A warhead electrical performance detection probe adjusting and fixing device
By designing an adjustment and fixing device for the warhead electrical performance detection probe, the problem of detection data fluctuation caused by unstable test pen pressure during manual detection was solved, and stable fixation and accurate detection of the probe were achieved.
Patent Information
- Application Number
- CN202411721729.8
- Authority / Receiving Office
- CN · China
- Patent Type
- Patents(China)
- Current Assignee / Owner
- Filing Date
- 2024-11-28
- Publication Date
- 2025-10-10
- Estimated Expiration
- 2044-11-28
AI Technical Summary
During the warhead electrical performance test, the pressure of the test lead tip during manual testing causes the test instrument readings to be unstable, affecting the accuracy of the test data.
A warhead electrical performance detection probe adjustment and fixing device was designed, including the electrical performance detection tooling for the head, shoulder and main charge shell. The fixture, probe unit and position adjustment assembly were used to achieve stable fixation and adjustment of the probe through butterfly screws, hinge pins and compression release assemblies.
Ensure that the detection probe can be stably connected to the detection point to avoid data fluctuations caused by human control and improve the stability and consistency of detection.
Smart Images

Figure CN119667232B_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of warhead electrical performance detection, in particular to a warhead electrical performance detection probe adjustment and fixing device. Background Art
[0002] Electrical performance testing, a process inspection for electronic products in industrial automation testing, ensures product quality and yield, avoiding returns and scrap due to substandard electrical performance. Spring test probes, commonly used in electrical performance testing, come in a wide variety of models, offering varying needle shapes, thicknesses, lengths, and clamping forces. Engineers select the appropriate probe tip model for electrical performance testing based on the specific testing environment and process requirements.
[0003] The electrical performance test of the warhead belongs to the electrical performance test of energetic materials. The testing station is dangerous and requires a design for human-machine isolation operation.
[0004] The current solution for testing the electrical performance of the warhead is manual testing, and the manual testing station is located in an independent explosion-proof room. Usually, the tester transports two warheads to the electrical performance testing room via a transfer cart, places one warhead on the testing table, and uses a V-shaped block to support it horizontally, with the head facing the explosion venting surface of the explosion-proof room. The tester connects two test leads to the test meter, short-circuits the tips of the two test leads, and zeroes the test meter. Afterwards, the tester performs electrical performance tests on each test point of the warhead in accordance with the test process sequence. Specifically, the tester adjusts the test meter to the corresponding gear, places the tip of the test lead against the test point, applies a little force with the hand, keeps it stable, and reads the meter.
[0005] However, during the current manual testing of warhead electrical performance, the test leads are placed against the test point, requiring the tester to maintain a steady force to ensure a reliable connection between the test leads and the test point. This pressure from the test lead tip can cause the test instrument reading to fluctuate, resulting in unstable test values. Summary of the Invention
[0006] In view of the above problems, the present invention provides a warhead electrical performance detection probe adjustment and fixing device for overcoming the above problems or at least partially solving the above problems.
[0007] The present invention provides the following solutions:
[0008] A warhead electrical performance detection probe adjustment and fixing device, comprising:
[0009] A head electrical performance testing tool, comprising a connected fixture and a first probe unit; the fixture comprises an open circular sleeve structure with a first butterfly screw at the opening to achieve clamping and loosening with the warhead head; the first probe unit comprises a plurality of head detection probes and a head probe position adjustment assembly, the head probe position adjustment assembly being used to adjust the plurality of head detection probes to abut against a plurality of electrical performance testing points on the warhead head in a one-to-one manner after the fixture is clamped to the warhead head;
[0010] A shoulder electrical performance testing tool, the shoulder electrical performance testing tool comprising a first base, a first upper buckle block, a first clamping and releasing assembly and a second probe unit; one end of the first upper buckle block is hinged to the first base through a first hinge pin, so that the first upper buckle block can be rotated around the first hinge pin to open so that the shoulder of the warhead can enter between the first upper buckle block and the first base; the first clamping and releasing assembly is used to realize the clamping and releasing of the first base and the first upper buckle block; the second probe unit is connected to the first upper buckle block, the second probe unit comprises a number of shoulder detection probes and a shoulder probe position adjustment assembly, the shoulder probe position adjustment assembly is used to adjust a number of the shoulder detection probes to correspond one by one to abut against a number of shoulder electrical performance testing points of the warhead after the first base and the first upper buckle block are clamped to the shoulder of the warhead;
[0011] A tool for testing the electrical performance of a main charge shell, the tool comprising a second base, a second upper buckle block, a second clamping and releasing assembly and a third probe unit; one end of the second upper buckle block is hinged to the second base through a second hinge pin, so that the second upper buckle block can be rotated open around the second hinge pin to allow the main charge shell of the warhead to enter between the second upper buckle block and the second base; the second clamping and releasing assembly is used to realize the clamping and releasing of the second base and the second upper buckle block; the third probe unit is connected to the second upper buckle block, and the third probe unit comprises a number of main charge shell detection probes and a main charge shell probe position adjustment assembly, the main charge shell probe position adjustment assembly is used to adjust a number of the main charge shell detection probes to correspond one by one to abut against a number of main charge shell electrical performance detection points of the warhead after the second base and the second upper buckle block are clamped with the main charge shell of the warhead.
[0012] Preferably: the head probe position adjustment assembly includes a first main guide rod, a first auxiliary guide rod, a first probe mounting seat and a first height adjustment rotary rod;
[0013] The plurality of head detection probes are fixedly connected to the first probe mounting seat; one end of each of the first main guide rod and the first auxiliary guide rod is connected to the clamp, and the first main guide rod and the first auxiliary guide rod are connected to the first probe mounting seat so as to be relatively slidable; the first main guide rod and the first auxiliary guide rod are each provided with a first compression spring at a position between the clamp and the first probe mounting seat;
[0014] One end of the first main guide rod extends away from the clamp to the outside of the first probe mounting seat and is connected to a first height adjustment rod through a first screw sleeve. The position of the first probe mounting seat relative to the clamp is adjusted by the first height adjustment rod to allow the front end of the head detection probe to enter and exit the clamp.
[0015] Preferably: the first auxiliary guide rod is connected to the first probe mounting seat through an oil-free bushing; a second screw sleeve is provided at the opening of the clamp, and the first butterfly screw is fitted and connected to the second screw sleeve; the material of the first probe mounting seat is epoxy glass cloth paper-based board material, and the material of the first height adjustment rod is polyformaldehyde material.
[0016] Preferably: the first compression and release assembly includes a first compression screw and a first butterfly nut, the other end of the first upper buckle block is provided with a first notch, the first compression screw is hinged to the first base through a first pin, and the first compression screw can enter and exit the first notch, so that after entering the first notch, the first base and the first upper buckle block are compressed by the first butterfly nut on the first compression screw.
[0017] Preferably: after the first base and the first upper buckle block are pressed together, an octagonal structure is formed inside, and the two lower oblique sides of the first base and the two upper oblique sides of the first upper buckle block are designed with step structures of the same height to fit the shoulder structure of the warhead.
[0018] Preferably: each of the two lower oblique sides of the first base has a through slot, a limit block that can slide up and down is provided in the through slot, and a second butterfly screw is connected to the outer side of the limit block, and the second butterfly screw is used to fix the position of the limit block in the through slot so that the limit block can be extended or retracted to be compatible with different axial limit distances of different warheads.
[0019] Preferably: the shoulder probe position adjustment assembly includes a second probe mounting seat, an upper guide pressure plate, a lower guide pressure plate, a ball seat, a second main guide rod and a second auxiliary guide rod;
[0020] The second probe mounting seat is connected to the first upper buckle block, one end of each of the second main guide rod and the second secondary guide rod is fixedly connected to the second probe mounting seat, and the second main guide rod and the second secondary guide rod are both connected to the upper guide pressure plate so as to be slidable relative to each other; the second main guide rod and the second secondary guide rod are each provided with a second compression spring at a position between the second probe mounting seat and the upper guide pressure plate;
[0021] One end of the second main guide rod away from the second probe mounting seat extends to the outside of the upper guide pressure plate and is connected to a second height adjustment rod through a second screw sleeve, and the position of the upper guide pressure plate relative to the second probe mounting seat is adjusted by the second height adjustment rod;
[0022] The lower portion of the upper guide plate and the upper portion of the lower guide plate are both provided with waist-shaped holes with inclined surface features; the ball seat is spherical in shape with a through hole, the axis of the through hole passing through the center of the sphere; the shoulder detection probe is installed in the through hole of the ball seat, and the shoulder detection probe passes through the waist-shaped holes of the upper guide plate and the lower guide plate respectively. The ball seat is formed by the rhombus formed by the upper and lower pairs of waist-shaped holes with inclined surface features to form a ball pair;
[0023] The probe shoulder detection can rotate around the center of the ball seat, and the ball seat can slide horizontally in the diamond space composed of inclined surface features; the butterfly screws on both sides of the upper guide pressure plate pass through the through holes to connect the lower guide pressure plate, and the butterfly screws on both sides are tightened to fix the ball seat with the probe.
[0024] Preferably: the second clamping and releasing assembly includes a second clamping screw and a second butterfly nut, the other end of the second upper buckle block is provided with a second notch, the second clamping screw is hinged to the second base through a second pin, and the second clamping screw can enter and exit the second notch, so that after entering the second notch, the second base and the second upper buckle block are clamped by the second butterfly nut on the second clamping screw.
[0025] Preferably: the main charge shell probe position adjustment assembly includes a third probe mounting seat, two guide rods and two third height adjustment rotary rods;
[0026] There is a notch structure on the upper side of the top edge of the second upper buckle block, and the two guide rods are connected to the notch structure. The third probe mounting seat is nested with an oil-free bushing to form a sliding pair with the two guide rods; the side surface of the third probe mounting seat forms a sliding fit with the side wall of the notch structure on the top edge of the second upper buckle block, limiting the rotational freedom of the third probe mounting seat; the threaded rod ends of the two guide rods are respectively and one-to-one connected with the two third height adjustment rotary rods, and the position of the third probe mounting seat on the guide rod can be adjusted by rotating the third height adjustment rotary rod; each of the two guide rods is provided with a compression spring, and a number of main charge shell detection probes are installed at the end of the third probe mounting seat.
[0027] Preferably, the clamp, the first base, the first upper buckle block, the second base and the second upper buckle block are all made of polyformaldehyde.
[0028] According to the specific embodiments provided by the present invention, the present invention discloses the following technical effects:
[0029] The embodiment of the present application provides a warhead electrical performance detection probe adjustment and fixing device. The tester adjusts and fixes the warhead probe through the device, which can ensure that the test probe can effectively and stably abut against the warhead test point during the electrical performance detection process of the warhead, avoiding the fluctuation of the electrical performance detection data caused by the unstable abutment of the test point due to human control. The shoulder electrical performance detection tooling and the main charge shell electrical performance detection tooling can restrain the axial movement of the warhead through the step features designed on the oblique edges. The shoulder electrical performance detection tooling and the main charge shell electrical performance detection tooling can keep the warhead stable during transportation through the upper buckle block that can be flipped open and buckled, and the butterfly nut lock design that can be quickly pressed, locked and loosened. The detection probe is stably abutted. By adjusting the protrusion and retraction of the shoulder electrical performance detection tooling limit block, the axial limit of warheads of different lengths can be compatible.
[0030] Of course, any product implementing the present invention does not necessarily need to achieve all of the advantages described above at the same time. BRIEF DESCRIPTION OF THE DRAWINGS
[0031] To more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the following briefly introduces the drawings required for use in the embodiments. Obviously, the drawings described below are only some embodiments of the present invention. For those skilled in the art, other drawings can be derived from these drawings without inventive effort.
[0032] Figure 1 This is a structural diagram of a warhead electrical performance detection probe adjustment and fixing device provided by an embodiment of the present invention;
[0033] Figure 2 This is a schematic diagram of the structure of the warhead electrical performance testing tool provided by an embodiment of the present invention;
[0034] Figure 3 1 is a schematic structural diagram of a shoulder electrical performance testing tool provided by an embodiment of the present invention;
[0035] Figure 4 Schematic diagram of the structure of the main charge shell electrical performance testing tool provided by an embodiment of the present invention;
[0036] Figure 5 It is a structural schematic diagram of the warhead electrical performance detection probe adjustment and fixing device provided by an embodiment of the present invention after being connected to the tray.
[0037] In the figure: warhead head electrical performance testing tool 1, fixture 101, head detection probe a102, head detection probe b103, first main guide rod 104, first auxiliary guide rod 105, first probe mounting seat 106, first height adjustment rod 107, first compression spring 108, oil-free bushing 109, second screw sleeve 110, first screw sleeve 111, first butterfly screw 112, shoulder electrical performance testing tool 2, first base 201, limit block 202, first upper buckle block 203, first hinge pin 204, first pin 205, first clamping screw 206, first butterfly screw Mother 207, second probe mounting seat 208, upper guide pressure plate 209, lower guide pressure plate 210, ball seat 211, shoulder detection probe 212, second main guide rod 213, second auxiliary guide rod 214, second height adjustment rotary rod 215, main charge shell electrical performance detection tooling 3, second base 301, second upper buckle block 302, second pin 303, second clamping screw 304, second butterfly nut 305, third probe mounting seat 306, main charge shell detection probe 307, guide rod 308, third height adjustment rotary rod 309, tray 4, electrical inspection box 5, quick connection plate 6. DETAILED DESCRIPTION
[0038] The following will be combined with the accompanying drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field are within the scope of protection of the present invention.
[0039] See also Figure 1 、 Figure 2 、 Figure 3 、 Figure 4 , is a warhead electrical performance detection probe adjustment and fixing device provided by an embodiment of the present invention, such as Figure 1 、 Figure 2 、 Figure 3 、 Figure 4 As shown in FIGS. 1-3, the system can include:
[0040] The head electrical performance detection tool 1 includes a clamp 101 and a first probe unit connected thereto. The clamp 101 has an open circular sleeve structure and a first butterfly screw 112 at the opening thereof to clamp and release the head of the warhead. The first probe unit includes a plurality of head detection probes and a head probe position adjusting assembly for adjusting the plurality of head detection probes to correspondingly abut the plurality of head electrical performance detection points of the warhead after the clamp 101 clamps the head of the warhead.
[0041] The shoulder electrical performance detection tool 2 includes a first base 201, a first upper buckle 203, a first pressing and releasing assembly, and a second probe unit. One end of the first upper buckle 203 is hingedly connected to the first base 201 through a first hinge pin 204, so that the first upper buckle 203 can rotate around the first hinge pin 204 to open to allow the shoulder of the warhead to enter between the first upper buckle 203 and the first base 201. The first pressing and releasing assembly is used to press and release the first base 201 and the first upper buckle 203. The second probe unit is connected to the first upper buckle 203 and includes a plurality of shoulder detection probes 212 and a shoulder probe position adjusting assembly for adjusting the plurality of shoulder detection probes 212 to correspondingly abut the plurality of shoulder electrical performance detection points of the warhead after the first base 201 and the first upper buckle 203 clamp the shoulder of the warhead.
[0042] A tool 3 for testing the electrical performance of a main charge shell, the tool 3 comprising a second base 301, a second upper buckle block 302, a second compression and release assembly, and a third probe unit; one end of the second upper buckle block 302 is hinged to the second base 301 via a second hinge pin, so that the second upper buckle block 302 can be rotated open around the second hinge pin to allow the main charge shell of the warhead to enter between the second upper buckle block 302 and the second base 301; the second compression and release assembly is used to achieve compression and release between the second base 301 and the second upper buckle block 302; the third probe unit is connected to the second upper buckle block 302, and the third probe unit comprises a number of main charge shell detection probes 307 and a main charge shell probe position adjustment assembly, the main charge shell probe position adjustment assembly being used to adjust a number of the main charge shell detection probes 307 to abut against a number of main charge shell electrical performance detection points of the warhead in a one-to-one manner after the second base 301 and the second upper buckle block 302 are clamped with the main charge shell of the warhead.
[0043] The warhead electrical performance test probe adjustment and fixing device provided in the embodiments of the present application solves the problem of ensuring the stability and consistency of the test probes when they are placed against the test points during the warhead electrical performance test. In response to various errors during the warhead production and assembly process that may cause the test points to deviate from the designed positions, a plurality of adjacent probe adjustment and fixing mechanisms are designed to facilitate the accurate and reliable placement of the test probes against the test points.
[0044] In a specific implementation, the embodiment of the present application can provide that the head probe position adjustment assembly includes a first main guide rod 104, a first auxiliary guide rod 105, a first probe mounting seat 106 and a first height adjustment rotary rod 107;
[0045] The plurality of head detection probes are fixedly connected to the first probe mounting seat 106; one end of each of the first main guide rod 104 and the first secondary guide rod 105 is connected to the clamp 101, and the first main guide rod 104 and the first secondary guide rod 105 are slidably connected to the first probe mounting seat 106; the first main guide rod 104 and the first secondary guide rod 105 are each provided with a first compression spring 108 at a position between the clamp 101 and the first probe mounting seat 106;
[0046] The first main guide rod 104 extends from one end of the clamp 101 to the outside of the first probe mounting seat 106 and is connected to the first height adjustment rod 107 through the first screw sleeve 111. The position of the first probe mounting seat 106 relative to the clamp 101 is adjusted by the first height adjustment rod 107 to enable the front end of the head detection probe to enter and exit the clamp 101.
[0047] Further, the first sub-guide rod 105 is connected with the first probe mounting seat 106 through an oil-free bushing 109; the opening of the clamp 101 is provided with a second threaded sleeve 110, and the first winged screw 112 is connected into the second threaded sleeve 110 in a matched mode; the material of the first probe mounting seat 106 is an epoxy glass cloth paper substrate, and the material of the first height-adjusting rotating rod 107 is a polyformaldehyde material.
[0048] The first compression releasing assembly comprises a first compression screw 206 and a first winged nut 207, and the other end of the first upper buckle 203 is provided with a first notch; the first compression screw 206 is hingedly connected with the first base 201 through a first pin 205; the first compression screw 206 can enter or exit the first notch, so that the first base 201 and the first upper buckle 203 are compressed through the first winged nut 207 on the first compression screw 206 after the first compression screw 206 enters the first notch.
[0049] After the first base 201 and the first upper buckle 203 are compressed, an octagonal structure is formed inside; the two lower inclined edges of the first base 201 and the two upper inclined edges of the first upper buckle 203 are all designed with step structures of the same height, which are used for matching the shoulder structure of a warhead.
[0050] Each of the two lower inclined edges of the first base 201 is provided with a through groove, and a limiting block 202 that can slide up and down is arranged in the through groove; the outer side of the limiting block 202 is connected with a second winged screw; the second winged screw is used for fixing the position of the limiting block 202 in the through groove, so that the limiting block 202 can be extended or retracted to be compatible with different warheads with different limiting distances in the axial direction.
[0051] The shoulder probe position adjusting assembly comprises a second probe mounting seat 208, an upper guide pressing plate 209, a lower guide pressing plate 210, a ball seat 211, a second main guide rod 213 and a second sub-guide rod 214;
[0052] The second probe mounting seat 208 is connected with the first upper buckle 203; one end of each of the second main guide rod 213 and the second sub-guide rod 214 is fixedly connected with the second probe mounting seat 208; the second main guide rod 213 and the second sub-guide rod 214 are slidably connected with the upper guide pressing plate 209; a compression spring is sleeved on each of the second main guide rod 213 and the second sub-guide rod 214 at a position between the second probe mounting seat 208 and the upper guide pressing plate 209;
[0053] One end of the second main guide rod 213 away from the second probe mounting seat 208 extends to the outside of the upper guide plate 209 and is connected to a second height adjustment rod 215 through a second screw sleeve 110. The second height adjustment rod 215 is used to adjust the position of the upper guide plate 209 relative to the second probe mounting seat 208;
[0054] The lower portion of the upper guide plate 209 and the upper portion of the lower guide plate 210 are both provided with waist-shaped holes with inclined surface features. The ball seat 211 is spherical in shape with a through hole, the axis of which passes through the center of the sphere. The shoulder detection probe is mounted in the through hole of the ball seat 211. The shoulder detection probe passes through the waist-shaped holes of the upper guide plate 209 and the lower guide plate 210 respectively. The ball seat 211 is formed by the rhombus formed by the upper and lower pairs of waist-shaped holes with inclined surface features to form a ball pair.
[0055] The probe shoulder detection can rotate around the center of the ball seat 211, and the ball seat 211 can slide horizontally in the rhombus space composed of inclined surface features; the butterfly screws on both sides of the upper guide pressure plate 209 pass through the through holes to connect to the lower guide pressure plate 210, and the butterfly screws on both sides are tightened to fix the ball seat 211 with the probe.
[0056] Furthermore, the second clamping and releasing assembly includes a second clamping screw 304 and a second butterfly nut 305. The other end of the second upper buckle block 302 is provided with a second notch. The second clamping screw 304 is hinged to the second base 301 through a second pin 303. The second clamping screw 304 can move in and out of the second notch so that after entering the second notch, the second base 301 and the second upper buckle block 302 are clamped by the second butterfly nut 305 on the second clamping screw 304.
[0057] The main charge shell probe position adjustment assembly includes a third probe mounting seat 306, two guide rods 308 and two third height adjustment rotary rods 309;
[0058] There is a notch structure on the upper side of the top edge of the second upper buckle block 302, and the two guide rods 308 are connected to the notch structure. The third probe mounting seat 306 is nested with an oil-free bushing to form a sliding pair with the two guide rods 308; the side surface of the third probe mounting seat 306 forms a sliding fit with the side wall of the notch structure on the top edge of the second upper buckle block, limiting the rotational freedom of the third probe mounting seat 306; the threaded rod ends of the two guide rods are respectively and one-to-one connected with the two third height adjustment rotary rods 309, and the position of the third probe mounting seat 306 on the guide rod can be adjusted by rotating the third height adjustment rotary rod 309; each of the two guide rods is provided with a compression spring, and a number of main charge shell detection probes are installed at the end of the third probe mounting seat 306.
[0059] The clamp 101 , the first base 201 , the first upper buckle block 203 , the second base 301 , and the second upper buckle block 302 are all made of polyoxymethylene.
[0060] The warhead head electrical performance testing tool 1 provided in the embodiment of the present application facilitates adjustment of the relative position of the warhead head and the electrical performance testing device, and can be quickly locked and secured after the position is adjusted, ensuring that the detection probe is accurately and reliably positioned against the detection location.
[0061] Warhead shoulder electrical performance test tool 2, by adjusting the direction and angle of the probe, can simultaneously point to multiple adjacent test points, and after adjusting the position, it can be quickly locked and secured to ensure that the test probe is accurately and reliably placed on the test site;
[0062] Warhead main charge shell electrical performance test tool 3, by rotating the hand-screw nut, to achieve the stability and consistency of the detection probe at the detection point;
[0063] The warhead position limiting mechanism can be quickly loaded and locked, and an adjustment slider is designed to achieve position limits for warheads of different lengths;
[0064] The materials selected for the design of various components of the electrical performance testing tooling are mainly to ensure that environmental interference is avoided during the electrical performance testing of the warhead and to ensure the implementation of the process.
[0065] The specific structure and usage method of the warhead electrical performance detection probe adjustment and fixing device provided in this application are introduced in detail below.
[0066] The present invention mainly comprises a warhead head electrical performance detection tool 1, a shoulder electrical performance detection tool 2 and a main charge shell electrical performance detection tool 3.
[0067] Among them, such as Figure 2 As shown, the head electrical performance detection tooling 1 is mainly composed of a fixture 101, a head detection probe a102, a head detection probe b103, a first main guide rod 104, a first auxiliary guide rod 105, a first probe mounting seat 106, a first height adjustment rod 107, a first compression spring 108, an oil-free bushing 109, a second screw sleeve 110, a first screw sleeve 111 and a first butterfly screw 112.
[0068] Specifically, the clamp 101 is designed as an open circular sleeve, and a first butterfly screw 112 is arranged at the opening to facilitate quick clamping and loosening. The opposite side of the opening of the clamp 101 is a movable mechanism, which specifically refers to a guiding part sliding with a first probe mounting seat 106 by a first main guide rod 104 and a first auxiliary guide rod 105. The two guide rods are installed outside the clamp 101, and the first probe mounting seat 106 is nested with two oil-free bushings 109 to form a sliding pair with the two guide rods. The first main guide rod 104 is longer than the first auxiliary guide rod 105 by a threaded rod, and the first main guide rod 104 is provided with a first height adjustment rotating rod 107 at the end of the threaded rod. The position of the first probe mounting seat 106 on the two guide rods can be adjusted by rotating the first height adjustment rotating rod 107. Each of the two guide rods is provided with a first compression spring 108 as a force closing action part. The end faces of the two guide rods are provided with flat round head inner hexagonal screws for limiting the movement of the first probe mounting seat 106. The first probe mounting seat 106 is nested with a head detection probe a 102 and a head detection probe b 103 for electrical performance detection.
[0069] In order to improve the accuracy of electrical performance detection, the clamp 101 is made of polyformaldehyde material, the first probe mounting seat 106 is made of epoxy glass cloth paper substrate, and the first height adjustment rotating rod 107 is made of polyformaldehyde material. A second screw sleeve 110 is nested at the opening of the clamp 101 to facilitate the frequent tightening and loosening action of the first butterfly screw 112, and a first screw sleeve 111 is nested in the first height adjustment rotating rod 107 to facilitate the frequent tightening and loosening action of the first height adjustment rotating rod 107, thereby improving the service life of the whole tool.
[0070] As can be seen, the warhead head electrical performance detection tool 1 adopts an open circular sleeve design, uses a butterfly screw for quick clamping and loosening, and is convenient for manual operation. The probe mounting seat slides up and down through two parallel guide rods, one of which has a threaded feature at the upper part, cooperates with a height adjustment rotating rod, and controls the up and down stop position of the probe mounting seat together with the compression spring installed at the lower part of the guide rod. This structure design can facilitate the test personnel to adjust the relative position of the probe and the detection position, and after the position adjustment is completed, the relative position of the tool and the warhead can also be quickly fixed and stable.
[0071] As shown in Figure 3 , the shoulder electrical performance detection tool 2 mainly comprises a first base 201, a first limiting block 202, a first upper clamping block 203, a first hinge pin 204, a first pin 205, a first compression screw 206, a first butterfly nut 207, a second probe mounting seat 208, an upper guide pressing plate 209, a lower guide pressing plate 210, a compression spring, a ball seat 211, a shoulder detection probe 212, a butterfly screw, a second main guide rod 213, a second auxiliary guide rod 214, and a second height adjustment rotating rod 215.
[0072] Specifically, the inner opening enclosed by the first base 201 and the first upper buckle block 203 is octagonal. The two lower oblique sides of the first base 201 and the two upper oblique sides of the first upper buckle block 203 are designed with step structures of the same height to fit the shoulder structure of the warhead and limit its axial movement space. Each of the 2 oblique sides of the first base 201 has a through slot, and the first limit block 202 can slide up and down in the through slot. A butterfly screw is connected to the outside to fix the position of the first limit block 202 in the through slot. The first limit block 202 can be extended or retracted to accommodate different warheads with different axial limit distances. The first base 201 and the first upper buckle block 203 are connected on one side by a first hinge pin 204. The first upper buckle block 203 can be rotated open around the first hinge pin 204 to facilitate the insertion or removal of the warhead. On the other side of the first base 201 and the first upper buckle block 203, a first clamping screw 206 is mounted on the side of the first base 201 via a first pin 205. The first clamping screw 206 can be rotated and flipped upward around the first pin 205. A first butterfly nut 207 is mounted on the first clamping screw 206 to facilitate locking the first upper buckle block 203. The top edge of the first upper buckle block 203 is connected to the second probe mounting base 208. The second probe mounting base 208 is connected to a second main guide rod 213 and a second secondary guide rod 214. The upper guide plate 209 is nested in an oil-free bushing, forming a sliding pair with the two guide rods. A second height adjustment lever 215, attached to the second main guide rod 213, adjusts the position of the upper guide plate 209 on the two guide rods. Each guide rod has a compression spring to maintain a closed force. The lower portion of the upper guide plate 209 has a waist-shaped hole with a beveled feature and two through holes on either side. The upper portion of the lower guide plate 210 has a similar waist-shaped hole with inclined features, with screw sleeves nested on both sides. The ball seat 211 is spherical in shape with a through hole, the axis of which passes through the center of the ball. The through hole of the ball seat 211 is installed with a shoulder detection probe 212 needle. The probe passes through the waist-shaped holes of the upper guide plate 209 and the lower guide plate 210 respectively. Four sets of ball seats 211 with probes are arranged side by side in the waist-shaped holes. The ball seats 211 are formed by the rhombus formed by two pairs of upper and lower inclined features to form a ball pair. The shoulder detection probe 212 can rotate around the center of the ball seat 211. The ball seat 211 can also slide horizontally within the rhombus space formed by the inclined features, achieving a certain degree of fine-tuning of the angle and position of the shoulder detection probe 212 in a small space. The butterfly screws on both sides of the upper guide plate 209 pass through the through holes and connect to the lower guide plate 210. Tightening the butterfly screws on both sides fixes the ball seat 211 with probes.
[0073] To improve the accuracy of electrical performance testing, the first base 201 and first upper buckle block 203 are made of polyformaldehyde, the second probe mounting base 208 is made of epoxy glass cloth paper-based material, and the second height adjustment rod 215 is also made of polyformaldehyde. A threaded sleeve is embedded in the second height adjustment rod 215, facilitating frequent tightening and loosening of the rod, thereby extending the overall service life of the tooling.
[0074] As can be seen, the warhead shoulder electrical performance testing tool 2 adopts an octagonal clamping design, with the base occupying the lower five sides and the upper buckle block occupying the upper three sides. The upper buckle block is connected to the base via a hinge pin, which facilitates the opening and closing of the upper buckle block, allowing the warhead to be inserted and removed. The upper buckle block uses a butterfly nut to quickly lock and release the warhead. Boss structures are designed on the oblique sides of the base and the upper buckle block to limit the axial movement of the warhead. The upper guide pressure plate 209 and the lower guide pressure plate 210 are designed with waist-shaped holes with inclined surface features. Four sets of ball seats 211 with detection probes installed pass through the upper and lower waist-shaped holes. The ball seats 211 form a ball pair between the prisms formed by the upper and lower inclined surface features, allowing the detection probes to be adjusted in angle. The ball seats 211 can also slide horizontally on the inclined surface to adjust the relative position of the detection probes. The upper guide plate 209 and the lower guide plate are connected by butterfly screws. Tightening the butterfly screws can lock the angle and position of the fixed ball seat 211, thereby fixing the direction and position of the detection probe.
[0075] like Figure 4 As shown, the main charge shell electrical performance detection tool 3 is mainly composed of a second base 301, a second upper block 302, a second hinge pin, a second pin 303, a second clamping screw 304, a second butterfly nut 305, a third probe mounting seat 306, a compression spring, a main charge shell detection probe 307, a guide rod 308 and a third height adjustment rotary rod 309.
[0076] Specifically, the second base 301 and the second upper buckle block 302 enclose an inner opening that is octagonal. The two lower oblique sides of the second base 301 and the two upper oblique sides of the second upper buckle block 302 are designed with step structures of the same height to fit the shoulder structure of the warhead and limit its axial movement space. The second base 301 and the second upper buckle block 302 are connected on one side by a second hinge pin. The second upper buckle block 302 can be rotated around the second hinge pin to open, making it easier to put the warhead in or out. On the other side of the second base 301 and the second upper buckle block 302, a second clamping screw 304 is installed on the side of the second base 301 through a second pin 303. The second clamping screw 304 can be rotated around the second pin 303 and flipped up. There is a second butterfly nut 305 on the second clamping screw 304 to facilitate locking the second upper buckle block 302. The second upper buckle block 302 has a notch on the top edge, within which two guide rods are connected. The third probe mount 306 is nested with an oil-free bushing, forming a sliding pair with the guide rods. The side of the third probe mount 306 forms a sliding fit with the sidewall of the notch on the top edge of the second upper buckle block 302, limiting the rotational freedom of the third probe mount 306. Each threaded end of the two guide rods has a third height adjustment rod 309. Rotating the third height adjustment rod 309 adjusts the position of the third probe mount 306 on the guide rod 308. Each of the two guide rods 308 has a compression spring that acts as a force-closing component for adjustment. A main charge shell detection probe is mounted at the end of the third probe mount 306.
[0077] To improve the accuracy of electrical performance testing, the second base 301 and second upper buckle 302 are made of polyoxymethylene, the third probe mounting base 306 is made of epoxy glass cloth paper-based material, and the third height adjustment rod 309 is also made of polyoxymethylene. A threaded sleeve b is inserted into the third height adjustment rod 309, facilitating frequent tightening and loosening of the rod 309 and extending the overall service life of the tooling.
[0078] As can be seen, the warhead main charge shell electrical performance test fixture 3, like the warhead shoulder electrical performance test fixture 2, adopts an octagonal clamping design. The boss structure designed on the base and the oblique edge of the upper buckle block, together with the boss structure on the warhead electrical performance test fixture, constitutes a structural form that limits the axial movement of the warhead. There are two sets of electrical performance test probes on the upper buckle block of the warhead main charge shell electrical performance test fixture 3. Specifically, the two sets of electrical performance test probes are each guided up and down by a guide rod. The notch structure on the upper mouth block limits the rotation of the probe mounting seat around the guide rod. The height adjustment lever on the upper part of the guide rod and the compression spring on the lower part control the up and down position of the probe mounting seat.
[0079] The warhead electrical performance detection probe adjustment and fixing device provided in the embodiment of the present application is used as follows: Figure 5 As shown, the shoulder electrical performance test tool 2 and the main charge shell electrical performance test tool 3 can be installed on the tray 4. The tray 4 is provided with an electrical inspection box 5 and a quick connection plate 6 that are electrically connected to each other. The head electrical performance test tool 1 can be connected to the mounting bracket of the quick connection plate 6. After the warhead is fixed, the probes of each tool are brought into contact with the detection points on the warhead, and then the wiring terminals of each probe are connected to the spring aging clips on the quick connection plate 6, so that the probes are electrically connected to the quick connection plate 6 and the electrical inspection box 5. Transport the tray 4 and all the components on it to the electrical inspection tool. After the electrical inspection box 5 is connected to the electrical inspection mother box at the electrical inspection tool, the electrical performance test of the warhead can be carried out.
[0080] In summary, the warhead electrical performance detection probe adjustment and fixing device provided by the present application allows testers to adjust and fix the warhead probe through the device, ensuring that the test probe can effectively and stably abut against the warhead test point during the electrical performance detection process, avoiding the fluctuation of electrical performance detection data caused by unstable test point abutment due to human control. The shoulder electrical performance detection tooling and the main charge shell electrical performance detection tooling can restrain the axial movement of the warhead through the step features designed on the bevel. The shoulder electrical performance detection tooling and the main charge shell electrical performance detection tooling can keep the warhead stable during transportation through the upper buckle block that can be flipped open and buckled, and the butterfly nut lock design that can be quickly pressed, locked and loosened. The detection probe is stably abutted. By adjusting the protrusion and retraction of the shoulder electrical performance detection tooling limit block, the axial limit of warheads of different lengths can be compatible.
[0081] It should be noted that, in this document, relational terms such as first and second, etc., are used only to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply the existence of any such actual relationship or order between these entities or operations. Moreover, the terms "comprises," "comprising," or any other variants thereof are intended to cover non-exclusive inclusion, so that a process, method, article, or device comprising a series of elements includes not only those elements, but also other elements not explicitly listed, or elements inherent to such process, method, article, or device. In the absence of further limitations, an element defined by the phrase "comprising a ..." does not exclude the presence of other identical elements in the process, method, article, or device comprising the element.
[0082] Through the description of the above embodiments, it can be seen that those skilled in the art can clearly understand that the present application can be implemented by means of software plus a necessary general hardware platform. Based on this understanding, the technical solution of the present application, or the part that contributes to the prior art, can be embodied in the form of a software product, which can be stored in a storage medium such as ROM / RAM, a magnetic disk, an optical disk, etc., and includes a number of instructions for enabling a computer device (which can be a personal computer, a server, or a network device, etc.) to execute the methods described in various embodiments or certain parts of the embodiments of the present application.
[0083] Each embodiment in this specification is described in a progressive manner. The same or similar parts between the embodiments can be referred to each other. Each embodiment focuses on the differences from other embodiments. In particular, for system or system embodiments, since they are basically similar to method embodiments, the description is relatively simple. For relevant parts, refer to the partial description of the method embodiment. The system and system embodiments described above are merely schematic, wherein the units described as separate components may or may not be physically separated, and the components displayed as units may or may not be physical units, that is, they may be located in one place, or they may be distributed on multiple network units. Some or all of the modules can be selected according to actual needs to achieve the purpose of the solution of this embodiment. A person of ordinary skill in the art can understand and implement it without expending creative work.
[0084] The above description is only a preferred embodiment of the present invention and is not intended to limit the scope of protection of the present invention. Any modifications, equivalent replacements, improvements, etc. made within the spirit and principles of the present invention are included in the scope of protection of the present invention.
Claims
1. A warhead electrical performance detection probe adjustment and fixing device, characterized in that: include: A head electrical performance testing tool, comprising a connected fixture and a first probe unit; The fixture includes an open circular sleeve structure with a first butterfly screw at the opening to achieve clamping and loosening with the warhead head; the first probe unit includes a plurality of head detection probes and a head probe position adjustment assembly, the head probe position adjustment assembly being used to adjust the plurality of head detection probes to abut against a plurality of electrical performance detection points on the warhead head in a one-to-one correspondence after the fixture is clamped with the warhead head; A shoulder electrical performance testing tool, the shoulder electrical performance testing tool comprising a first base, a first upper buckle block, a first clamping and releasing assembly and a second probe unit; one end of the first upper buckle block is hinged to the first base through a first hinge pin, so that the first upper buckle block can be rotated around the first hinge pin to open so that the shoulder of the warhead can enter between the first upper buckle block and the first base; the first clamping and releasing assembly is used to realize the clamping and releasing of the first base and the first upper buckle block; the second probe unit is connected to the first upper buckle block, the second probe unit comprises a number of shoulder detection probes and a shoulder probe position adjustment assembly, the shoulder probe position adjustment assembly is used to adjust a number of the shoulder detection probes to correspond one by one to abut against a number of shoulder electrical performance testing points of the warhead after the first base and the first upper buckle block are clamped to the shoulder of the warhead; A tool for testing the electrical performance of a main charge shell, the tool comprising a second base, a second upper buckle block, a second clamping and releasing assembly and a third probe unit; one end of the second upper buckle block is hinged to the second base through a second hinge pin, so that the second upper buckle block can be rotated open around the second hinge pin to allow the main charge shell of the warhead to enter between the second upper buckle block and the second base; the second clamping and releasing assembly is used to realize the clamping and releasing of the second base and the second upper buckle block; the third probe unit is connected to the second upper buckle block, and the third probe unit comprises a number of main charge shell detection probes and a main charge shell probe position adjustment assembly, the main charge shell probe position adjustment assembly is used to adjust a number of the main charge shell detection probes to correspond one by one to abut against a number of main charge shell electrical performance detection points of the warhead after the second base and the second upper buckle block are clamped with the main charge shell of the warhead.
2. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The head probe position adjustment assembly includes a first main guide rod, a first auxiliary guide rod, a first probe mounting seat and a first height adjustment rotary rod; The plurality of head detection probes are fixedly connected to the first probe mounting seat; one end of each of the first main guide rod and the first auxiliary guide rod is connected to the clamp, and the first main guide rod and the first auxiliary guide rod are connected to the first probe mounting seat so as to be relatively slidable; the first main guide rod and the first auxiliary guide rod are each provided with a first compression spring at a position between the clamp and the first probe mounting seat; One end of the first main guide rod extends away from the clamp to the outside of the first probe mounting seat and is connected to a first height adjustment rod through a first screw sleeve. The position of the first probe mounting seat relative to the clamp is adjusted by the first height adjustment rod to allow the front end of the head detection probe to enter and exit the clamp.
3. The warhead electrical performance detection probe adjustment and fixing device according to claim 2, characterized in that: The first auxiliary guide rod is connected to the first probe mounting seat through an oil-free bushing; a second screw sleeve is provided at the opening of the clamp, and the first butterfly screw is connected to the second screw sleeve; the material of the first probe mounting seat is epoxy glass cloth paper-based board material, and the material of the first height adjustment rod is polyformaldehyde material.
4. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The first compression and release assembly includes a first compression screw and a first butterfly nut. A first notch is provided at the other end of the first upper buckle block. The first compression screw is hinged to the first base through a first pin. The first compression screw can enter and exit the first notch, so that after entering the first notch, the first base and the first upper buckle block are compressed by the first butterfly nut on the first compression screw.
5. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: When the first base and the first upper buckle block are pressed together, an octagonal structure is formed inside. The two lower oblique sides of the first base and the two upper oblique sides of the first upper buckle block are designed with step structures of the same height to fit the shoulder structure of the warhead.
6. The warhead electrical performance detection probe adjustment and fixing device according to claim 5, characterized in that: Each of the two lower oblique sides of the first base has a through slot, and a limit block that can slide up and down is set in the through slot. The outer side of the limit block is connected to a second butterfly screw, and the second butterfly screw is used to fix the position of the limit block in the through slot so that the limit block can be extended or retracted to be compatible with different axial limit distances of different warheads.
7. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The shoulder probe position adjustment assembly includes a second probe mounting seat, an upper guide pressure plate, a lower guide pressure plate, a ball seat, a second main guide rod and a second auxiliary guide rod; The second probe mounting seat is connected to the first upper buckle block, one end of each of the second main guide rod and the second secondary guide rod is fixedly connected to the second probe mounting seat, and the second main guide rod and the second secondary guide rod are both connected to the upper guide pressure plate so as to be slidable relative to each other; the second main guide rod and the second secondary guide rod are each provided with a second compression spring at a position between the second probe mounting seat and the upper guide pressure plate; One end of the second main guide rod away from the second probe mounting seat extends to the outside of the upper guide pressure plate and is connected to a second height adjustment rod through a second screw sleeve, and the position of the upper guide pressure plate relative to the second probe mounting seat is adjusted by the second height adjustment rod; The lower portion of the upper guide plate and the upper portion of the lower guide plate are both provided with waist-shaped holes with inclined surface features; the ball seat is spherical in shape with a through hole, the axis of the through hole passing through the center of the sphere; the shoulder detection probe is installed in the through hole of the ball seat, and the shoulder detection probe passes through the waist-shaped holes of the upper guide plate and the lower guide plate respectively. The ball seat is formed by the rhombus formed by the upper and lower pairs of waist-shaped holes with inclined surface features to form a ball pair; The probe shoulder detection can rotate around the center of the ball seat, and the ball seat can slide horizontally in the diamond space composed of inclined surface features; the butterfly screws on both sides of the upper guide pressure plate pass through the through holes to connect the lower guide pressure plate, and the butterfly screws on both sides are tightened to fix the ball seat with the probe.
8. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The second compression and release assembly includes a second compression screw and a second butterfly nut. A second notch is provided at the other end of the second upper buckle block. The second compression screw is hinged to the second base through a second pin. The second compression screw can enter and exit the second notch, so that after entering the second notch, the second base and the second upper buckle block are compressed by the second butterfly nut on the second compression screw.
9. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The main charge shell probe position adjustment assembly includes a third probe mounting seat, two guide rods and two third height adjustment rotary rods; There is a notch structure on the upper side of the top edge of the second upper buckle block, and the two guide rods are connected to the notch structure. The third probe mounting seat is nested with an oil-free bushing to form a sliding pair with the two guide rods; the side surface of the third probe mounting seat forms a sliding fit with the side wall of the notch structure on the top edge of the second upper buckle block, limiting the rotational freedom of the third probe mounting seat; the threaded rod ends of the two guide rods are respectively and one-to-one connected with the two third height adjustment rotary rods, and the position of the third probe mounting seat on the guide rod can be adjusted by rotating the third height adjustment rotary rod; each of the two guide rods is provided with a compression spring, and a number of main charge shell detection probes are installed at the end of the third probe mounting seat.
10. The warhead electrical performance detection probe adjustment and fixing device according to claim 1, characterized in that: The clamp, the first base, the first upper buckle block, the second base and the second upper buckle block are all made of polyformaldehyde.
Citation Information
Patent Citations
Warhead manufacturing device
CN108592713A
All-day intelligent homing flapping wing bionic ammunition and control method
CN116929158A