Unmanned aerial vehicle window breaker
By carrying a window breaker on the drone, using a combination of arrow hammers and window hammers, the problems of low efficiency and major safety hazards in high-altitude window breaking rescue are solved, and efficient and safe window breaking effect is achieved.
Patent Information
- Application Number
- CN202510372181.9
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- Filing Date
- 2025-03-27
- Publication Date
- 2025-04-25
- Estimated Expiration
- Not applicable · inactive patent
AI Technical Summary
The existing high-altitude broken window rescue operations are inefficient and have major safety hazards.
A drone window breaker was designed, including a drive unit, a launch unit, an arrow and an arrow basin. The drone was equipped with an arrow launcher, and the combination of arrow hammer and window hammer was used to achieve efficient breaking of windows.
The continuous launch of arrows has been achieved, the efficiency of breaking windows has been improved, the safety risks during the rescue process has been reduced, and the efficiency of rescue is improved.
Smart Images

Figure CN119868844A_ABST
Abstract
Description
Technical Field
[0001] The present invention relates to the technical field of aviation emergency rescue, and in particular to a window breaker for unmanned aerial vehicles. Background Art
[0002] As the emergency rescue system continues to improve, there are demands for greater mobility, professionalism and modernization in the modern emergency rescue system. The use of drone technology in the emergency field is an urgent need of modern society and an important manifestation of the continuous modernization of emergency rescue technology.
[0003] Drones have more advantages than traditional emergency rescue methods in terms of cost, flexibility, maneuverability and environment. At the same time, the advantages of drones such as small size, high speed and easy operation enable them to be used in conjunction with various devices and sensors to work in various environments, which greatly helps in emergency service support, on-site searches, emergency communications and other aspects.
[0004] Since modern buildings are generally tall, when conducting fire rescue, firefighters need to climb or use ropes to descend to the windows on the floors to break windows and then conduct rescue operations. The process is slow, which affects the rescue efficiency and poses a major safety hazard.
[0005] Therefore, based on the continuous requirements of the modern rescue system, the present invention proposes a drone window breaker, which uses a drone to carry out window breaking operations, which is more efficient and safer, and plays a positive role in improving rescue efficiency and ensuring the life safety of people to be rescued and rescuers. Summary of the invention
[0006] The purpose of the present invention is to provide an unmanned aerial vehicle window breaker to solve the problems of slow window breaking efficiency and great safety hazards in existing high-altitude window breaking and rescue operations.
[0007] To achieve the above-mentioned purpose, the present invention adopts the following technical solution: a drone window breaker includes a driving unit, a launching unit, an arrow and an arrow chamber; The launching unit comprises a bow and arrow, the bow and arrow comprises a bow arm and a bow string, and the driving unit cooperates with the bow string through a bow pulling mechanism; The arrows are stored in the arrow chamber. When the bow drawing mechanism draws the bow to full draw, the bow string cooperates with the tail end of the arrow. The bow string continues to be drawn, and the bow drawing mechanism releases the bow string. Under the action of the bow string, the arrow is shot out. The arrow magazine stores a plurality of arrows. When a previous arrow is shot out, a subsequent arrow replaces the previous arrow, and the bow drawing mechanism cooperates with the bowstring again to achieve continuous shooting of arrows. An arrow hammer is arranged at the front end of the arrow, and a window-breaking hammer is arranged around the energy storage of the front end of the arrow. When the arrow hammer contacts the window, the energy stored in the window-breaking hammer is released due to the impact force exerted on the arrow hammer, and the arrow hammer cooperates with the window-breaking hammer to break the window.
[0008] A drone quick release is arranged above the arrow warehouse, and the window breaker of the present invention cooperates with the drone through the drone quick release, and the driving unit is connected to the drone quick release.
[0009] Furthermore, the driving unit includes an electric push rod, which is located below the arrow magazine. The front end of the push rod is connected to the bow drawing mechanism, and the bow drawing mechanism cooperates with the bowstring.
[0010] Furthermore, bowstring grooves are provided on both sides of the arrow magazine, and the bowstring grooves cooperate with the bowstring; the bow drawing mechanism includes a connecting rod, and two connecting rods are provided and symmetrically arranged on both sides of the arrow magazine; one end of the connecting rod is hinged to the front end of the push rod, and the other end of the connecting rod is hinged to the buckle, and the buckle cooperates with the bowstring.
[0011] Furthermore, a first torsion spring is arranged between the buckle and the connecting rod, and guide grooves are respectively arranged on both sides of the arrow magazine, and the guide grooves cooperate with the buckle; the buckle includes a hanging part and a top block matching part, the hanging part cooperates with the bowstring, and the top block matching part cooperates with the top block; the top block is arranged at the end of the arrow magazine, and when the bowstring is pulled to the full bow and cooperates with the tail end of the arrow, the bowstring continues to be pulled, the top block cooperates with the top block matching part and forces the buckle to rotate to release the bowstring.
[0012] Furthermore, a fixing mechanism is provided at the upper end of the arrow magazine, which compresses and fixes the arrows in the arrow magazine, and the fixing mechanism does not interfere with the quick release of the drone in space; in the arrow magazine, a limiting mechanism is provided between the arrows; when the previous arrow is shot out, the next arrow moves downward under the action of the fixing mechanism, and the limiting mechanism loses its limiting effect under the action of the downward force of the fixing mechanism, and when the next arrow replaces the position of the previous arrow, the limiting mechanism starts to work again.
[0013] Furthermore, the fixing mechanism includes a pressure plate mounting portion and a torsion spring matching portion, the pressure plate is rotatably mounted by the pressure plate mounting portion, a second torsion spring is installed between the pressure plate and the torsion spring matching portion, and the pressure plate matches the topmost arrow.
[0014] Furthermore, the limiting mechanism includes an installation groove, in which a connecting spring is arranged, one end of the connecting spring is fixedly connected to the installation groove, and the other end of the connecting spring is fixedly connected to the limiting block, and the limiting block is located between the two arrows and cooperates with the two arrows respectively.
[0015] Furthermore, the arrow includes an arrow shaft, the front end of the arrow shaft is hollow, and the arrow hammer is installed in the hollow part; a pressure ring is sleeved on the outside of the arrow shaft, and the pressure ring is in transmission with the arrow hammer; the window breaking hammer is arranged around the front end of the arrow shaft, one end of the window breaking hammer is hinged to the arrow shaft, and the other end of the window breaking hammer cooperates with the pressure ring, and a compression spring is arranged between the window breaking hammer and the arrow shaft.
[0016] Furthermore, the end of the arrow hammer is connected to the second spring, and limiting rods are arranged on both sides of the rear end of the arrow hammer, and a limiting groove is arranged on the arrow shaft, and the limiting rod extends out of the limiting groove and cooperates with the pressure ring.
[0017] Furthermore, a limiting portion is provided on the arrow shaft, a first spring is provided between the limiting portion and the pressure ring, and the first spring is sleeved on the arrow shaft.
[0018] Beneficial effects of the present invention: 1. The present invention can realize the continuous firing of arrows. Multiple firings can effectively ensure the window breaking effect, effectively improve the window breaking efficiency, and play a positive role in ensuring the rescue efficiency; 2. The present invention adopts a method of cooperating a window-breaking hammer with an arrow hammer to further improve the effect of breaking windows from point to surface, which is of great significance to rescue operations and has broad application prospects. BRIEF DESCRIPTION OF THE DRAWINGS
[0019] Figure 1 It is a schematic diagram of the overall structure of the present invention; Figure 2 This is a schematic diagram of the structure of the present invention (UAV quick disassembly); Figure 3 is a schematic diagram of the bow drawing mechanism of the present invention; Figure 4 The present invention Figure 3 A partial enlarged schematic diagram of part A; Figure 5 It is a schematic diagram of the bowstring buckle and connecting rod structure of the present invention; Figure 6 It is a schematic diagram of the matching structure of the bowstring and the buckle of the present invention; Figure 7 The present invention Figure 3 A partial enlarged schematic diagram of part B; Figure 8 It is a schematic diagram of the arrow magazine structure of the present invention; Fig. 9 It is a schematic diagram of the structure of the limiting mechanism of the present invention; Fig.10 It is a schematic diagram of the structure when the two arrows are limited in position; Fig.11 Schematic diagram of the arrow structure of the present invention (arrow hammer is not under stress); Fig.12 It is a schematic diagram of the arrow structure of the present invention (stress state of the arrow hammer); Fig.13 It is a schematic diagram of the arrow hammer structure of the present invention.
[0020] The names corresponding to the marks in the figure are: 1. Electric push rod; 11. Driving motor; 12. Push rod; 2. Bow drawing mechanism; 21. Connecting rod; 22. Buckle mounting part; 221. Guide groove matching part; 23. Buckle; 231. Hanging part; 232. Top block matching part; 24. First torsion spring; 3. Bow and arrow; 31. Bow arm; 32. Bow string; 4. Arrow chamber; 41. Bow string groove; 42. Guide groove; 43. Top block; 44. Limiting mechanism; 441. Mounting groove; 442. Limit block; 45. Fixing mechanism; 451. Pressure plate mounting portion; 452. Torsion spring matching portion; 453. Pressure plate; 454. Second torsion spring; 5. Arrow; 51. Arrow shaft; 511. Limit groove; 52. Limit portion; 53. First spring; 54. Pressing ring; 541. Limit rod matching groove; 55. Arrow hammer; 551. Limit rod; 56. Window breaking hammer; 57. Compression spring; 58. Second spring; 6. Quick release; 7. Mounting frame. DETAILED DESCRIPTION
[0021] The technical solution of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention.
[0022] like Figure 1-13 As shown, the window breaker of the present invention includes an electric push rod 1, which drives a bow-drawing mechanism 2, and the bow-drawing mechanism 2 drives a bow and arrow 3 to realize the firing of an arrow 5. An arrow hammer 55 and a window-breaking hammer 56 are arranged at the front end of the arrow 5 to realize the breaking of the window.
[0023] In this embodiment, the electric push rod 1 includes a driving motor 11, which is connected to the push rod 12 in a transmission manner; an arrow chamber 4 is fixedly installed above the electric push rod 1, and a bow and arrow 3 is fixedly installed at the front end of the arrow chamber 4. The bow and arrow 3 includes a bow arm 31 and a bow string 32. Bow string grooves 41 are provided on the two side walls of the arrow chamber 4, and the bow string grooves 41 match the bow string 32; the two sides of the front end of the push rod 12 are respectively connected to the connecting rod 21 for rotation, and the other end of the connecting rod 21 is connected to the buckle mounting part 22 for rotation, and the buckle 23 is rotatably installed through the buckle mounting part 22. Mounting plates are provided on both sides of the buckle 23, and the buckle 23 is rotatably plugged into the buckle mounting portion 22 through the mounting plates. A first torsion spring 24 is provided between the two mounting plates, and the first torsion spring 24 is sleeved on the buckle mounting portion 22. The two pins of the first torsion spring 24 respectively cooperate with the connecting rod 21 and the buckle 23; guide grooves 42 are also provided on both sides of the arrow magazine 4, and the guide grooves 42 are located below the bowstring groove 41, and the guide grooves 42 cooperate with the buckle mounting portion 22, and a guide groove matching portion 221 matching with the guide grooves 42 is provided on the buckle mounting portion 22.
[0024] The connecting rod 21 pulls the buckle 23 to move in the direction of the guide groove 42. A hanging portion 231 is provided above the buckle 23. In the direction of the guide groove 42, the tip of the hanging portion 231 extends to below the maximum diameter of the bowstring 32 in this direction, so as to prevent the bowstring 32 from falling off during the process of pulling the bowstring 32. A top block matching portion 232 is provided below the buckle 23, and a top block 43 is provided at the end of the arrow chamber 4. The top block 43 matches with the top block matching portion 232. Under the action of the top block 43, the buckle 23 moves along the guide groove 42. Figure 3 The bow string 32 is shown rotated and released in a clockwise direction.
[0025] An arrow 5 is placed in the arrow chamber 4. In the present embodiment, two arrows 5 are provided, one above and one below. During the placement of the arrow 5, the arrow 5 is pressed on the bowstring. When the bowstring 32 is pulled to the tail end of the arrow 5 under the action of the bow drawing mechanism 2, the bowstring 32 bounces upward and contacts the tail end of the arrow 5, thereby launching the arrow 5.
[0026] A fixing mechanism 45 is provided on one side above the arrow magazine 4 , and the fixing mechanism 45 is used to fix the two arrows 5 . A limiting mechanism 44 is provided between the two arrows 5 to avoid mutual influence between the two arrows 5 .
[0027] The fixing mechanism 45 includes a pressure plate mounting portion 451 and a torsion spring matching portion 452. A pressure plate 453 is rotatably mounted through the pressure plate mounting portion 451, and a second torsion spring 454 is rotatably mounted through the pressure plate mounting portion 451. Two pins of the second torsion spring 454 are respectively matched with the torsion spring matching portion 452 and the pressure plate 453. Under the action of the second torsion spring 454, the pressure plate 453 is tightly pressed on the upper arrow 5.
[0028] The limiting mechanism 44 includes a mounting groove 441, and the mounting groove 441 is arranged on both sides of the arrow magazine 4. A connecting spring is fixedly installed in the mounting groove 441, one end of the connecting spring is fixedly connected to the inner side of the mounting groove 441, and the other end of the connecting spring is fixedly connected to a limiting block 442. The two limiting blocks 442 are located between the two arrows 5 under the action of the connecting spring force, and an arc-shaped matching portion is provided at the position where the two limiting blocks 442 contact the arrows 5. When the arrow below is shot out, under the action of the upper pressure plate 453, the limiting block 442 shrinks into the mounting groove 441, and the arrow 5 above is pressed into the bottom of the limiting block 442, and the limiting block 442 pops out to fix the arrow 5.
[0029] A mounting frame 7 is provided above the arrow magazine 4 , and a UAV quick release 6 is mounted through the mounting frame 7 . The window breaker of the present invention is docked with the UAV through the quick release 6 , and a driving motor 11 is connected to the quick release 6 .
[0030] In this embodiment, the arrow 5 includes an arrow shaft 51, the front end of the arrow shaft 51 is hollow and an arrow hammer 55 is installed therein, wherein a limiting rod 551 is provided at the end of the arrow hammer 55, a second spring 58 is sleeved on the arrow hammer 55, and the second spring 58 is clamped and fixed by the limiting rod 551, and a limiting groove 511 is correspondingly provided on the arrow shaft 51, the limiting rod 551 cooperates with the limiting groove 511 and extends to the outside of the arrow shaft 51 through the limiting rod matching groove 541.
[0031] A limiting portion 52 is provided on the arrow shaft 51, a pressing ring 54 is provided behind the limiting rod 551, a first spring 53 is provided between the pressing ring 54 and the limiting portion 52, the first spring 53 is sleeved on the arrow shaft 51, a limiting rod matching groove 541 is provided on the pressing ring 54, and the limiting rod matching groove 541 matches with the limiting rod 551.
[0032] A window breaking hammer 56 is also provided at the front part of the arrow shaft 51. The front end of the window breaking hammer 56 is hinged to the arrow shaft 51, and the rear end of the window breaking hammer 56 is pressed and fixed by a pressing ring 54. A compression spring 57 is provided between the window breaking hammer 56 and the arrow shaft 51. The upper end of the compression spring 57 is fixedly connected to the window breaking hammer 56, and the lower end of the compression spring 57 abuts against the arrow shaft 51.
[0033] The principle of the present invention is: During use of the present invention, two arrows 5 are loaded into the arrow magazine 4. During the process, there is no need to disassemble the drone quick release 6, etc. The arrows 5 are inserted backwards from the front end of the arrow magazine 4. During the process, the lower arrow 5 is installed first, and then the upper arrow 5 is installed. When installing the upper arrow 5, the pressure plate 453 at the rear of the arrow magazine 4 is pulled up. After the installation is completed, the pressure plate 453 is lowered, which can realize the compression and fixation of the two arrows 5. During the process, the pressure plate 453 and the quick release 6 do not interfere with each other in space. At the same time, it should be noted during the installation process that the angle of the lower arrow 5 during the installation process is adjusted so that the bowstring 32 is pressed below the lower arrow 5.
[0034] After the installation is completed, the drone can be docked with the drone through the drone quick release 6, and the drone can be controlled to take off to the designated location to perform the window breaking operation. During the process, the drone controls the action of the electric push rod 1 (the electric push rod 1 is existing and will not be described in detail). The push rod 12 of the electric push rod 1 drives the connecting rod 21 during the extension process, and the connecting rod 21 pulls the bowstring 32 through the buckle 23. When the bowstring 32 is pulled to the tail end of the arrow shaft 51, the bowstring 32 bounces upward and rests on the tail end of the arrow shaft 51. The bowstring 32 continues to be pulled. Under the action of the top block 43, the buckle 23 rotates and releases the bowstring 32, thereby launching the arrow 5 below.
[0035] When the arrow 5 below is launched, since the upper arrow 5 is suspended in the air (there is no support below the limit block 442), under the action of the pressure plate 453, the limit block 442 contracts inward and presses the upper arrow 5 downward. When the arrow 5 is pressed downward, the limit block 442 pops up to fix the arrow 5. At this time, the electric push rod 1 retracts. When the electric push rod 1 contacts the bowstring 32, due to the smooth design of the front end of the buckle 23, the bowstring 32 is forced to bend and deform downward and cooperate with the buckle 23. The above process is repeated to achieve the launch of the second arrow 5.
[0036] When the arrow 5 is fired, the arrow hammer 55 at the front end of the arrow 5 first contacts the glass, and a cracking network centered on the impact point appears at the contact point between the arrow hammer 55 and the glass. Under the action of the impact force, the arrow hammer 55 contracts backwards. At this time, the limit rod 551 drives the pressure ring 54 to contract backwards. When the pressure ring 54 contracts backwards, under the action of the compression spring 57, the window-breaking hammer 56 pops outward, thereby further smashing the above-mentioned cracking network and realizing the process of breaking the glass.
[0037] The present invention is not limited to the above-mentioned optimal implementation mode. Anyone can derive other various forms of products under the inspiration of the present invention. However, no matter what changes are made in the shape or structure, all technical solutions that are the same or similar to those of the present application fall within the protection scope of the present invention.
Claims
1. UAV window breaker, characterized by: It comprises a driving unit, a launching unit, an arrow (5) and an arrow chamber (4); The launching unit comprises a bow and arrow (3), the bow and arrow (3) comprises a bow arm (31) and a bow string (32), and the driving unit cooperates with the bow string (32) through the bow drawing mechanism (2); The arrow (5) is stored in the arrow chamber (4). When the bow drawing mechanism (2) draws the bow (3) to a full draw, the bow string (32) cooperates with the tail end of the arrow (5). The bow string (32) is continuously drawn, and the bow drawing mechanism (2) releases the bow string (32). Under the action of the bow string (32), the arrow (5) is shot out. The arrow magazine (4) stores a plurality of arrows (5). When a previous arrow (5) is shot out, a subsequent arrow (5) replaces the previous arrow (5), and the bow-drawing mechanism (2) is re-coordinated with the bowstring (32) to achieve continuous shooting of the arrows (5). The front end of the arrow (5) is provided with an arrow hammer (55), and the energy storage around the front end of the arrow (5) is provided with a window-breaking hammer (56). When the arrow hammer (55) contacts the window, the energy stored in the window-breaking hammer (56) is released due to the impact force exerted on the arrow hammer (55), and the arrow hammer (55) cooperates with the window-breaking hammer (56) to break the window. A drone quick release (6) is provided above the arrow magazine (4), and the window breaker of the present invention cooperates with the drone via the drone quick release (6), and the drive unit is connected to the drone quick release (6).
2. The drone window breaker according to claim 1, characterized in that: The driving unit comprises an electric push rod (1), the electric push rod (1) is located below the arrow magazine (4), the front end of the push rod (12) in the electric push rod (1) is connected to the bow drawing mechanism (2), and the bow drawing mechanism (2) cooperates with the bow string (32).
3. The drone window breaker according to claim 2, characterized in that: Bowstring grooves (41) are provided on both sides of the arrow magazine (4), and the bowstring grooves (41) cooperate with the bowstring (32); the bow drawing mechanism (2) includes a connecting rod (21), and two connecting rods (21) are provided and symmetrically arranged on both sides of the arrow magazine (4); one end of the connecting rod (21) is hinged to the front end of the push rod (12), and the other end of the connecting rod (21) is hinged to the buckle (23), and the buckle (23) cooperates with the bowstring (32).
4. The drone window breaker according to claim 3, characterized in that: A first torsion spring (24) is arranged between the buckle (23) and the connecting rod (21), and guide grooves (42) are respectively arranged on both sides of the arrow magazine (4), and the guide grooves (42) cooperate with the buckle (23); the buckle (23) includes a hanging portion (231) and a top block matching portion (232), the hanging portion (231) cooperates with the bowstring (32), and the top block matching portion (232) cooperates with the top block (43); the top block (43) is arranged at the end of the arrow magazine (4), when the bowstring (32) is pulled to a full bow and matches with the tail end of the arrow (5), the bowstring (32) is continued to be pulled, and the top block (43) cooperates with the top block matching portion (232) and forces the buckle (23) to rotate to release the bowstring (32).
5. The drone window breaker according to claim 1, characterized in that: The upper end of the arrow magazine (4) is provided with a fixing mechanism (45), which compresses and fixes the arrows (5) in the arrow magazine (4), and the fixing mechanism (45) does not interfere with the drone quick release (6) in space; in the arrow magazine (4), a limiting mechanism (44) is provided between the arrows (5) and the arrows (5); when the first arrow (5) is shot out, the second arrow (5) moves downward under the action of the fixing mechanism (45), and the limiting mechanism (44) loses its limiting effect under the action of the downward force of the fixing mechanism (45); when the second arrow (5) replaces the position of the first arrow (5), the limiting mechanism (44) starts to function again.
6. The drone window breaker according to claim 5, characterized in that: The fixing mechanism (45) comprises a pressure plate mounting portion (451) and a torsion spring matching portion (452), a pressure plate (453) is rotatably mounted on the pressure plate mounting portion (451), a second torsion spring (454) is mounted between the pressure plate (453) and the torsion spring matching portion (452), and the pressure plate (453) matches with the uppermost arrow (5).
7. The drone window breaker according to claim 5, characterized in that: The limiting mechanism (44) comprises a mounting groove (441), a connecting spring is arranged in the mounting groove (441), one end of the connecting spring is fixedly connected to the mounting groove (441), and the other end of the connecting spring is fixedly connected to a limiting block (442), and the limiting block (442) is located between the two arrows (5) and cooperates with the two arrows (5) respectively.
8. The drone window breaker according to claim 1, characterized in that: The arrow (5) comprises an arrow shaft (51), the front end of the arrow shaft (51) is hollow, and an arrow hammer (55) is installed in the hollow part; a pressure ring (54) is sleeved on the outside of the arrow shaft (51), and the pressure ring (54) and the arrow hammer (55) are arranged in a transmission manner; a window-breaking hammer (56) is arranged around the front end of the arrow shaft (51), one end of the window-breaking hammer (56) is hinged to the arrow shaft (51), and the other end of the window-breaking hammer (56) is matched with the pressure ring (54), and a compression spring (57) is arranged between the window-breaking hammer (56) and the arrow shaft (51).
9. The drone window breaker according to claim 8, characterized in that: The end of the arrow striker (55) is connected to the second spring (58), and limiting rods (551) are arranged on both sides of the rear end of the arrow striker (55), and a limiting groove (511) is arranged on the arrow rod (51), and the limiting rod (551) extends out of the limiting groove (511) and cooperates with the pressure ring (54).
10. The drone window breaker according to claim 9, characterized in that: The arrow shaft (51) is provided with a limiting portion (52), a first spring (53) is provided between the limiting portion (52) and the pressure ring (54), and the first spring (53) is sleeved on the arrow shaft (51).
Citation Information
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