阅读说明：本技术 一种方便进行收纳的无人机机翼防护装置 (Conveniently accomodate unmanned aerial vehicle wing protector ) 是由 吴东标 于 2019-12-06 设计创作，主要内容包括：本发明公开了一种方便进行收纳的无人机机翼防护装置,包括机翼连接柱,所述机翼连接柱的顶部连接设置有顶部防护罩,且机翼连接柱的外侧设置有侧向防护罩,所述机翼连接柱的顶端连接有顶部安装柱,所述顶部安装柱与顶部防护罩之间连接有快拆连接机构,所述快拆连接机构由锁紧安装座、固定座、拉动杆、限位块、复位弹簧、扣紧销和扣紧槽组成,所述顶部防护罩的顶部固定安装有一号支撑杆和二号支撑杆,所述一号支撑杆和二号支撑杆的上表面均支撑有多个环形挡条,所述侧向防护罩的内侧水平连接有横向挡条。本发明所述的一种方便进行收纳的无人机机翼防护装置,且能够提高机翼防护装置安装后的稳定性。(The invention discloses an unmanned aerial vehicle wing protection device convenient to store, which comprises a wing connecting column, wherein the top of the wing connecting column is connected with a top protection cover, a lateral protection cover is arranged on the outer side of the wing connecting column, the top end of the wing connecting column is connected with a top mounting column, a quick-release connecting mechanism is connected between the top mounting column and the top protection cover, the quick-release connecting mechanism consists of a locking mounting seat, a fixing seat, a pulling rod, a limiting block, a reset spring, a fastening pin and a fastening groove, a first supporting rod and a second supporting rod are fixedly mounted on the top of the top protection cover, a plurality of annular retaining strips are supported on the upper surfaces of the first supporting rod and the second supporting rod, and a transverse retaining strip is horizontally connected to the inner side of the lateral protection. The wing protection device of the unmanned aerial vehicle, which is convenient to store, can improve the stability of the wing protection device after installation.)

1. The utility model provides an unmanned aerial vehicle wing protector that conveniently accomodates which characterized in that: the wing protection device comprises a wing connecting column (1), wherein a top protection cover (2) is connected to the top of the wing connecting column (1), a lateral protection cover (3) is arranged on the outer side of the wing connecting column (1), a top mounting column (4) is connected to the top of the wing connecting column (1), a quick-release connecting mechanism (5) is connected between the top mounting column (4) and the top protection cover (2), the quick-release connecting mechanism (5) is composed of a locking mounting seat (501), a fixing seat (502), a pulling rod (503), a limiting block (504), a reset spring (505), a fastening pin (506) and a fastening groove (507), a first supporting rod (6) and a second supporting rod (7) are fixedly mounted at the top of the top protection cover (2), and a plurality of annular blocking strips (8) are supported on the upper surfaces of the first supporting rod (6) and the second supporting rod (7), the inboard horizontally connected of side direction protection casing (3) has horizontal blend stop (9), and the inboard of side direction protection casing (3) is connected with vertical blend stop (10) perpendicularly, the bottom of side direction protection casing (3) is connected with bottom sprag device (11), bottom sprag device (11) comprise linking up seat (1101), supporting seat (1102), support column (1103), connecting axle (1104), No. two support columns (1105), linking piece (1106) and expanding spring (1107), the surface of wing spliced pole (1) is close to intermediate position fixed mounting and has connecting seat (12).

2. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the locking mounting seat (501) is fixedly mounted on the upper surface of the top protective cover (2), the fixing seat (502) is fixedly mounted on the outer surface of the locking mounting seat (501), the fixing seat (502) is symmetrically distributed on the two sides of the locking mounting seat (501), the pulling rod (503) penetrates through the inside of the fixing seat (502), the limiting block (504) is fixed at one end of the pulling rod (503), the limiting block (504) is embedded in the inside of the fixing seat (502), one end of the reset spring (505) is fixed on the outer surface of the limiting block (504), the other end of the reset spring (505) is fixed on the inner wall of the fixing seat (502), the reset spring (505) is sleeved on the outer surface of the pulling rod (503), one end of the fastening pin (506) is fixed on the outer surface of the limiting block (504), and the other end of the fastening pin (506) is embedded in the inside of the top mounting column (4), the fastening groove (507) is arranged on the outer surface of the top mounting column (4).

3. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the fastening pin (506) is movably connected with the locking mounting seat (501) and the fixing seat (502) through a limiting block (504), a pulling rod (503) and a return spring (505), and the outer surface of the fastening pin (506) is tangent to the inner surface of the fastening groove (507).

4. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: and a fixing piece is connected between the top mounting column (4) and the wing connecting column (1).

5. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: mutually perpendicular between bracing piece (6) and No. two bracing pieces (7), and all be equipped with the fixed pin between bracing piece (6) and No. two bracing pieces (7) and annular blend stop (8), the radius size of top protection casing (2) is greater than the radius size of annular blend stop (8).

6. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the joint seat (1101) is fixedly arranged at the bottom position of the lateral protective cover (3), the support seat (1102) is fixedly arranged at the bottom of the wing connecting column (1), the end of the first supporting column (1103) is arranged on the inner side of the connecting seat (1101), the connecting shaft (1104) penetrates through the connecting seat (1101) and the first supporting column (1103), one end of the second supporting column (1105) extends to the inner part of the first supporting column (1103), the other end of the second supporting column (1105) extends into the supporting seat (1102), the connecting block (1106) is fixed at one end of the second supporting column (1105), the connecting block (1106) is embedded in the first supporting column (1103), one end of the telescopic spring (1107) is fixed on the outer surface of the connecting block (1106), and the other end of the telescopic spring (1107) is fixed on the inner surface of the first supporting column (1103).

7. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: support column (1103) pass through connecting axle (1104) and link up seat (1101) swing joint, link up seat (1101) and support column (1103) inside all seted up with connecting axle (1104) assorted connecting hole, be connected with the anticreep axle sleeve between connecting axle (1104) and link up seat (1101).

8. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the second supporting column (1105) is movably connected with the first supporting column (1103) through a connecting block (1106) and a telescopic spring (1107).

9. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the inside of supporting seat (1102) is seted up with No. two fixed notches of support column (1105) assorted, and the inside of fixed notch has the slipmat through adhesive bonding.

10. The unmanned aerial vehicle wing protector that conveniently accomodates of claim 1, characterized in that: the top protection cover (2) and the lateral protection cover (3) are connected in an integrated forming mode.

Technical Field

The invention relates to the field of unmanned aerial vehicle related devices, in particular to an unmanned aerial vehicle wing protection device convenient to store.

Background

Unmanned planes are commonly known as unmanned planes, unmanned aerial vehicles, unmanned operational planes and bee-type machines; the wide application is various remote control aircrafts without the need of the pilot to board the aircraft, in particular to unmanned reconnaissance aircrafts in the military, unmanned planes and on-board pilotless cabins, but is provided with an automatic pilot, a program control device and other equipment, and personnel on the ground, a naval vessel or a mother aircraft remote control station pass through radar and other equipment, the unmanned aerial vehicle is tracked, positioned, remotely controlled, telemetered and digitally transmitted, and when the unmanned aerial vehicle flies high in the using process of the unmanned aerial vehicle, the wings of the unmanned aerial vehicle are damaged due to the fact that the unmanned aerial vehicle touches objects such as branches which are raised up possibly because the unmanned aerial vehicle is not well controlled, and the wings of the unmanned aerial vehicle are not provided with any protective device, so that the wings of the unmanned aerial vehicle are not protected in the operation process, the wings of the unmanned aerial vehicle are damaged, economic loss is caused, and the wing protective device of the unmanned aerial vehicle which is convenient to store is an unmanned aerial vehicle wing protective device which is convenient to install and disassemble;

the existing unmanned aerial vehicle protection device is too complex in steps when being installed and detached, inconvenient and quick to install, inconvenient to store the wing protection device, no supporting structure is arranged between the wing protection device and the wing connecting column, the stability of the wing protection device after being installed is poor, and the wing protection device is easy to drop after being installed.

Disclosure of Invention

The invention mainly aims to provide an unmanned aerial vehicle wing protection device convenient to store, which can effectively solve the problems in the background technology.

In order to achieve the purpose, the invention adopts the technical scheme that:

an unmanned aerial vehicle wing protection device convenient to store comprises a wing connecting column, wherein the top of the wing connecting column is connected with a top protection cover, a lateral protection cover is arranged on the outer side of the wing connecting column, the top end of the wing connecting column is connected with a top mounting column, a quick-release connecting mechanism is connected between the top mounting column and the top protection cover, the quick-release connecting mechanism consists of a locking mounting seat, a fixing seat, a pulling rod, a limiting block, a reset spring, a fastening pin and a fastening groove, a first supporting rod and a second supporting rod are fixedly mounted at the top of the top protection cover, a plurality of annular retaining strips are supported on the upper surfaces of the first supporting rod and the second supporting rod, a transverse retaining strip is horizontally connected to the inner side of the lateral protection cover, a vertical retaining strip is vertically connected to the inner side of the lateral protection cover, and a bottom supporting, the bottom support device comprises a joint seat, a support seat, a first support column, a connecting shaft, a second support column, a joint block and a telescopic spring, wherein the connecting seat is fixedly arranged on the outer surface of the wing connecting column close to the middle position.

Preferably, locking mount pad fixed mounting is at the upper surface of top protection casing, fixing base fixed mounting is at the surface of locking mount pad, and fixing base symmetric distribution is in the both sides position of locking mount pad, the pulling rod runs through in the inside of fixing base, the stopper is fixed in the one end of pulling rod, and the stopper inlays the inside of locating the fixing base, reset spring's one end is fixed in the surface of stopper, and reset spring's the other end is fixed in the inner wall of fixing base, the reset spring cover is established at the surface of pulling rod, the one end of straining pin is fixed in the surface of stopper, and the other end of straining pin imbeds to the inside of top erection column, the surface of top erection column is seted up in the straining groove.

Preferably, the fastening pin is movably connected with the locking mounting seat and the fixing seat through a limiting block, a pulling rod and a return spring, and the outer surface of the fastening pin is tangent to the inner surface of the fastening groove.

Preferably, a fixing piece is connected between the top mounting column and the wing connecting column.

Preferably, mutually perpendicular between a bracing piece and No. two bracing pieces, and all be equipped with the fixed pin between a bracing piece and No. two bracing pieces and the annular blend stop, the radius size of top protection casing is greater than the radius size of annular blend stop.

Preferably, join seat fixed mounting in the bottom position of side direction protection casing, supporting seat fixed mounting is in the bottom position of wing spliced pole, the end of a support column sets up in the inboard of joining the seat, the connecting axle runs through in the inside of joining the seat and a support column, the one end of No. two support columns extends to the inside of a support column, and the other end of No. two support columns extends to the inside of supporting seat, the linking piece is fixed in the one end of No. two support columns, and the linking piece inlays the inside of locating a support column, expanding spring's one end is fixed in the surface of linking piece, and expanding spring's the other end is fixed in the internal surface of a support column.

Preferably, the first supporting column is movably connected with the linking seat through a connecting shaft, connecting holes matched with the connecting shaft are formed in the linking seat and the first supporting column, and an anti-falling shaft sleeve is connected between the connecting shaft and the linking seat.

Preferably, the second support column is movably connected with the first support column through a connecting block and a telescopic spring.

Preferably, the inside of supporting seat is seted up with No. two fixed notches of support column assorted, and the inside of fixed notch has the slipmat through the adhesive bonding.

Preferably, the top protection cover and the lateral protection cover are connected in an integrated forming mode.

Compared with the prior art, the invention has the following beneficial effects:

this conveniently accomodate unmanned aerial vehicle wing protector through the quick detach coupling mechanism who sets up, can make things convenient for wing protector's installation and dismantlement to can conveniently accomodate wing protector, improve wing protector's practicality.

Through the bottom supporting device, the wing protection device and the wing connecting column can be supported, so that the stability of the wing protection device after installation can be improved, and the wing protection device is prevented from falling off after installation.

Drawings

Fig. 1 is a schematic view of the overall structure of an unmanned aerial vehicle wing protection device convenient to store according to the invention;

fig. 2 is a schematic structural diagram of a quick release connecting mechanism of an unmanned aerial vehicle wing protection device convenient to store;

fig. 3 is a top view of a top protective cover of an unmanned aerial vehicle wing guard of the present invention that facilitates stowing;

fig. 4 is a side view of a side shield of an unmanned aerial vehicle wing guard of the present invention for easy stowing;

fig. 5 is a schematic structural view of a bottom support device of the wing protection device of the unmanned aerial vehicle, which is convenient to store;

fig. 6 is a profile view of a first support column of the unmanned aerial vehicle wing protection device convenient to store.

In the figure: 1. a wing connection post; 2. a top shield; 3. a lateral protective cover; 4. a top mounting post; 5. a quick release connecting mechanism; 501. locking the mounting seat; 502. a fixed seat; 503. pulling a rod; 504. a limiting block; 505. a return spring; 506. a fastening pin; 507. a fastening groove; 6. a first support rod; 7. a second support rod; 8. an annular barrier strip; 9. a transverse barrier strip; 10. a vertical barrier strip; 11. a bottom support means; 1101. a linking seat; 1102. a supporting seat; 1103. a first support column; 1104. a connecting shaft; 1105. a second support column; 1106. a joining block; 1107. a tension spring; 12. a connecting seat.

Detailed Description

In order to make the technical means, the creation characteristics, the achievement purposes and the effects of the invention easy to understand, the invention is further described with the specific embodiments.

In the description of the present invention, it should be noted that the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", and the like indicate orientations or positional relationships based on those shown in the drawings, and are only for convenience of description and simplicity of description, but do not indicate or imply that the referred device or element must have a specific orientation, be constructed in a specific orientation, and be operated, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first" and "second" are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "mounted," "disposed," "connected," and the like are to be construed broadly, such as "connected," which may be fixedly connected, detachably connected, or integrally connected; can be mechanically or electrically connected; they may be connected directly or indirectly through intervening media, or they may be interconnected between two elements. The specific meanings of the above terms in the present invention can be understood in specific cases to those skilled in the art.

As shown in fig. 1-6, an unmanned aerial vehicle wing protection device convenient for storage comprises a wing connection column 1, a top protection cover 2 is connected to the top of the wing connection column 1, a lateral protection cover 3 is arranged on the outer side of the wing connection column 1, a top mounting column 4 is connected to the top end of the wing connection column 1, a quick-release connection mechanism 5 is connected between the top mounting column 4 and the top protection cover 2, the quick-release connection mechanism 5 is composed of a locking mounting seat 501, a fixing seat 502, a pulling rod 503, a limiting block 504, a reset spring 505, a fastening pin 506 and a fastening groove 507, a first support rod 6 and a second support rod 7 are fixedly mounted on the top of the top protection cover 2, a plurality of annular barrier strips 8 are supported on the upper surfaces of the first support rod 6 and the second support rod 7, a transverse barrier strip 9 is horizontally connected to the inner side of the lateral protection cover 3, and a vertical, the bottom of the lateral protective cover 3 is connected with a bottom supporting device 11, the bottom supporting device 11 is composed of a connecting seat 1101, a supporting seat 1102, a first supporting column 1103, a connecting shaft 1104, a second supporting column 1105, a connecting block 1106 and a telescopic spring 1107, and a connecting seat 12 is fixedly arranged on the outer surface of the wing connecting column 1 close to the middle position;

the locking mounting seat 501 is fixedly mounted on the upper surface of the top protection cover 2, the fixing seat 502 is fixedly mounted on the outer surface of the locking mounting seat 501, the fixing seats 502 are symmetrically distributed at two sides of the locking mounting seat 501, the pulling rod 503 penetrates through the inside of the fixing seat 502, the limiting block 504 is fixed at one end of the pulling rod 503, the limiting block 504 is embedded in the fixing seat 502, one end of the return spring 505 is fixed on the outer surface of the limiting block 504, the other end of the return spring 505 is fixed on the inner wall of the fixing seat 502, the return spring 505 is sleeved on the outer surface of the pulling rod 503, one end of the fastening pin 506 is fixed on the outer surface of the limiting block 504, the other end of the fastening pin 506 is embedded in the top mounting column 4, and the fastening; the fastening pin 506 is movably connected with the locking mounting seat 501 and the fixed seat 502 through a limiting block 504, a pulling rod 503 and a return spring 505, and the outer surface of the fastening pin 506 is tangent with the inner surface of the fastening groove 507; a fixing piece is connected between the top mounting column 4 and the wing connecting column 1, and the fixing piece can increase the connection stability between the top mounting column 4 and the wing connecting column 1; the first support rod 6 and the second support rod 7 are perpendicular to each other, fixing pins are arranged between the first support rod 6 and the second support rod 7 and the annular barrier strip 8, the fixing pins are used for fixing the first support rod 6 and the second support rod 7 with the annular barrier strip 8, and the radius of the top protective cover 2 is larger than that of the annular barrier strip 8; the connecting seat 1101 is fixedly installed at the bottom of the lateral protective cover 3, the supporting seat 1102 is fixedly installed at the bottom of the wing connecting post 1, the end of the first supporting post 1103 is arranged on the inner side of the connecting seat 1101, the connecting shaft 1104 penetrates through the connecting seat 1101 and the inside of the first supporting post 1103, one end of the second supporting post 1105 extends into the inside of the first supporting post 1103, the other end of the second supporting post 1105 extends into the inside of the supporting seat 1102, the connecting block 1106 is fixed at one end of the second supporting post 1105, the connecting block 1106 is embedded in the inside of the first supporting post 1103, one end of the expansion spring 1107 is fixed on the outer surface of the connecting block 1106, and the other end of the expansion spring 1107 is fixed on the inner surface of the first supporting post 1103; the first supporting column 1103 is movably connected with the connecting seat 1101 through a connecting shaft 1104, connecting holes matched with the connecting shaft 1104 are formed in the connecting seat 1101 and the first supporting column 1103, an anti-falling shaft sleeve is connected between the connecting shaft 1104 and the connecting seat 1101, the connecting holes are used for the connecting shaft 1104 to pass through, and the anti-falling bearing can prevent the connecting shaft 1104 and the connecting seat 1101 from falling off; the second support column 1105 is movably connected with the first support column 1103 through a connecting block 1106 and a telescopic spring 1107; a fixing notch matched with the second support column 1105 is formed in the supporting seat 1102, an anti-slip pad is bonded in the fixing notch through an adhesive, the fixing notch is used for the second support column 1105 to be embedded in, and the anti-slip pad can increase the friction force between contact surfaces and plays a role in anti-slip; the top shield 2 and the side shield 3 are connected in an integrated manner.

The invention is an unmanned aerial vehicle wing protection device convenient to store, when in use, a top protection cover 2 and a lateral protection cover 3 form a main body part of the whole unmanned aerial vehicle wing protection device convenient to store, a first support rod 6, a second support rod 7 and an annular barrier strip 8 support and fix the top protection cover 2, a transverse barrier strip 9 and a vertical barrier strip 10 support and fix the lateral protection cover 3, the top protection cover 2 and the lateral protection cover 3 are taken to the top of a wing connecting column 1, a top mounting column 4 penetrates through the inside of a locking mounting seat 501, a pulling rod 503 is pulled outwards, a fastening pin 506 moves oppositely to the locking mounting seat 501 and a fixing seat 502 through a limiting block 504, the pulling rod 503 and a reset spring 505, the fastening pin 506 is aligned to a fastening groove 507 on the outer surface of the top mounting column 4, the pulling rod 503 is loosened, and the fastening pin 506 passes through the limiting block 504, The pulling rod 503 and the return spring 505 move relative to the locking mounting seat 501 and the fixed seat 502, the fastening pin 506 is embedded into the fastening groove 507, the top protective cover 2 and the lateral protective cover 3 can be mounted with the wing connecting column 1 and the top mounting column 4, the second supporting column 1105 is rotated, the first supporting column 1103 moves relative to the linking seat 1101 through the connecting shaft 1104, when the first supporting column 1103 and the second supporting column 1105 are horizontal, the rotation is stopped, the end of the second supporting column 1105 is pressed, the second supporting column 1105 retracts into the first supporting column 1103, the second supporting column 1105 is loosened again, the second supporting column 1105 moves relative to the first supporting column 1103 through the linking block 1106 and the expansion spring 1107, the second supporting column 1105 is embedded into the fixed notch in the supporting seat 1102, the linking seat 1101, the supporting seat 1102, the first supporting column 1103, the connecting shaft, the second supporting column 1105, the linking block 1106 and the expansion spring 1107, and the bottom supporting device 11 composed of the wing protective device and the wing connecting column 1 can move relative to each other The support is carried out, so that the stability of the wing protection device after installation can be improved, the wing protection device is prevented from falling off after installation, the anti-slip mat can increase the friction force between contact surfaces, and the anti-slip effect is achieved, when the wing protection device needs to be disassembled, the second support column 1105 is pulled out, the second support column 1105 is relatively movably retracted with the first support column 1103 through the connecting block 1106 and the expansion spring 1107, the second support column 1105 is separated from the support seat 1102, the bottom support device 11 is disassembled with the wing connecting column 1, the pulling rod 503 is pulled, the fastening pin 506 is relatively movable with the locking mounting seat 501 and the fixing seat 502 through the limiting block 504, the pulling rod 503 and the reset spring 505, the fastening pin 506 is separated from the top mounting column 4, the top protection cover 2 and the lateral protection cover 3 are lifted, and the top protection cover 2 and the lateral protection cover 3 can be disassembled from the top mounting column 4, thereby can conveniently accomodate wing protector, improve wing protector's practicality, connecting seat 12 is used for the connection of wing, and top protection casing 2 and side direction protection casing 3 are the fretwork form and can avoid causing the influence to the work of wing.

The foregoing shows and describes the general principles and broad features of the present invention and advantages thereof. It will be understood by those skilled in the art that the present invention is not limited to the embodiments described above, which are described in the specification and illustrated only to illustrate the principle of the present invention, but that various changes and modifications may be made therein without departing from the spirit and scope of the present invention, which fall within the scope of the invention as claimed. The scope of the invention is defined by the appended claims and equivalents thereof.