CN220662857U - Coaxial unmanned aerial vehicle with broken window function - Google Patents
Coaxial unmanned aerial vehicle with broken window function Download PDFInfo
- Publication number
- CN220662857U CN220662857U CN202322464138.4U CN202322464138U CN220662857U CN 220662857 U CN220662857 U CN 220662857U CN 202322464138 U CN202322464138 U CN 202322464138U CN 220662857 U CN220662857 U CN 220662857U
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- fixedly connected
- movable
- coaxial
- unmanned aerial
- aerial vehicle
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- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 6
- 229910052742 iron Inorganic materials 0.000 claims description 3
- 239000011521 glass Substances 0.000 description 9
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- TVEXGJYMHHTVKP-UHFFFAOYSA-N 6-oxabicyclo[3.2.1]oct-3-en-7-one Chemical compound C1C2C(=O)OC1C=CC2 TVEXGJYMHHTVKP-UHFFFAOYSA-N 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 230000003116 impacting effect Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
Classifications
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/40—Weight reduction
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Abstract
The utility model discloses a coaxial unmanned aerial vehicle with a window breaking function, which comprises a coaxial unmanned aerial vehicle body, wherein foot frames are fixedly connected to two sides of the bottom end of the coaxial unmanned aerial vehicle body, two supporting rods are fixedly connected between the two foot frames together, a cross post is fixedly connected to the top ends of the two supporting rods together, a first movable cavity is formed in one side, close to a head of the coaxial unmanned aerial vehicle body, of the cross post, an inner cavity is formed in the other side of the cross post.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to a coaxial unmanned aerial vehicle with a window breaking function.
Background
The coaxial double-rotor unmanned aerial vehicle can provide a lift-off scientific experiment platform with medium-low altitude, large range and high maneuverability for various scientific task loads. The automatic flight control system has the advantages that the automatic flight control system has the purely manual and automatic flight control modes, and the operation complexity of operators is effectively reduced on the premise that the flight safety and scientific tasks are satisfactorily completed. Meanwhile, the requirements of various scientific flight tasks can be met.
The existing coaxial unmanned aerial vehicle can carry equipment with specified weight to execute tasks, but in some special scenes, such as when high-altitude window breaking is needed, the existing coaxial unmanned aerial vehicle cannot complete the operation, so in order to improve the practicability of the existing coaxial unmanned aerial vehicle, the utility model provides the coaxial unmanned aerial vehicle with the window breaking function.
Disclosure of Invention
The utility model aims to solve the defects in the prior art, and provides a coaxial unmanned aerial vehicle with a window breaking function.
In order to achieve the above purpose, the present utility model adopts the following technical scheme: the utility model provides a coaxial unmanned aerial vehicle with broken window function, includes coaxial unmanned aerial vehicle organism, the equal fixedly connected with foot rest in coaxial unmanned aerial vehicle organism bottom both sides, two common fixedly connected with two bracing pieces between the foot rest, two the bracing piece top is fixedly connected with diaphragm jointly, the diaphragm is close to coaxial unmanned aerial vehicle organism aircraft nose one side and has seted up first movable chamber, and first movable chamber section is square, the inner chamber has been seted up to diaphragm opposite side inside, first movable chamber is close to coaxial unmanned aerial vehicle organism aircraft nose one side and has been seted up first opening, the inside sliding connection of first opening has the movable rod, the servo motor that drives the movable rod and remove is located the one end of first movable chamber of movable rod, the second movable chamber has been seted up to diaphragm one end, the second movable chamber is kept away from the diaphragm one end, the inside broken window structure that is provided with of second movable chamber, the second movable chamber roof is provided with the block structure that is used for fixing broken window structure, the one end that the movable rod is close to the second opening is fixedly connected with contact switch.
Further, servo motor drive end fixedly connected with lead screw, servo motor one end is kept away from to the lead screw extends to inside the first movable chamber, the lead screw runs through the movable rod and with the movable rod screw thread rotation is connected. The screw rod is driven to rotate through the servo motor, and the screw rod can drive the movable rod to move along the first movable cavity.
Further, one end of the moving rod, which is positioned in the first movable cavity, is fixedly connected with a first sliding plate, and the size of the first sliding plate is larger than that of the first opening. When the moving rod moves in the first movable cavity, the first sliding plate can prevent the moving rod from being separated from the first movable cavity.
Further, the window breaking structure comprises a first spring fixed on the inner wall of the second movable cavity, the other end of the first spring is fixedly connected with a second sliding plate, and the other side of the second sliding plate is fixedly connected with an impact needle. The first spring ejects the impact pin, so that the impact pin can impact glass, and window breaking is realized.
Further, the second slide plate is larger than the second opening in size. When the striker pin moves to the outside of the second movable cavity, the second sliding plate can prevent the striker pin from being separated from the second movable cavity.
Further, the draw-in groove has been seted up to second slide top lateral wall, the block structure is including being fixed in the fixed pipe at second movable chamber top, roof fixedly connected with second spring in the fixed pipe, second spring bottom fixedly connected with draw-in lever, the draw-in lever bottom card is gone into inside the draw-in groove. The clamping rod is pushed downwards through the second spring, so that the clamping rod can be clamped inside the clamping groove, and the second sliding plate and the striking needle are fixed.
Further, the inner top wall of the fixed pipe is fixedly connected with an electromagnet, the electromagnet is electrically connected with the contact switch, and the clamping rod is made of iron. After the contact switch is contacted with the glass window, the electromagnet is electrified, the clamping rod is attracted by the electromagnet, the clamping rod is separated from the clamping groove, and the impact needle can be ejected out by the first spring.
The utility model has the beneficial effects that:
when the coaxial unmanned aerial vehicle is used, the coaxial unmanned aerial vehicle body, the foot rest, the supporting rod, the transverse column, the moving rod, the servo motor, the screw rod, the window breaking structure, the clamping structure and the contact switch are arranged, when the coaxial unmanned aerial vehicle body approaches to a window with the transverse column, once the contact switch contacts with the glass window, the clamping rod of the clamping structure is retracted, at the moment, the first spring of the window breaking structure can rapidly eject the impact needle, the impact needle is used for impacting the glass, the window breaking function is achieved, and therefore the practicability of the unmanned aerial vehicle is improved.
Drawings
FIG. 1 is an overall schematic of the present utility model;
FIG. 2 is a partial perspective view of the present utility model;
FIG. 3 is an enlarged view of FIG. 1 at A;
fig. 4 is an enlarged view at B in fig. 1.
Legend description:
1. a coaxial unmanned aerial vehicle body; 2. a foot rest; 3. a support rod; 4. a cross column; 41. an inner cavity; 42. a first movable chamber; 43. a first opening; 5. a first slide plate; 6. a moving rod; 7. a servo motor; 8. a screw rod; 9. a second movable chamber; 10. a second opening; 11. a window breaking structure; 111. a first spring; 112. a second slide plate; 113. a clamping groove; 114. a striker pin; 12. a clamping structure; 121. a fixed tube; 122. a second spring; 123. a clamping rod; 124. an electromagnet; 13. and a contact switch.
Detailed Description
As shown in fig. 1-4, the coaxial unmanned aerial vehicle with window breaking function includes a coaxial unmanned aerial vehicle body 1, two sides of the bottom end of the coaxial unmanned aerial vehicle body 1 are fixedly connected with a foot rest 2, two support rods 3 are fixedly connected between the two foot rest 2, a cross column 4 is fixedly connected with the top ends of the two support rods 3, a first movable cavity 42 is formed on one side of the cross column 4, which is close to the head of the coaxial unmanned aerial vehicle body 1, the cross section of the first movable cavity 42 is square, an inner cavity 41 is formed in the other side of the cross column 4, a first opening 43 is formed on one side, which is close to the head of the coaxial unmanned aerial vehicle body 1, of the first movable cavity 42, a movable rod 6 is slidably connected in the first opening 43, a servo motor 7 for driving the movable rod 6 to move is fixedly mounted in the inner cavity 41, a second movable cavity 9 is formed in one end, which is located outside the first movable cavity 42, of the second movable cavity 9 is far away from the cross column 4, a second opening 10 is formed in one end, a window breaking structure 11 is formed in the second movable cavity 9, a clamping structure 12 is formed on the top wall of the second movable cavity 9, which is used for fixing the window breaking structure 11, and a first opening 6 is fixedly connected with a contact switch 13.
The servo motor 7 drive end fixedly connected with lead screw 8, the lead screw 8 keep away from servo motor 7 one end and extend to inside the first movable chamber 42, and lead screw 8 runs through movable rod 6 and is connected with movable rod 6 screw thread rotation.
When the coaxial unmanned aerial vehicle body 1 moves to the front of glass to be broken with the transverse column 4, the screw rod 8 can be driven by the motor to rotate, and the screw rod 8 is used for driving the moving rod 6 to move out of the first movable cavity 42, so that the window breaking structure 11 is close to the glass.
The first sliding plate 5 is fixedly connected to one end of the moving rod 6 located in the first movable cavity 42, and the size of the first sliding plate 5 is larger than that of the first opening 43. By providing the first slide plate 5, the movable rod 6 can be prevented from being separated from the first movable chamber 42 when moving toward the first movable chamber 42.
The window breaking structure 11 comprises a first spring 111 fixed on the inner wall of the second movable cavity 9, the other end of the first spring 111 is fixedly connected with a second sliding plate 112, and the other side of the second sliding plate 112 is fixedly connected with an impact needle 114. The striker pin 114 can be ejected from the inside of the second movable chamber 9 by the first spring 111 so that the striker pin 114 strikes the glass. The second slide plate 112 is larger in size than the second opening 10. And second slide plate 112 is provided to prevent striker pin 114 from being disengaged from second movable chamber 9 when moved outwardly.
The clamping groove 113 is formed in the side wall of the top end of the second sliding plate 112, the clamping structure 12 comprises a fixed tube 121 fixed at the top of the second movable cavity 9, a second spring 122 is fixedly connected to the inner top wall of the fixed tube 121, a clamping rod 123 is fixedly connected to the bottom end of the second spring 122, and the bottom end of the clamping rod 123 is clamped into the clamping groove 113.
The second spring 122 pushes the locking rod 123 downwards in a normal state, and after the bottom of the locking rod 123 is locked into the locking groove 113, the second sliding plate 112 and the striking pin 114 are fixed inside the second movable cavity 9.
The electromagnet 124 is fixedly connected to the inner top wall of the fixing tube 121, the electromagnet 124 is electrically connected to the contact switch 13, and the clamping rod 123 is made of iron. The clamping rod 123 can be attracted by energizing the electromagnet 124, so that the clamping rod 123 can be separated from the clamping groove 113.
Working principle: the coaxial unmanned aerial vehicle body 1 drives the transverse column 4 to fly to a designated position, then the servo motor 7 is started to drive the screw rod 8 to rotate, the screw rod 8 drives the moving rod 6 to move out of the first movable cavity 42, after the contact switch 13 contacts glass, the electromagnet 124 is electrified, the electromagnet 124 adsorbs the clamping rod 123, the clamping rod 123 is separated from the clamping groove 113, at the moment, the first spring 111 can rapidly push the second sliding plate 112 and the striking needle 114, and the striking needle 114 slides out from the second opening 10 and impacts the glass to break windows.
The foregoing description of the preferred embodiments of the utility model is not intended to limit the utility model to the precise form disclosed, and any such modifications, equivalents, and alternatives falling within the spirit and scope of the utility model are intended to be included within the scope of the utility model.
Claims (7)
1. Coaxial unmanned aerial vehicle with broken window function, including coaxial unmanned aerial vehicle organism (1), its characterized in that: the utility model discloses a coaxial unmanned aerial vehicle organism (1) bottom both sides fixedly connected with foot rest (2), two common fixedly connected with bracing piece (3) between foot rest (2), two common fixedly connected with diaphragm (4) in bracing piece (3) top, first movable chamber (42) have been seted up to diaphragm (4) near coaxial unmanned aerial vehicle organism (1) aircraft nose one side, and first movable chamber (42) cross section is square, inner chamber (41) have been seted up inside diaphragm (4) opposite side, first movable chamber (42) are close to coaxial unmanned aerial vehicle organism (1) aircraft nose one side and have been seted up first opening (43), first opening (43) inside sliding connection has movable rod (6), servo motor (7) that the inside fixedly mounted of inner chamber (41) has driven movable rod (6) to remove, second movable chamber (9) have been seted up to one end that movable rod (6) are located outside first movable chamber (42), second movable chamber (9) keep away from diaphragm (4) one end and have been seted up second opening (10), second movable chamber (9) are close to one side of coaxial unmanned aerial vehicle organism aircraft nose one side has been seted up first opening (43), first opening (4), inside sliding connection has movable rod (6) drive the inside movable rod (6) is equipped with drive motor (9) to move outside the one side (42), one end of the movable rod (6) close to the second opening (10) is fixedly connected with a contact switch (13).
2. A coaxial drone with a window breaking function as claimed in claim 1, wherein: the servo motor (7) drive end fixedly connected with lead screw (8), lead screw (8) keep away from servo motor (7) one end and extend to inside first movable chamber (42), lead screw (8) run through movable rod (6) and with movable rod (6) screw thread rotation connection.
3. A coaxial drone with a window breaking function as claimed in claim 2, wherein: one end of the moving rod (6) positioned in the first movable cavity (42) is fixedly connected with a first sliding plate (5), and the size of the first sliding plate (5) is larger than that of the first opening (43).
4. A coaxial drone with a window breaking function as claimed in claim 1, wherein: the window breaking structure (11) comprises a first spring (111) fixed on the inner wall of the second movable cavity (9), the other end of the first spring (111) is fixedly connected with a second sliding plate (112), and the other side of the second sliding plate (112) is fixedly connected with an impact needle (114).
5. The coaxial drone with a window breaking function of claim 4, wherein: the second slide plate (112) is larger in size than the second opening (10).
6. The coaxial drone with a window breaking function of claim 4, wherein: the clamping groove (113) is formed in the side wall of the top end of the second sliding plate (112), the clamping structure (12) comprises a fixed tube (121) fixed to the top of the second movable cavity (9), a second spring (122) is fixedly connected to the inner top wall of the fixed tube (121), a clamping rod (123) is fixedly connected to the bottom end of the second spring (122), and the bottom end of the clamping rod (123) is clamped into the clamping groove (113).
7. The coaxial drone with a window breaking function of claim 6, wherein: the inner top wall of the fixed pipe (121) is fixedly connected with an electromagnet (124), the electromagnet (124) is electrically connected with the contact switch (13), and the clamping rod (123) is made of iron.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322464138.4U CN220662857U (en) | 2023-09-12 | 2023-09-12 | Coaxial unmanned aerial vehicle with broken window function |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322464138.4U CN220662857U (en) | 2023-09-12 | 2023-09-12 | Coaxial unmanned aerial vehicle with broken window function |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220662857U true CN220662857U (en) | 2024-03-26 |
Family
ID=90340946
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322464138.4U Active CN220662857U (en) | 2023-09-12 | 2023-09-12 | Coaxial unmanned aerial vehicle with broken window function |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220662857U (en) |
-
2023
- 2023-09-12 CN CN202322464138.4U patent/CN220662857U/en active Active
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