CN113716041A - Quick detach formula is open-air patrols line unmanned aerial vehicle - Google Patents
Quick detach formula is open-air patrols line unmanned aerial vehicle Download PDFInfo
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- CN113716041A CN113716041A CN202111064884.3A CN202111064884A CN113716041A CN 113716041 A CN113716041 A CN 113716041A CN 202111064884 A CN202111064884 A CN 202111064884A CN 113716041 A CN113716041 A CN 113716041A
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- 230000003014 reinforcing effect Effects 0.000 claims description 9
- 239000002184 metal Substances 0.000 claims description 7
- 210000001503 joint Anatomy 0.000 claims description 6
- 241000219122 Cucurbita Species 0.000 claims description 3
- 235000009852 Cucurbita pepo Nutrition 0.000 claims description 3
- 238000005452 bending Methods 0.000 claims description 3
- 238000005192 partition Methods 0.000 claims description 3
- 238000007689 inspection Methods 0.000 abstract description 2
- 238000003780 insertion Methods 0.000 description 2
- 230000037431 insertion Effects 0.000 description 2
- 241000463219 Epitheca Species 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000005389 magnetism Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C27/00—Rotorcraft; Rotors peculiar thereto
- B64C27/04—Helicopters
- B64C27/12—Rotor drives
- B64C27/14—Direct drive between power plant and rotor hub
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U10/00—Type of UAV
- B64U10/10—Rotorcrafts
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U50/00—Propulsion; Power supply
- B64U50/10—Propulsion
- B64U50/19—Propulsion using electrically powered motors
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- H—ELECTRICITY
- H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
- H02G—INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
- H02G1/00—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
- H02G1/02—Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U2101/00—UAVs specially adapted for particular uses or applications
Abstract
This application belongs to portable line auxiliary assembly technical field that patrols, especially relates to a quick detach formula open-air unmanned aerial vehicle that patrols. The aircraft comprises an airframe and an airborne line patrol device, wherein the airframe comprises an airframe component and a rotor wing component; the fuselage assembly includes: an upper shell plate and a lower shell plate; the rotor assembly includes: the device comprises a supporting arm, a motor, a rotating block, a quick-connection clamping strip, a rectangular connecting rod, a quick-connection clamping block and a rotor wing; this application is based on actual demand, provides a simple structure is compact, and the quality is light, and dismouting convenient to use is quick, requires low quick detach formula field inspection line unmanned aerial vehicle to service environment and operator. The quick-release type field line patrol unmanned aerial vehicle is simple and light in structure, is integrally connected by adopting the quick-release type buckles, and is stably supported by the supporting structures; unmanned aerial vehicle organism and the equal quick assembly disassembly of rotor are accomodate, carry the use during the outdoor operations of being convenient for.
Description
Technical Field
This application belongs to portable line auxiliary assembly technical field that patrols, especially relates to a quick detach formula open-air unmanned aerial vehicle that patrols.
Background
The electric wire netting operation process involves a large amount of field line patrol operations, because a large amount of transmission network ways are rare to the inconvenient area of road traffic, the environment is complicated, consequently often can only rely on the mode that the manpower was walked to patrol the line, for the work load that reduces manual work, people begin to utilize all kinds of technical equipment to alleviate manual work's work load and the degree of difficulty, wherein portable unmanned aerial vehicle can help the line patrol personnel accurate quick acquisition first hand information data when patrolling the line, all obtain the application in many operation occasions, but receive the restriction of environment and condition, some outdoor operations can't carry more auxiliary equipment facilities, operation people's portable ability is limited, consequently more light, it is simpler to use, unmanned aerial vehicle equipment that the requirement that assembly and use are lower is very necessary to field line patrol the operation.
Disclosure of Invention
The utility model provides an aim at provides a simple structure is compact, and the quality is light, and dismouting convenient to use is quick, requires low quick detach formula field inspection unmanned aerial vehicle to service environment and operator based on actual demand.
In order to achieve the purpose, the following technical scheme is adopted in the application.
A quick-release type field line patrol unmanned aerial vehicle comprises a machine body and airborne line patrol equipment, wherein the machine body comprises a machine body assembly 1 and a rotor wing assembly 2;
the fuselage assembly 1 comprises: an upper shell plate 10 and a lower shell plate 11;
the upper shell plate 10 and the lower shell plate 11 are flat, and the upper shell plate 10 and the lower shell plate 11 are opposite in parallel;
an equipment connecting hole 1a is formed in the center of the upper shell plate 10;
a partition plate is arranged on the outer side of the equipment connecting hole 1a and encloses an equipment mounting box structure 1 b;
the surfaces of the upper shell plate 10 on the front side and the rear side of the equipment mounting box structure 1b form two rotor wing fixing surfaces;
the left side and the right side of the rotor wing fixing plate surface are respectively provided with a plurality of rotor wing mounting holes 1 c;
the center of the lower shell plate 11 is provided with a mounting connecting hole 2a which is coaxial with the equipment connecting hole 1 a;
the lower shell plate 11 is provided with a jack corresponding to the rotor wing mounting hole 1 c;
the rotor assembly 2 includes: the device comprises a support arm 20, a motor 21, a rotating block 22, a quick-connection clamping strip 23, a rectangular connecting rod 24, a quick-connection clamping block 25 and a rotor wing 26;
the support arm 20 is of an L-shaped structure and comprises a short arm 20a and a long arm 20b which are perpendicular to each other;
a plurality of through holes 20c are formed on the short arm 20 a; the through hole corresponds to the rotor wing mounting hole 1c on the rotor wing fixing plate surface;
the motor 21 is fixed at the free end of the long arm 20 b; the rotating block 22 is fixed on the rotating shaft of the motor 21;
the rotating block 22 is in a strip shape, two ends of the rotating block 22 are respectively provided with a rectangular connecting groove 22a, and the bottom of the rectangular connecting groove 22a is provided with a spring;
strip-shaped openings 22b are formed in the left side and the right side of the rectangular connecting groove 22 a;
the quick-connection clamping strip 23 is of a cuboid structure, and the quick-connection clamping strip 23 can be slidably inserted into the rectangular connecting groove 22a and abuts against the spring;
a rectangular hole is formed in the middle of the quick connection clamping strip 23, and the width of the rectangular hole is consistent with that of the strip-shaped opening 22 b;
the rectangular connecting rod 24 extends into the strip-shaped opening 22b and penetrates through the rectangular hole; the thickness of the rectangular connecting rod 24 is consistent with the width of the rectangular hole;
the quick-connection clamping block 25 is of a rectangular flat plate structure, and the length of the quick-connection clamping block is consistent with that of the rotating block 22;
the rotor 26 is fixed on the upper side of the fast-connection clamping block 25;
the quick-connection clamping block 25 is buckled on the upper side of the rotating block 22;
the hook structure 25a is formed by extending four corners of a rectangular flat plate structure downwards and bending the four corners towards the center of the flat plate;
the hook structure 25a may be hung at both ends of the rectangular connecting rod 24.
The quick-release type field line patrol unmanned aerial vehicle further comprises a quick-connection component 3;
the quick-connect assembly 3 comprises: right angle connection plate 30, magnetic connection rod 31, metal lantern ring 32
The right-angle connecting plate 30 comprises a connecting plate surface 30a buckled on the rotor wing fixing plate surface and a positioning plate surface 30b which is perpendicular to the connecting plate surface 30a and extends downwards;
the connecting plate surface 30a is provided with a magnetic connecting rod mounting hole corresponding to the rotor wing mounting hole 1 c;
the magnetic connecting rod 31 is embedded in the magnetic connecting rod mounting hole;
one end of the long arm 20b close to the short arm 20a is provided with a convex clamping part 20 e;
the clamping part 20e and the short arm 20a are respectively arranged at the front side and the rear side of the long arm 20b in a back-to-back manner;
the positioning plate surface 30b is provided with a clamping hole 30e corresponding to the clamping part 20 e;
after the supporting arm 20 is installed, the clamping part 20e is clamped into the clamping hole 30 e;
the metal collar 32 is embedded in each rotor mounting hole 1c and the insertion hole.
In a further improvement or preferred embodiment of the quick-release type field line patrol unmanned aerial vehicle, a movable connecting groove 1d is formed in the bottom of the equipment mounting box structure 1 b;
the movable connecting groove 1d is communicated with the equipment connecting hole 1 a;
a T-shaped anti-falling column 1e is arranged at the bottom of the movable connecting groove 1 d;
a movable connecting plate 4 is arranged in the movable connecting groove 1d, and the middle part of the movable connecting plate 4 is provided with an equipment butt joint hole;
the movable connecting plates 4 are multiple, and the sizes of the equipment butt joint holes on each movable connecting plate 4 respectively correspond to different equipment connecting parts;
the movable connecting plate 4 is provided with a gourd hole which can be clamped on the T-shaped anti-falling column 1 e.
In a further improvement or preferred embodiment of the aforementioned quick-release type field line patrol unmanned aerial vehicle, the rotor 26 is a straight-line double-blade rotor;
the middle part of the double-blade rotor wing is provided with a rotor wing fixing hole 26a, and the double-blade rotor wing is vertical to the length direction of the connecting clamping block 25;
a rotor wing fixing auxiliary hole 25b corresponding to the rotor wing fixing hole 26a is formed in the upper side of the connecting clamping block 25;
the two-blade rotor is fixed on the upper side of the connecting clamping block 25 through bolts or rivets arranged in the rotor fixing holes 26a and the rotor fixing auxiliary holes 25 b.
In a further improvement or preferred embodiment of the quick-release type field line patrol unmanned aerial vehicle, wing-shaped reinforcing parts 22c are arranged on two sides of the middle part of the rotating block 22;
a strip-shaped clamping groove 22d is formed in the outer side of the wing-shaped reinforcing part 22 c;
wing-shaped connecting arms 25c corresponding to the wing-shaped reinforcing parts 22c are arranged at two sides of the connecting clamping block 25
The rotor wing fixing auxiliary hole 25b is dug out from the wing-shaped connecting arm 25 c;
the lower side of the wing-shaped connecting arm 25c is provided with a strip-shaped connecting part 25d which can be clamped into the strip-shaped clamping groove 22 d.
The beneficial effects are that:
the quick-release type field line patrol unmanned aerial vehicle is simple and light in structure, is integrally connected by adopting the quick-release type buckles, and is stably supported by the supporting structures; unmanned aerial vehicle organism and the equal quick assembly disassembly of rotor are accomodate, carry the use during the outdoor operations of being convenient for.
Drawings
FIG. 1 is a front view of a quick release type field line patrol unmanned aerial vehicle;
FIG. 2 is an assembly drawing of a quick release type field line patrol unmanned aerial vehicle;
FIG. 3 is an assembled schematic view of the rotor assembly;
figure 4 is a schematic view of the installation of the rotor assembly;
FIG. 5 is a schematic structural view of a snap-fit latch;
wherein the reference numerals include:
fuselage subassembly 1, equipment connecting hole 1a, equipment fixing box structure 1b, rotor mounting hole 1c, activity spread groove 1d, T shape anticreep post 1e, epitheca board 10, inferior valve plate 11, rotor subassembly 2, carry connecting hole 2a, support arm 20, short arm 20a, long arm 20b, via hole 20c, joint portion 20e, motor 21, rotatory piece 22, rectangle spread groove 22a, strip opening 22b, wing rib 22c, bar draw-in groove 22d, connect the card strip 23 soon, rectangle connecting rod 24, connect fixture block 25 soon, hook structure 25a, rotor fixed auxiliary hole 25b, rotor 26, rotor fixed orifices 26a, connect subassembly 3 soon, right angle connecting plate 30, magnetism connecting rod 31, the metal lantern ring 32, connecting plate face 30a, location face 30b, card hole 30 e.
Detailed Description
The present application will be described in detail with reference to specific examples.
The utility model provides a quick detach formula open-air line unmanned aerial vehicle that patrols, the auxiliary assembly of the line operation is patrolled to various open air of mainly used, for outdoor work personnel provide one kind easy dismouting accomodate, the quality is light, connect reliable line equipment of patrolling.
As shown in fig. 1 and 2, the basic structure of the aircraft comprises an airframe and an onboard line patrol device, wherein the airframe comprises a fuselage assembly 1 and a rotor assembly 2; the onboard line patrol equipment is special equipment for acquiring information related to line patrol, and comprises a camera for acquiring images, GIS equipment for acquiring information such as terrain and the like, and the like.
The fuselage assembly 1 comprises: an upper shell plate 10 and a lower shell plate 11;
the upper shell plate 10 and the lower shell plate 11 are flat, and the upper shell plate 10 and the lower shell plate 11 are opposite in parallel;
an equipment connecting hole 1a is formed in the center of the upper shell plate 10;
a partition plate is arranged on the outer side of the equipment connecting hole 1a and encloses an equipment mounting box structure 1 b;
the surfaces of the upper shell plate 10 on the front side and the rear side of the equipment mounting box structure 1b form two rotor wing fixing surfaces;
the left side and the right side of the rotor wing fixing plate surface are respectively provided with a plurality of rotor wing mounting holes 1 c;
the center of the lower shell plate 11 is provided with a mounting connecting hole 2a which is coaxial with the equipment connecting hole 1 a;
the lower shell plate 11 is provided with a jack corresponding to the rotor wing mounting hole 1 c;
particularly, a movable connecting groove 1d is arranged at the bottom of the equipment mounting box structure 1 b;
the movable connecting groove 1d is communicated with the equipment connecting hole 1 a;
a T-shaped anti-falling column 1e is arranged at the bottom of the movable connecting groove 1 d;
a movable connecting plate 4 is arranged in the movable connecting groove 1d, and the middle part of the movable connecting plate 4 is provided with an equipment butt joint hole;
the movable connecting plates 4 are multiple, and the sizes of the equipment butt joint holes on each movable connecting plate 4 respectively correspond to different equipment connecting parts;
the movable connecting plate 4 is provided with a gourd hole which can be clamped on the T-shaped anti-falling column 1 e.
The rotor assembly 2 includes: the device comprises a support arm 20, a motor 21, a rotating block 22, a quick-connection clamping strip 23, a rectangular connecting rod 24, a quick-connection clamping block 25 and a rotor wing 26;
the support arm 20 is of an L-shaped structure and comprises a short arm 20a and a long arm 20b which are perpendicular to each other;
a plurality of through holes 20c are formed on the short arm 20 a; the through hole corresponds to the rotor wing mounting hole 1c on the rotor wing fixing plate surface;
the motor 21 is fixed at the free end of the long arm 20 b; the rotating block 22 is fixed on the rotating shaft of the motor 21;
the rotating block 22 is in a strip shape, two ends of the rotating block 22 are respectively provided with a rectangular connecting groove 22a, and the bottom of the rectangular connecting groove 22a is provided with a spring;
strip-shaped openings 22b are formed in the left side and the right side of the rectangular connecting groove 22 a;
the quick-connection clamping strip 23 is of a cuboid structure, and the quick-connection clamping strip 23 can be slidably inserted into the rectangular connecting groove 22a and abuts against the spring;
a rectangular hole is formed in the middle of the quick connection clamping strip 23, and the width of the rectangular hole is consistent with that of the strip-shaped opening 22 b;
the rectangular connecting rod 24 extends into the strip-shaped opening 22b and penetrates through the rectangular hole; the thickness of the rectangular connecting rod 24 is consistent with the width of the rectangular hole;
the quick-connection clamping block 25 is of a rectangular flat plate structure, and the length of the quick-connection clamping block is consistent with that of the rotating block 22;
the rotor 26 is fixed on the upper side of the fast-connection clamping block 25;
the quick-connection clamping block 25 is buckled on the upper side of the rotating block 22;
the hook structure 25a is formed by extending four corners of a rectangular flat plate structure downwards and bending the four corners towards the center of the flat plate;
the hook structure 25a may be hung at both ends of the rectangular connecting rod 24.
In particular, in the present embodiment, wing-shaped reinforcing portions 22c are provided at two sides of the middle portion of the rotating block 22;
a strip-shaped clamping groove 22d is formed in the outer side of the wing-shaped reinforcing part 22 c;
wing-shaped connecting arms 25c corresponding to the wing-shaped reinforcing parts 22c are arranged at two sides of the connecting clamping block 25
The rotor wing fixing auxiliary hole 25b is dug out from the wing-shaped connecting arm 25 c;
the lower side of the wing-shaped connecting arm 25c is provided with a strip-shaped connecting part 25d which can be clamped into the strip-shaped clamping groove 22 d.
For convenience of assembly, in the present embodiment, the rotor 26 is a straight-line double-blade rotor;
the middle part of the double-blade rotor wing is provided with a rotor wing fixing hole 26a, and the double-blade rotor wing is vertical to the length direction of the connecting clamping block 25;
a rotor wing fixing auxiliary hole 25b corresponding to the rotor wing fixing hole 26a is formed in the upper side of the connecting clamping block 25;
the two-blade rotor is fixed on the upper side of the connecting clamping block 25 through bolts or rivets arranged in the rotor fixing holes 26a and the rotor fixing auxiliary holes 25 b.
In order to further strengthen the strength of the machine body, the equipment also comprises a quick connection component 3;
the quick-connect assembly 3 comprises: right angle connection plate 30, magnetic connection rod 31, metal lantern ring 32
The right-angle connecting plate 30 comprises a connecting plate surface 30a buckled on the rotor wing fixing plate surface and a positioning plate surface 30b which is perpendicular to the connecting plate surface 30a and extends downwards;
the connecting plate surface 30a is provided with a magnetic connecting rod mounting hole corresponding to the rotor wing mounting hole 1 c;
the magnetic connecting rod 31 is embedded in the magnetic connecting rod mounting hole;
one end of the long arm 20b close to the short arm 20a is provided with a convex clamping part 20 e;
the clamping part 20e and the short arm 20a are respectively arranged at the front side and the rear side of the long arm 20b in a back-to-back manner;
the positioning plate surface 30b is provided with a clamping hole 30e corresponding to the clamping part 20 e;
after the supporting arm 20 is installed, the clamping part 20e is clamped into the clamping hole 30 e;
the metal collar 32 is embedded in each rotor mounting hole 1c and the insertion hole.
Finally, it should be noted that the above embodiments are only used for illustrating the technical solutions of the present application, and not for limiting the protection scope of the present application, and although the present application is described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions can be made on the technical solutions of the present application without departing from the spirit and scope of the technical solutions of the present application.
Claims (5)
1. A quick-release type field line patrol unmanned aerial vehicle comprises a machine body and airborne line patrol equipment, and is characterized in that the machine body comprises a machine body assembly (1) and a rotor wing assembly (2);
the fuselage assembly (1) comprises: an upper shell plate (10) and a lower shell plate (11);
the upper shell plate (10) and the lower shell plate (11) are flat, and the upper shell plate (10) and the lower shell plate (11) are opposite in parallel;
an equipment connecting hole (1a) is formed in the center of the upper shell plate (10);
a partition plate is arranged on the outer side of the equipment connecting hole (1a) and encloses an equipment mounting box structure (1 b);
the surfaces of the upper shell plate (10) positioned on the front side and the rear side of the equipment mounting box structure (1b) form two rotor wing fixing plate surfaces;
the left side and the right side of the rotor wing fixing plate surface are respectively provided with a plurality of rotor wing mounting holes (1 c);
the center of the lower shell plate (11) is provided with a mounting connecting hole (2a) which is coaxial with the equipment connecting hole (1 a);
the lower shell plate (11) is provided with a jack corresponding to the rotor wing mounting hole (1 c);
the rotor assembly (2) comprises: the device comprises a supporting arm (20), a motor (21), a rotating block (22), a quick-connection clamping strip (23), a rectangular connecting rod (24), a quick-connection clamping block (25) and a rotor wing (26);
the supporting arm (20) is of an L-shaped structure and comprises a short arm (20a) and a long arm (20b) which are perpendicular to each other;
a plurality of through holes (20c) are formed in the short arm (20 a); the through hole corresponds to a rotor wing mounting hole (1c) on the rotor wing fixing plate surface;
the motor (21) is fixed at the free end of the long arm (20 b); the rotating block (22) is fixed on the rotating shaft of the motor (21);
the rotating block (22) is strip-shaped, two ends of the rotating block (22) are respectively provided with a rectangular connecting groove (22a), and the bottom of the rectangular connecting groove (22a) is provided with a spring;
strip-shaped openings (22b) are formed in the left side and the right side of the rectangular connecting groove (22 a);
the quick-connection clamping strip (23) is of a cuboid structure, and the quick-connection clamping strip (23) can be slidably inserted into the rectangular connecting groove (22a) and abuts against the spring;
a rectangular hole is formed in the middle of the quick connection clamping strip (23), and the width of the rectangular hole is consistent with that of the strip-shaped opening (22 b);
the rectangular connecting rod (24) extends into the rectangular hole from the strip-shaped opening (22b) and penetrates through the rectangular hole; the thickness of the rectangular connecting rod (24) is consistent with the width of the rectangular hole;
the quick-connection clamping block (25) is of a rectangular flat plate structure, and the length of the quick-connection clamping block is consistent with that of the rotating block (22);
the rotor wing (26) is fixed on the upper side of the quick-connection clamping block (25);
the quick-connection clamping block (25) is buckled on the upper side of the rotating block (22);
hook structures (25a) are arranged at two ends of the connecting clamping block (25);
the hook structure (25a) is formed by extending four corners of a rectangular flat plate structure downwards and bending towards the center of the flat plate;
the hook structures (25a) can be hung at two ends of the rectangular connecting rod (24).
2. The quick-release type field line patrol unmanned aerial vehicle of claim 1, further comprising a quick-connect assembly (3);
the quick-connect assembly (3) comprises: a right angle connecting plate (30), a magnetic connecting rod (31), a metal lantern ring (32)
The right-angle connecting plate (30) comprises a connecting plate surface (30a) buckled on the rotor wing fixing plate surface and a positioning plate surface (30b) which is perpendicular to the connecting plate surface (30a) and extends downwards;
the connecting plate surface (30a) is provided with a magnetic connecting rod mounting hole corresponding to the rotor wing mounting hole (1 c);
the magnetic connecting rod (31) is embedded in the magnetic connecting rod mounting hole;
one end of the long arm (20b) close to the short arm (20a) is provided with a convex clamping part (20 e);
the clamping part (20e) and the short arm (20a) are respectively positioned at the front side and the rear side of the long arm (20b) and are arranged in a back direction;
the positioning plate surface (30b) is provided with a clamping hole (30e) corresponding to the clamping part (20 e);
after the supporting arm (20) is installed, the clamping part (20e) is clamped into the clamping hole (30 e);
the metal lantern ring (32) is embedded in each rotor wing mounting hole (1c) and the jack.
3. The quick-release type field line patrol unmanned aerial vehicle according to claim 1, wherein a movable connecting groove (1d) is formed in the bottom of the equipment mounting box structure (1 b);
the movable connecting groove (1d) is communicated with the equipment connecting hole (1 a);
a T-shaped anti-falling column (1e) is arranged at the bottom of the movable connecting groove (1 d);
a movable connecting plate (4) is arranged in the movable connecting groove (1d), and the middle part of the movable connecting plate (4) is provided with an equipment butt joint hole;
the movable connecting plates (4) are multiple, and the sizes of the equipment butt joint holes on each movable connecting plate (4) respectively correspond to different equipment connecting parts;
the movable connecting plate (4) is provided with a gourd hole which can be clamped on the T-shaped anti-falling column (1 e).
4. The quick release type field line patrol unmanned aerial vehicle of claim 1, wherein the rotor (26) is a straight two-bladed rotor;
the middle part of the double-blade rotor wing is provided with a rotor wing fixing hole (26a), and the double-blade rotor wing is vertical to the length direction of the connecting clamping block (25);
a rotor wing fixing auxiliary hole (25b) corresponding to the rotor wing fixing hole (26a) is formed in the upper side of the connecting clamping block (25);
the double-blade rotor wing is fixed on the upper side of the connecting clamping block (25) through bolts or rivets arranged in the rotor wing fixing holes (26a) and the rotor wing fixing auxiliary holes (25 b).
5. The quick-release type field line patrol unmanned aerial vehicle according to claim 2, wherein wing-shaped reinforcing parts (22c) are arranged on two sides of the middle part of the rotating block (22);
a strip-shaped clamping groove (22d) is formed in the outer side of the wing-shaped reinforcing part (22 c);
wing-shaped connecting arms (25c) corresponding to the wing-shaped reinforcing parts (22c) are arranged on two sides of the connecting clamping block (25)
The rotor wing fixing auxiliary hole (25b) is dug out from the wing-shaped connecting arm (25 c);
the lower side of the wing-shaped connecting arm (25c) is provided with a strip-shaped connecting part (25d) which can be clamped into the strip-shaped clamping groove (22 d).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111064884.3A CN113716041B (en) | 2021-09-11 | 2021-09-11 | Quick detach formula open-air unmanned aerial vehicle that patrols line |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202111064884.3A CN113716041B (en) | 2021-09-11 | 2021-09-11 | Quick detach formula open-air unmanned aerial vehicle that patrols line |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN113716041A true CN113716041A (en) | 2021-11-30 |
| CN113716041B CN113716041B (en) | 2024-01-12 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN202111064884.3A Active CN113716041B (en) | 2021-09-11 | 2021-09-11 | Quick detach formula open-air unmanned aerial vehicle that patrols line |
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