Aircraft control interferometer
By designing the mobile mechanism and storage components in the aviation control interferer, the problem of equipment being out of control during movement is solved, the stability and portability are improved, the risk of collision is reduced, and the use of equipment and part management is simplified.
Patent Information
- Application Number
- CN202421222943.4
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- Filing Date
- 2024-05-31
- Publication Date
- 2025-01-10
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
Existing aviation control interferers cannot be fixed when adjusting the distance between the connecting sleeve and the extended slide rod, causing the equipment to lose control during movement, especially on uneven grounds or stairs, which may cause personnel to Injury or equipment damage.
A moving mechanism including a rotor, a telescopic cylinder, a slide cylinder, a lifting portion, a restricting groove, a spring and a adjusting column are designed. Through the coordination between the adjusting column and the spring, the position of the lifting portion can be fixed to ensure that the interferometer is stable when moving. and through the coordination of storage components such as storage frames, covers and Velcro, it facilitates dragging and storage of equipment and parts.
It effectively reduces the risk of the interferer colliding with other objects during movement, improves the stability and portability of the equipment, avoids equipment damage and personnel injury, and facilitates the use of the equipment and the storage of parts.
Smart Images
Figure CN222339417U_ABST
Abstract
Description
Technical Field
[0001] The utility model relates to the technical field of aviation control, in particular to an aviation control interference instrument. Background Art
[0002] An aviation control jammer is a device that enforces mandatory control over drones or flying model aircraft. It interferes with the drone's remote control signal, cuts off all communication between the drone and the controller, and causes the drone's remote control to malfunction, making it unable to receive aerial images and videos, and unable to locate. When controlling drones in no-fly zones, a jammer is needed to shoot down the drone to prevent further crimes.
[0003] Existing aviation control jammers, when used in some larger confidential places, require multiple people to operate small devices, and the scope of use is limited. When used on larger devices, due to the large size of the devices, it takes more physical effort to move the equipment;
[0004] The existing patent (publication number: CN220359169U) is an aviation control jammer. Through the setting of the walking mechanism, the height of the connecting wheel can be lowered when the device needs to be moved, so that the connecting wheel and the ground are connected together. Combined with the setting of the pulling mechanism, the device can be conveniently dragged away after the connecting wheel is lowered, forming a suitcase state, which is convenient for users to drag and move to the location where it needs to be used.
[0005] In view of the above problems, the existing patent provides a solution, but when adjusting the distance between the connecting sleeve and the extension slide rod, it is unable to fix the position of the extension slide rod, which may cause the interferometer body to suddenly lose control during movement, especially on uneven ground or stairs, increasing the risk of the interferometer body tipping over or hitting other objects, which may cause personal injury or damage to the interferometer body.
[0006] Therefore, an aviation control jammer is proposed. Utility Model Content
[0007] The purpose of the utility model is to provide an aviation control jammer, which can solve the problem that an existing aviation control jammer cannot fix the position of the extended slide bar when adjusting the distance between the connecting sleeve and the extended slide bar, which may cause the jammer body to suddenly lose control during movement, especially on uneven ground or stairs, increasing the risk of the jammer body tipping over or colliding with other objects, which may cause personal injury or damage to the jammer body.
[0008] To achieve the above-mentioned purpose, the utility model provides the following technical solutions: an aviation control jammer, comprising a jammer body and a signal output head, wherein the signal output head is hinged to the top of the jammer body, a moving mechanism for facilitating the movement of the jammer body is arranged on the outside of the jammer body, and a storage component is arranged on the outside of the jammer body;
[0009] The moving mechanism includes a rotating wheel, a telescopic cylinder, a slide cylinder, a lifting part, a limiting groove, a spring and an adjusting column. The rotating wheel is rotatably connected to the outer wall of the interferometer body, the telescopic cylinder and the slide cylinder are bolted to the side wall of the interferometer body, the lifting part is slidably connected to the inside of the telescopic cylinder and the slide cylinder, the limiting groove is opened on the outer wall of the telescopic cylinder, the spring is welded to the inner wall of the lifting part, the adjusting column is welded to one end of the spring, the number of the limiting grooves is several and evenly distributed, and one end of the adjusting column passes through the lifting part and is slidably connected to the lifting part.
[0010] Preferably, the storage assembly comprises a storage frame and a cover plate, the storage frame is bolted to the side wall of the interferometer body, and the cover plate is hinged to the top of the storage frame.
[0011] Preferably, a shielding cloth is sewn on one end of the cover plate, a Velcro is sewn on the outer wall of the shielding cloth, a Velcro mother tape is adhered on the outer wall of the storage frame, and the Velcro son tape is used in conjunction with the Velcro mother tape.
[0012] Preferably, a support rod for improving the stability of the interferometer body is bolted to the bottom of the interferometer body, and the number of the support rods is two and they are symmetrically arranged.
[0013] Preferably, a handle for facilitating lifting the interferometer body is bolted to the side wall of the interferometer body, and a buffer sleeve for preventing the user from being injured is bonded to the outer wall of the handle.
[0014] Preferably, a soft sleeve is welded onto the outer wall of the lifting part, and the soft sleeve is made of rubber material.
[0015] Preferably, a guide rod is welded on the inner wall of the lifting part, a guide groove is provided inside the adjusting column, and one end of the guide rod extends into the inside of the guide groove and is slidably connected to the guide groove.
[0016] Preferably, a limiting ring is welded on the outer wall of one end of the adjusting column to prevent the adjusting column from escaping from the limiting groove.
[0017] Compared with the prior art, the beneficial effects of the utility model are:
[0018] 1. The present application is provided with a moving mechanism, and when in use, the interferometer body moving mechanism can quickly drag and move the interferometer body. When dragging the interferometer body to move, the moving mechanism can prevent the interferometer body from shaking when dragging the interferometer body, thereby greatly reducing the risk of collision between the interferometer body and other objects.
[0019] 2. The present application is provided with a storage component. When the interferometer body is in use, the storage component can be used to store accessories or parts used in the interferometer body, which is convenient for users. BRIEF DESCRIPTION OF THE DRAWINGS
[0020] In order to more clearly illustrate the specific implementation methods of the utility model or the technical solutions in the prior art, the drawings required for use in the specific implementation methods or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are some implementation methods of the utility model. For ordinary technicians in this field, other drawings can be obtained based on these drawings without paying creative work.
[0021] Figure 1 This is the overall structural view of the utility model;
[0022] Figure 2 It is a right side view of the utility model;
[0023] Figure 3 For this utility model Figure 2 The three-dimensional cross-section view at AA in the middle;
[0024] Figure 4 This is a structural view of the handle and buffer sleeve of the utility model;
[0025] Figure 5 For this utility model Figure 1 The enlarged view of point A in the middle;
[0026] Figure 6 For this utility model Figure 3 Enlarged view of point B in the middle.
[0027] Description of reference numerals:
[0028] 1. Interferometer body; 2. Signal output head; 3. Moving mechanism; 4. Storage assembly; 5. Shielding cloth; 6. Velcro; 7. Velcro; 8. Support rod; 9. Handle; 10. Buffer sleeve; 11. Soft sleeve; 12. Guide rod; 13. Guide groove; 14. Limiting ring; 301. Rotating wheel; 302. Telescopic cylinder; 303. Sliding cylinder; 304. Lifting part; 305. Limiting groove; 306. Spring; 307. Adjusting column; 401. Storage frame; 402. Cover plate. DETAILED DESCRIPTION
[0029] 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.
[0030] See also Figures 1 to 6 , the utility model provides a technical solution:
[0031] An aviation control jammer comprises a jammer body 1 and a signal output head 2, wherein the signal output head 2 is hinged to the top of the jammer body 1, a moving mechanism 3 for facilitating the movement of the jammer body 1 is arranged outside the jammer body 1, and a storage component 4 is arranged outside the jammer body 1;
[0032] The moving mechanism 3 includes a rotating wheel 301, a telescopic cylinder 302, a slide 303, a lifting part 304, a limiting groove 305, a spring 306 and an adjusting column 307. The rotating wheel 301 is rotatably connected to the outer wall of the interferometer body 1, the telescopic cylinder 302 and the slide 303 are both bolted to the side wall of the interferometer body 1, the lifting part 304 is slidably connected to the inside of the telescopic cylinder 302 and the slide 303, the limiting groove 305 is opened on the outer wall of the telescopic cylinder 302, the spring 306 is welded to the inner wall of the lifting part 304, the adjusting column 307 is welded to one end of the spring 306, the number of limiting grooves 305 is several and evenly distributed, and one end of the adjusting column 307 passes through the lifting part 304 and is slidably connected to the lifting part 304.
[0033] Specifically, Figure 4 As shown, a support rod 8 for improving the stability of the interferometer body 1 is bolted to the bottom of the interferometer body 1 , and the number of the support rods 8 is two and they are symmetrically arranged.
[0034] Specifically, Figure 4 As shown, a handle 9 for lifting the interferometer body 1 is bolted to the side wall thereof, and a buffer sleeve 10 is bonded to the outer wall of the handle 9 to prevent the user from being injured.
[0035] Specifically, Figure 4 As shown, a soft cover 11 is welded on the outer wall of the lifting part 304, and the soft cover 11 is made of rubber material.
[0036] Specifically, Figure 6 As shown, a guide rod 12 is welded on the inner wall of the lifting part 304 , a guide groove 13 is opened inside the adjusting column 307 , and one end of the guide rod 12 extends into the inside of the guide groove 13 and is slidably connected to the guide groove 13 .
[0037] Specifically, Figure 6 As shown, a limiting ring 14 is welded on the outer wall of one end of the adjusting column 307 to prevent the adjusting column 307 from escaping from the limiting groove 305 .
[0038] When the interferometer body 1 needs to be moved, the user can press the adjustment column 307 to one side so that the adjustment column 307 enters the interior of the telescopic cylinder 302 along the guide rod 12. At this time, the spring 306 contracts, and then the lifting part 304 is pulled upward through the soft cover 11, thereby driving the adjustment column 307 to move. When the adjustment column 307 moves to the interior of another limiting groove 305, the spring 306 will drive the adjustment column 307 to reset, thereby fixing the position of the lifting part 304. When it is necessary to continue to adjust the distance between the lifting part 304 and the telescopic cylinder 302, repeat the above steps. After the adjustment is completed, the user can use the lifting part 304 to drag the interferometer body 1 to move. When dragging the interferometer body 1, the lifting part 304 will not slide inside the telescopic cylinder 302, thereby reducing the risk of collision between the interferometer body 1 and external hard objects.
[0039] Specifically, Figure 4 As shown, the storage assembly 4 includes a storage frame 401 and a cover plate 402 . The storage frame 401 is bolted to the side wall of the interferometer body 1 , and the cover plate 402 is hinged to the top of the storage frame 401 .
[0040] Specifically, Figure 5 As shown, a shielding cloth 5 is sewn to one end of the cover plate 402, a Velcro 6 is sewn to the outer wall of the shielding cloth 5, a Velcro mother tape 7 is adhered to the outer wall of the storage frame 401, and the Velcro 6 and the Velcro mother tape 7 are used in conjunction with each other.
[0041] Before using the device, the user can place some parts or tools needed to use the interferometer body 1 inside the storage frame 401, and then cover the cover 402 and the shielding cloth 5, and then use the Velcro 6 and Velcro 7 to position the cover 402 to prevent the contents inside the storage frame 401 from falling.
[0042] By adopting the above technical solution, the problem that an existing aviation control jammer cannot fix the position of the extended slide rod when adjusting the distance between the connecting sleeve and the extended slide rod is solved, which may cause the jammer body 1 to suddenly lose control during movement, especially on uneven ground or stairs, increasing the risk of the jammer body 1 tipping over or colliding with other objects, thereby possibly causing personal injury or damage to the jammer body 1.
[0043] Working principle: Before using the device, the user can place some parts or tools needed to use the interferometer body 1 inside the storage frame 401, and then cover the cover 402 and the shielding cloth 5, and then use the Velcro 6 and Velcro 7 to position the cover 402 to prevent the contents inside the storage frame 401 from falling. When the interferometer body 1 needs to be moved, the user can press the adjustment column 307 to one side to make the adjustment column 307 enter the interior of the telescopic cylinder 302 along the guide rod 12. At this time, the spring 306 contracts, and then the lifting part 304 is pulled upward through the soft cover 11, so that And drive the adjustment column 307 to move. When the adjustment column 307 moves to the inside of another limiting groove 305, the spring 306 will drive the adjustment column 307 to reset, thereby fixing the position of the lifting part 304. When it is necessary to continue to adjust the distance between the lifting part 304 and the telescopic tube 302, repeat the above steps. After the adjustment is completed, the user can use the lifting part 304 to drag the interferometer body 1 to move. When dragging the interferometer body 1, the lifting part 304 will not slide inside the telescopic tube 302, thereby reducing the risk of collision between the interferometer body 1 and external hard objects.
[0044] Finally, it should be noted that the above embodiments are only used to illustrate the technical solution of the utility model, rather than to limit it. Although the utility model has been described in detail with reference to the aforementioned embodiments, ordinary technicians in this field should understand that they can still modify the technical solutions recorded in the aforementioned embodiments, or replace some or all of the technical features therein with equivalents. However, these modifications or replacements do not make the essence of the corresponding technical solution deviate from the scope of the technical solution of the embodiments of the utility model.
Claims
1. An aviation control jammer, comprising a jammer body (1) and a signal output head (2), characterized in that: The signal output head (2) is hinged to the top of the interferometer body (1), a moving mechanism (3) for facilitating the movement of the interferometer body (1) is arranged outside the interferometer body (1), and a storage component (4) is arranged outside the interferometer body (1); The moving mechanism (3) comprises a rotating wheel (301), a telescopic cylinder (302), a slide cylinder (303), a lifting part (304), a limiting groove (305), a spring (306) and an adjusting column (307); the rotating wheel (301) is rotatably connected to the outer wall of the interferometer body (1); the telescopic cylinder (302) and the slide cylinder (303) are both bolted to the side wall of the interferometer body (1); the lifting part (304) is slidably connected to the inside of the telescopic cylinder (302) and the slide cylinder (303); the limiting groove (305) is provided on the outer wall of the telescopic cylinder (302); the spring (306) is welded to the inner wall of the lifting part (304); the adjusting column (307) is welded to one end of the spring (306); the limiting grooves (305) are in multiple numbers and are evenly distributed; one end of the adjusting column (307) passes through the lifting part (304) and is slidably connected to the lifting part (304).
2. The aviation control jammer according to claim 1, characterized in that: The storage assembly (4) comprises a storage frame (401) and a cover plate (402), wherein the storage frame (401) is bolted to the side wall of the interferometer body (1), and the cover plate (402) is hinged to the top of the storage frame (401).
3. The aviation control jammer according to claim 2, characterized in that: A shielding cloth (5) is sewn onto one end of the cover plate (402), a Velcro tape (6) is sewn onto the outer wall of the shielding cloth (5), a Velcro tape (7) is adhered onto the outer wall of the storage frame (401), and the Velcro tape (6) and the Velcro tape (7) are used in conjunction with each other.
4. The aviation control jammer according to claim 1, characterized in that: The bottom of the interferometer body (1) is bolted with a support rod (8) for improving the stability of the interferometer body (1), and the number of the support rods (8) is two and they are symmetrically arranged.
5. The aviation control jammer according to claim 1, characterized in that: A handle (9) for facilitating lifting the interferometer body (1) is bolted to the side wall of the interferometer body (1), and a buffer sleeve (10) for preventing the user from being injured is bonded to the outer wall of the handle (9).
6. The aviation control jammer according to claim 1, characterized in that: A soft sleeve (11) is welded onto the outer wall of the lifting portion (304), and the soft sleeve (11) is made of rubber material.
7. The aviation control jammer according to claim 1, characterized in that: A guide rod (12) is welded on the inner wall of the lifting part (304), a guide groove (13) is provided inside the adjusting column (307), and one end of the guide rod (12) extends into the inside of the guide groove (13) and is slidably connected to the guide groove (13).
8. The aviation control jammer according to claim 1, characterized in that: A limiting ring (14) is welded on the outer wall of one end of the adjusting column (307) to prevent the adjusting column (307) from escaping from the limiting groove (305).
Citation Information
Patent Citations
Aircraft control interferometer
CN220359169U