

[0018] Figure 2 yes Figure 1 Rear view of

[0019] Figure 3 yes Figure 1 Left view of;

[0020] Figure 4 It is a schematic diagram of the structure of the seeker mechanism in the push-out state of the present invention;

[0021] Figure 5 yes Figure 4 Schematic diagram of the structure without a seeker;

[0022] Figure 6 It is a schematic diagram of the main body frame structure of the present invention;

[0023] Figure 7 This is a schematic diagram of the initial locking mechanism structure of the present invention.

[0024] Figure 8 This is a schematic diagram of the lifting cylinder structure of the present invention.

[0025] Fig. 9 It is a schematic diagram of the structure of the in-place feedback mechanism of the present invention.

[0026] In the figure: 1-high-pressure accumulator, 2-initial locking mechanism, 3-lifting cylinder, 4-body frame, 5-rolling guide pair, 6-guide head mechanism, 7-in-place feedback mechanism, 8-first gas pipeline, 9-second gas pipeline, 10-high-pressure accumulator terminal, 11-in-place feedback mechanism terminal, 12-pin shaft, 13-vibration damping pad, 14-lever screw, 15-buffer pad. DETAILED DESCRIPTION

[0027] The technical solution of the present invention is further described below, but the scope of protection claimed is not limited to the description.

[0028] like Figures 1 to 9A fast-response, low-impact, large-load seeker displacement device shown in the figure comprises a high-pressure accumulator 1; the high-pressure accumulator 1 is fixed on a main body frame 4, the high-pressure accumulator 1 serves as the energy source of the seeker displacement device, the high-pressure accumulator 1 pipeline is connected with an initial locking mechanism 2 and a lifting cylinder 3, the initial locking mechanism 2 is between the high-pressure accumulator 1 and the lifting cylinder 3, the lifting cylinder 3 is hinged with the seeker mechanism 6, the seeker mechanism 6 adopts a large-load rolling guide pair 5 as a guide support, the starting position of the seeker mechanism 6 is fixed by the initial locking mechanism 2, when the high-pressure accumulator 1 releases energy, the initial locking mechanism 2 is quickly unlocked so that the lifting cylinder 3 lifts the seeker mechanism 6 to a set position, at this time, the buffer pad 15 on the main body frame 4 and the buffer ring in the lifting cylinder absorb the large impulse generated by the seeker mechanism 6, and when in place, an in-place feedback mechanism 7 locks the seeker mechanism 6 and forms a circuit path feedback signal.

[0029] The high-pressure accumulator 1 can exhaust gas at a constant pressure of a certain ratio within a certain period of time, so that the unlocking and lifting process is smooth and smooth.

[0030] The initial locking mechanism 2 is connected to the high-pressure accumulator 1 through the first gas pipeline 8. After the high-pressure accumulator 1 releases the gas source, the initial locking mechanism 2 is completely unlocked and the gas source enters the lifting cylinder 3 to ensure the safety of the guide head mechanism 6 during the pushing process.

[0031] The initial locking mechanism 2 is designed with an air source detection interface, which can detect the pressure in the lifting cylinder 3.

[0032] The lifting cylinder 3 is connected to the initial locking mechanism 2 through the second air pipeline 9. A vibration-damping ring is provided on the internal lever of the lifting cylinder 3, which can buffer the guide head mechanism 6 and reduce the impact.

[0033] The lifting cylinder 3 is hinged to the guide head mechanism 6 through a lever screw 14, a vibration-damping pad 13, and a pin shaft 12. The vibration-damping pad 13 can provide reverse buffering to the guide head mechanism 6 to reduce reverse impact.

[0034] The rolling guide pair 5 is symmetrically distributed with the lifting cylinder 3 as the center, and can bear 20000N in one direction.

[0035] The tops of the left and right sides of the main body frame 4 are provided with limiting steps, and the buffer pads 15 are bonded and fixed to the limiting steps to buffer the guide head mechanism 6 and reduce impact.

[0036] The in-position feedback mechanism 7 can lock the seeker mechanism 6 after it is in position, and form a circuit path to feed back the locking signal to the collector.

[0037] The initial locking mechanism 2, the lifting cylinder 3, the main body frame 4, and the in-position feedback mechanism 7 are all made of high-strength aluminum alloy.

[0038] The seeker mechanism 6 can be in place in about 0.1S under no-load conditions and in 0.3S under complex load conditions. ~ 1S in place.

[0039] The following steps are generally taken during operation:

[0040] 1) First, the high-voltage energy storage device terminal 10 and the in-position feedback mechanism terminal 11 are connected to the electric control assembly through cables;

[0041] 2) Turn on the electric control combination switch, the high-pressure accumulator 1 instantly generates a constant pressure of a certain ratio and exhausts to the initial locking mechanism 2 through the first gas pipeline 8. After the initial locking mechanism 2 is completely unlocked, the high-pressure gas enters the lifting cylinder 3 through the second gas pipeline 9 and pushes the lever to quickly push out the guide head mechanism 6;

[0042] 3) When the guide head mechanism 6 reaches the end, the vibration reduction ring in the lifting cylinder 3 and the buffer pad 13 on the main body frame 4 buffer the guide head mechanism;

[0043] 4) When the seeker mechanism 6 is in position, the locking pin of the in-position feedback mechanism 7 is quickly locked, and the in-position signal is fed back to the electric control assembly through the in-position feedback mechanism terminal 11. At this time, the vibration damping pad 13 on the lever screw 14 reversely buffers the seeker mechanism 6 until the seeker mechanism 6 stops completely. At this time, the seeker mechanism is turned off.

Claims

1. A fast-response, low-impact, large-load seeker displacement device, characterized in that: The invention comprises a high-pressure energy accumulator (1); the high-pressure energy accumulator (1) is fixed on one side of a main body frame (4); the high-pressure energy accumulator (1) is connected to an initial locking mechanism (2) and a lifting cylinder (3) in sequence; the initial locking mechanism (2) is between the high-pressure energy accumulator (1) and the lifting cylinder (3); the lifting cylinder (3) is hinged to a guide head mechanism (6); the guide head mechanism (6) is installed on the other side fixed to the main body frame (4) by using a large-load rolling guide pair (5); the starting position of the guide head mechanism (6) is fixed by the initial locking mechanism (2); and the push rod of the lifting cylinder (3) is connected to the guide head mechanism (6).

2. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: A buffer pad (15) and a feedback mechanism (7) are also installed on the main body frame (4); the buffer pad (15) is installed on the inner wall of the main body frame (4) at the travel limit position of the guide head mechanism (6); and the feedback mechanism (7) is installed on the outer wall of the main body frame (4).

3. The fast-response, low-impact, high-load seeker displacement device according to claim 4, characterized in that: The in-position feedback mechanism (7) can lock the seeker mechanism (6) after it is in position, and form a circuit path to feed back the locking signal to the collector.

4. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: The initial locking mechanism (2) is connected to the high-pressure energy storage device (1) via a first gas pipeline (8), and the lifting cylinder (3) is connected to the initial locking mechanism (2) via a second gas pipeline (9).

5. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: A vibration-damping ring is arranged on the internal lever of the lifting cylinder (3).

6. The fast-response, low-impact, large-load seeker displacement device according to claim 4, characterized in that: The lifting cylinder (3) is hinged to the guide head mechanism (6) via a lever screw (14), a vibration-damping pad (13) and a pin shaft (12).

7. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: The rolling guide rail pair (5) is symmetrically distributed with the lifting cylinder (3) as the center, and can bear 20,000N in one direction.

8. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: The main body frame (4) has limiting steps at the tops of the left and right sides, and the buffer pads (15) are bonded and fixed to the limiting steps.

9. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: The initial locking mechanism (2), the lifting cylinder (3), the main body frame (4) and the in-position feedback mechanism (7) are all made of high-strength aluminum alloy.

10. The fast-response, low-impact, large-load seeker displacement device according to claim 1, characterized in that: The seeker mechanism (6) can be in place in about 0.1S under no-load conditions and in 0.3S under complex load conditions. ~ 1S in place.

Citation Information

Patent Citations

  • Cylinder-type launched rotor-wing patrolling bomb and working method thereof

    CN116499307A