TWI640455B - Flying device - Google Patents

Abstract

The invention relates to a flying vehicle. The flying vehicle includes a flying body and at least one joint assembly. The flight body is provided with at least one connecting unit for positioning a box body and a pipeline unit. Each of the connector assemblies is provided with a plug assembly and a body assembly. The plug assembly is selectively inserted into the base assembly, and one of the plug assembly and the base assembly is disposed in the cabinet and connected The inside of the box is provided on the flight body and communicates with the pipe unit. Wherein, when the box is coupled to the flying body, the plug component is inserted into the seat assembly, and the inside of the box communicates with the pipeline unit through the joint assembly.

Description

Flying vehicle

The invention relates to a flying vehicle.

With the advancement of technology, remote-controlled aircraft has also made major breakthroughs. In addition to improving its flight stability, handling and structural strength, it has added different functions to various fields. For example, the recent film--seeing Taiwan, is to design a remote-controlled aircraft as an aerial camera, from the bird's point of view to look down at the world, to provide a visual effect different from the general photography, and to be loved by the general public, and then pick up one The boom in the stock market.

Understandably, the function of the remote control aircraft can be used not only for the aerial photography, but also for the needs of various industries. For example, when the traditional farmers are spraying pesticides, they are carrying the medicine barrels and walking in the fields, such as Taiwan. The patent M500457 is. However, this type of spraying causes the user to constantly inhale the pesticide during the spraying process, causing physical damage; and the spraying method is inefficient, the spraying time is long, and the medicine cannot be evenly distributed in the field, and there is Need to improve the shortcomings.

Therefore, some operators have developed another type of flying sprinkler device in combination with remote-controlled aircraft and pesticides, and solved the above problems by means of remote remote-controlled flight sprinkling, such as Chinese patent CN10349446.

In this patent, referring to Figures 3 and 4, paragraph [0011-0017], the medicine box (21) is first fixed to the landing gear (13), and then the landing gear is fastened by fasteners (2, 6, 1). (13) Fixed to the bottom of the fuselage (12). Next, the medicine pump (26) is used to communicate the medicine feeding tube (27) extending into the chamber of the medicine box (21), and then the medicine pump (26) is activated to take the pesticide in the medicine box (21), so that the pesticide can be transported through The nozzle (25) delivered to the medicine rod (24) is sprinkled.

In other words, the technical features of this patent are divided into two separately operated locking systems and spraying systems. The user needs to lock the fixed landing gear first, and then start the medicine pump to connect the medicine box with the medicine rod for pesticide spraying. The whole structure is too complicated, the parts are numerous and the operation steps are numerous.

Therefore, it is necessary to provide a novel and progressive flight vehicle to solve the above problems.

The main object of the present invention is to provide a flying vehicle that can load at least one box, and the contents of the box can be replaced according to requirements (eg, medicine, gasoline); and a joint assembly is designed to enable the user to Quickly connect the interior of the cabinet to the piping of the flight vehicle.

To achieve the above object, the present invention provides a flying vehicle comprising a flying body and at least one joint assembly. The flight body is provided with at least one connecting unit for positioning a box body and a pipeline unit. Each of the connector assemblies is provided with a plug assembly and a body assembly. The plug assembly is selectively inserted into the base assembly, and one of the plug assembly and the base assembly is disposed in the cabinet and connected The inside of the box is provided on the flight body and communicates with the pipe unit. Wherein, when the box is combined and positioned on the flying body, the plug assembly is inserted into the seat assembly, and the inside of the box directly communicates with the pipeline unit through the joint assembly.

The following is a description of the possible embodiments of the present invention, and is not intended to limit the scope of the invention as claimed.

Referring to Figures 1 through 9, there is shown a preferred embodiment of the present invention. The flight carrier of the present invention includes a flight body 1 and at least one connector assembly 3.

The flight body 1 is provided with at least one connecting unit 11 for positioning a box A and a pipe unit 12. Each of the connector assemblies 3 is provided with a plug assembly 4 and a body assembly 5. The plug assembly 4 is selectively inserted into the base assembly 5, and one of the plug assembly 4 and the base assembly 5 is provided. It is provided in the casing A and communicates with the inside of the casing A, and the other is installed in the flight body 1 and communicates with the pipeline unit 12. When the box A is coupled to the flying body 1 , the plug assembly 4 is inserted into the base assembly 5 , and the inside of the box A directly communicates with the pipe unit 12 through the joint assembly 3 .

In more detail, the plug assembly 4 is disposed on the housing A, and the base assembly 5 is disposed on the flight body 1. Each of the connecting units 11 includes a sliding assembly 111 and a base 113. The seat 113 is for receiving and fixing the box A. Preferably, the base 113 is slidably inserted into the sliding assembly 111 to achieve rapid assembly.

It is to be emphasized that since the plug assembly 4 is kept in communication with the cabinet A, the base assembly 5 is kept in communication with the duct unit 12, so that the plug assembly 4 is inserted into the base assembly 5, The inside of the box A can directly communicate with the pipe unit 12, and the liquid in the box A can be immediately flowed into the pipe unit 12 without being assisted by other sputum units (such as pumps). Connected. Moreover, once the docking assembly 4 is inserted into the seat assembly 5, the cabinet A is simultaneously positioned on the flying body 1. In other words, the user can complete two different mechanisms of the lock fixing position and the connection at the same time in one operation, so that the other locking elements are not required to be positioned for positioning, and no other sputum unit is required to be actuated, so that the entire flight body 1 is The structure is simple, the operation is intuitive and convenient.

In this embodiment, the pedestal 113 is a rectangular frame body, and the pedestal 113 is provided with two spaced-apart support plates 114 for supporting the cabinet A, and the plug-in assembly 4 is interposed Between the two support plates 114. Wherein, considering the flight stability, the number of the at least one connecting unit 11 is two, and the two connecting units 11 are symmetrically disposed; and considering the balance of the combination of the respective boxes A, the sliding assembly 111 is preferably There are four slide members 112, which are disposed on opposite sides of the flight body 1 in two groups. In addition, each of the slide members 112 can also be provided with a limiting slot 115. The base 113 is provided with at least one sliding protrusion 116 that can slide on the limiting slot 115, thereby improving the base 113 and each of the sliding guides. The degree of integration of the pieces 112 is also indispensable.

In more detail, each of the slide members 112 is provided with at least one first fixing portion 71. The base 113 is provided with at least one second fixing portion 72, and the first fixing portion 71 is coupled to the second fixing portion 72. The fixing is combined, thereby preventing unintended factors from causing the susceptor 113 to be detached from the sliding assembly 111. For example, but not limited to, the first fixing portion 71 is a block, and the second fixing portion 72 is a hole that is disposed in the base 113. The first and second fixing portions 71, 72 are fixed to each other. .

It is worth mentioning that the pipeline unit 12 can be the oil pipeline of the flight body 1. At this time, as long as the oil body is built in each of the cabinets A, each of the cabinets A can be regarded as a backup. The oil sump allows the flight to carry more fuel to effectively extend flight time. Alternatively, the flight body 1 is further provided with a spray assembly 6, the spray assembly 6 is provided with the pipeline unit 12, and each of the tanks A is provided with a medicament, and at this time, the flight carrier can be sprayed with pesticides. Therefore, the operator can control at a remote place without the risk of inhaling a large amount of medicine; and the medicine can be sprayed from above the farmland to be evenly distributed and the spray area is wider, and the medicament can be fully and efficiently used, thereby reducing The amount used. Of course, the load of each of the cases A is not limited to a fluid, and may be other object types such as a small solid.

The structure of the joint assembly 3 is further described. The plug assembly 4 is provided with a body 41, a stop member 42 and a rod member 43 disposed on the box body A. a passage 45 communicating with the inside of the box A, the blocking member 42 selectively blocking the passage 45 from communicating with the inside of the box A, the rod member 43 connecting the blocking member 42 and movably inserted in the passage 45. The base assembly 5 is provided with a body 51 and a top member 52. The base body 51 is provided with a joint portion 511 and an inner space 513. The inner space 513 communicates with the pipeline unit 12, and the top member 52 is accommodated therein. Internal space 513. When the box A is coupled to the flying body 1 , the body 41 is inserted and positioned on the joint portion 511 , the passage 45 communicates with the inner space 513 , and the top member 52 abuts the rod member 43 . The stop 42 is not blocked by the stop 42.

Further, the plug assembly 4 is further provided with a first elastic member 91. The first elastic member 91 connects the body 41 and the rod member 43 such that the blocking member 42 normally blocks the passage 45 from communicating with the box. The inside of body A. The base member 5 is further provided with a second elastic member 92. The top member 52 is movably disposed in the inner space 513. The joint portion 511 is provided with an opening 512 for external communication with the inner space 513. The elastic member 92 connects the seat body 51 and the top member 52 such that the top member 52 normally closes the opening 512. Only when the case A is coupled to the flight body 1 , the body 41 extends from the opening 512 into the inner space 513 and presses against the top piece 52 to a predetermined position, so that the top piece 52 does not close the opening. 512, at the same time, the stop 42 is not blocked by the passage 45. The two-way linkage opening and closing structure design ensures that the joint assembly 3 can only be connected when the box A is combined and positioned on the flight body 1, and can effectively prevent the object of the box A from moving to the outside without being noticed, and blocking the The pipeline unit 12 communicates with the outside world to prevent impurities from entering the pipeline unit 12 or the occurrence of bad volatiles (such as oil and chemicals), thereby ensuring better safety in use.

In the present embodiment, the blocking member 42 is a cover member that is disposed on the body 41. For quick assembly, the body 41 is further provided with a screwing portion 411 for screwing to the housing A, and a The mounting portion 412 of the channel 45 is disposed with a mounting hole 413 and a plurality of through holes 414. The rod member 43 passes through the mounting hole 413. The first elastic member 91 is sleeved on the rod member. The one end of the first elastic member 91 is connected to the mounting portion 412, and the other end of the first elastic member 91 is connected to a locking member 44. The locking member 44 is movably screwed to the rod member 43. The base member 5 is further provided with a limiting member 53 and a supporting member 54 . The limiting member 53 is fixed to the seat body 51 , and the second elastic member 92 is sleeved on the limiting member 53 . The supporting member 54 is further disposed on the limiting member 53 . One end is connected to the top piece 52, and the other end of the support member 54 is movably inserted into the limiting member 53 and the seat body 51. When the box A is combined and positioned on the flying body 1, the limit is The piece 53 is moved to the predetermined position to abut the top piece 52.

Preferably, the plug assembly 4 is further provided with at least one first stop member 81. Each of the first stop members 81 is disposed on the body 41. When the box A is coupled to the flight body 1, each The first leakage preventing member 81 is interposed between the joint portion 511 and the body 41, and can effectively prevent an object (such as a fluid) from running from the gap to the outside. Moreover, the main body 41 and the joint portion 511 can be tightly coupled and coupled through the first stop member 81, and a preferred combination is obtained.

It is to be noted that the body 41 is further provided with at least one through hole 415 which communicates with the passage 45. The top piece 52 is provided with a head portion 521 and a body portion 522. When the box body A is combined and positioned on the flight body 1 The head portion 521 extends into the channel 45 to abut the rod member 43 . The body portion 522 abuts the body 41 , and the passage 45 communicates with the inner space 513 through the through holes 415 . More specifically, the top member 52 is further provided with a bottom portion 523, and a second stop member 82 is sleeved on the body portion 522. When the body portion 41 is not inserted into the joint portion 511, the second stop leaking The member 82 is interposed between the joint portion 511 and the bottom portion 523 to improve the degree of sealing. More specifically, the top member 52 is substantially "convex" in view of the direction in which the plug assembly 4 is perpendicular to the mating direction of the base assembly 5.

In summary, the flying carrier of the present invention can quickly assemble the box body and fill different objects in the box according to different requirements. If the aircraft is to be flying for a long time, the fuel is installed in the box body; if the spraying operation is to be carried out, the space can be placed. The medicine is in the box.

Moreover, the joint component is normally in a closed state, which can prevent the object in the box from moving to the outside, and can prevent the foreign matter from entering the pipeline unit or avoid the leakage of the bad volatiles of the pipeline unit, only when the cabinet is combined and positioned. When the flying body is inserted into the flying body, the plug assembly can be opened in both directions at the same time, and a better and safe use mechanism can be obtained.

<TABLE border="1" borderColor="#000000" width="85%"><TBODY><tr><td> 1: Flight body 11: Connection unit 111: Sliding assembly 112: Slide member 113: Base Seat 114: support plate 115: limit groove 116: slide 12: pipe unit 3: joint assembly 4: plug assembly 41: body 411: screw portion 412: mounting portion 413: mounting hole 414: through hole 415 :through hole 42: stopper 43: rod 44: lock piece </td><td> 45: channel 5: seat body assembly 51: seat body 511: joint portion 512: opening 513: inner space 52: top piece 521 : Head 522: Body 523: Bottom 53: Limiting member 54: Supporting member 6: Spraying assembly 71: First fixing portion 72: Second fixing portion 81: First stopping member 82: Second stopping member 91 : first elastic member 92: second elastic member A: cabinet </td></tr></TBODY></TABLE>

1 is a perspective view of a preferred embodiment of the present invention. Figure 2 is a partial exploded view of Figure 1. Figure 3 is a side cross-sectional view of Figure 1. Figure 4 is an enlarged partial cross-sectional view of Figure 3. Figure 5 is another partial cross-sectional enlarged view of Figure 3. Figure 6 shows a joint assembly in accordance with a preferred embodiment of the present invention. Figure 7 is an exploded view of Figure 6. 8 and 9 are cross-sectional views of a joint assembly in accordance with a preferred embodiment of the present invention.

Claims (6)

A flying vehicle includes: a flying body, at least one connecting unit for positioning a box body and a pipeline unit; at least one joint assembly each having a plug assembly and a body assembly, the plug assembly being selected The socket assembly is connected to the housing and is connected to the interior of the cabinet. The base assembly is disposed on the flight body and communicates with the pipeline unit. There is a body, a stopper and a rod disposed on the box, the body enclosing a passage for communicating with the inside of the box, the blocking member selectively blocking the passage to communicate with the box Internally, the rod member is connected to the blocking member and movably inserted into the passage. The seat assembly is provided with a body and a top member. The base body is provided with a joint portion and an inner space, and the inner space communicates with the tube. The splicing component is inserted into the pedestal assembly, and the body is inserted and positioned at the joint portion. The passage communicates with the inner space, and the top piece abuts the The stopper member so that the channel is not blocked, and further through the interior of the housing of the joint assembly of the pipe unit and the direct communication. The flight vehicle of claim 1, wherein the flight body is further provided with a spray assembly, the spray assembly being provided with the pipeline unit. The flight carrier of claim 1, wherein the plug assembly is further provided with at least one first stop member, each of the first stop members being disposed on the body; wherein when the case is coupled to the flight In the body, each of the first stop members sandwiches the joint portion and the body. The flight carrier of claim 1, wherein the plug assembly is further provided with a first elastic member, the first elastic member connecting the body and the rod, so that the blocking member normally blocks the passage from communicating with the box. The inside of the body is further provided with a second elastic member, the top member is movably disposed in the inner space, the joint portion is provided with an opening for external communication of the inner space, and the second elastic member is connected to the inner portion The seat body and the top piece, the top piece is normally closed to the opening; wherein, when the box body is coupled to the flying body, the body extends from the opening into the inner space to press the top piece to a predetermined position So that the top piece does not close the opening, and at the same time, the blocking member does not block the passage. The flight vehicle of claim 4, wherein the body is further provided with at least one through hole communicating with the passage, the top member is provided with a head portion and a body portion; wherein when the box body is coupled to the flight body The head portion extends into the passage to abut the rod member, and the body abuts against the body, and the passage communicates with the inner space by each of the through holes. The flight vehicle of claim 5, wherein the number of the at least one connecting unit is two, the two connecting units are symmetrically disposed; the flying body is further provided with a spraying assembly, and the spraying unit is provided with the pipeline unit The plug assembly is further provided with at least one first leak stop member, wherein each of the first leak stop members is disposed on the body; wherein, when the box body is coupled to the flight body, each of the first leak stop members The top member is further provided with a bottom portion, and a second leakage preventing member is sleeved on the body portion, and the second stop leaking when the body is not inserted into the joint portion The component is located between the joint portion and the bottom portion; the top member is substantially convex when viewed from the direction of insertion of the socket assembly and the base assembly; the seat assembly is further provided with a limit a positional member and a supporting member, the limiting member is fixed to the seat body, the second elastic member is sleeved on the limiting member, and one end of the supporting member is assembled to the top member, and the other end of the supporting member is Movably inserted in the limiting member and the seat body, when the box body is combined and positioned on the flying body, the limiting member moves to the Retaining the top member; the member is a cover member that is disposed on the body; the body is further provided with a screwing portion for screwing the box body, and a mounting portion of the channel. The mounting portion is provided with a mounting hole and a plurality of through holes, the rod member is disposed through the mounting hole, the first elastic member is sleeved on the rod member, and one end of the first elastic member is connected to the mounting portion, The other end of the first elastic member is connected to a lock member, and the lock member is movably screwed to the rod member; the body and the joint portion are in a tight fit relationship.