Luggage support device and unmanned luggage transporter

Abstract

To prevent or suppress falling of a cargo during flight.SOLUTION: A cargo support device 14 includes a plate 20, a ground part 18 which is grounded on a landing surface in a landed state, leg parts 22 for supporting a cargo 30, a drive part 40 for moving the leg parts 22, and a restriction part 50 for restricting operation of the drive part 40. The drive part 40 is operated in a first state to move the leg parts 22 to the cargo 30 side, and is operated in a second state to move the leg parts 22 to an opposite side to the cargo 30. The restriction part 50 is provided independently of the drive part 40, permits the operation of the drive part 40 in a state where the ground part 18 is grounded on the landing surface, and restricts the operation in at least the second state of the drive part 40 in a state where the ground part 18 is separated from the landing surface.SELECTED DRAWING: Figure 20

Description

[Technical field]

[0001] The present invention relates to a luggage support device and an unmanned luggage transport vehicle. [Background technology]

[0002] The following Patent Document 1 discloses a transport device that supports a container or the like at the bottom of a small unmanned aerial vehicle and transports the container or the like. [Prior art documents] [Patent documents]

[0003] [Patent Document 1] International Publication No. 2020 / 194533 Summary of the Invention [Problem to be solved by the invention]

[0004] Incidentally, in a transport device that transports luggage by flying, such as the transport device described in the above Patent Document 1, it is desirable to be able to prevent or suppress the luggage from falling during flight.

[0005] In consideration of the above, an object of the present invention is to provide a luggage support device and an unmanned luggage transport vehicle that can prevent or suppress the dropping of luggage during flight. [Means for solving the problem]

[0006] The first embodiment of the luggage support device comprises a base on which a small unmanned aerial vehicle is attached, a ground contact part that contacts the landing surface when landing, a luggage support part provided on the lower side of the base and supports luggage, a drive part that operates in a first state to move the luggage support part toward the luggage side and operates in a second state to move the luggage support part away from the luggage, and a limiting part that is provided independently of the drive part and allows operation of the drive part when the ground contact part is in contact with the landing surface and limits operation of the drive part in at least the second state when the ground contact part is separated from the landing surface.

[0007] According to the luggage support device of the first aspect, when the ground contact portion is in contact with the landing surface, if the drive unit operates in the first state, the luggage support portion moves toward the luggage side. This allows the luggage to be supported by the luggage support portion. Also, when the ground contact portion is in contact with the landing surface, if the drive unit operates in the second state, the luggage support portion moves to the opposite side of the luggage. This allows the luggage to be separated from the luggage support portion. Here, when the ground contact portion is in contact with the landing surface, the limiting unit allows the drive unit to operate. On the other hand, when the ground contact portion is separated from the landing surface, the limiting unit limits the operation of the drive unit in at least the second state. This prevents or suppresses the luggage support portion from moving to the opposite side of the luggage when the ground contact portion is separated from the landing surface. As a result, it is possible to prevent or suppress the luggage from falling during flight.

[0008] The second aspect of the luggage support device is the luggage support device of the first aspect, wherein the limiting portion includes a drive unit side limiting portion that is displaceable between a first position that limits the operation of the drive unit in at least the second state and a second position that allows the operation of the drive unit, a ground contact portion that is provided on the ground contact portion, and a connection portion that connects the drive unit side limiting portion and the ground contact portion side limiting portion, wherein when the ground contact portion side limiting portion touches the landing surface, the connection portion is displaced and the drive unit side limiting portion is displaced from the first position to the second position, and when the ground contact portion side limiting portion moves away from the landing surface, the connection portion is displaced and the drive unit side limiting portion is displaced from the second position to the first position.

[0009] According to the luggage support device of the second aspect, when the ground contact portion side limiting portion touches the landing surface, the connection portion is displaced and the drive portion side limiting portion is displaced from the first position to the second position. When the drive portion side limiting portion is in the second position, the limiting portion allows the drive portion to operate. In contrast, when the ground contact portion side limiting portion moves away from the landing surface, the connection portion is displaced and the drive portion side limiting portion is displaced from the second position to the first position. When the drive portion side limiting portion is in the first position, the limiting portion limits the operation of the drive portion in at least the second state. This makes it possible to prevent or suppress the luggage from falling during flight.

[0010] A third aspect of the luggage support device is the luggage support device of the second aspect, further comprising a biasing member that constantly biases the drive unit side limiting portion toward the first position.

[0011] According to the luggage support device of the third aspect, the drive unit side limiting portion is constantly biased toward the first position by the biasing member, so that, for example, even if the ground contact unit side limiting portion or the connection portion malfunctions, it is possible to prevent or suppress the luggage from falling during flight.

[0012] A fourth aspect of the luggage support device is the luggage support device of the second aspect, wherein the drive unit side limiting portion is provided with a pressing portion that is pressed against a member that constitutes the drive unit when the drive unit is located in the first position, and the operation of the drive unit is restricted by the pressing portion being pressed against the member that constitutes the drive unit.

[0013] According to the luggage support device of the fourth aspect, the pressing portion of the drive unit side limiting portion is pressed against the member that constitutes the drive unit, thereby making it possible to limit the operation of the drive unit.

[0014] A fifth aspect of the luggage support device is the luggage support device of the second aspect, wherein the drive unit side limiting portion has a first ratchet tooth protruding toward the drive unit side, and the drive unit has a second ratchet tooth protruding toward the drive unit side limiting portion and meshing with the first ratchet tooth of the drive unit side limiting portion located at the first position, and when the first ratchet tooth and the second ratchet tooth are meshed, operation of the drive unit in the second state is restricted, and when the drive unit operates in the first state with the first ratchet tooth and the second ratchet tooth meshed, the second ratchet tooth overcomes the first ratchet tooth, thereby allowing operation of the drive unit in the first state.

[0015] According to the luggage support device of the fifth aspect, the operation of the drive unit in the second state can be restricted by meshing the first ratchet teeth of the drive unit side limiting portion with the second ratchet teeth of the drive unit. Also, even if the first ratchet teeth of the drive unit side limiting portion and the second ratchet teeth of the drive unit are meshed, the operation of the drive unit in the first state can be permitted.

[0016] A sixth aspect of the luggage support device is a luggage support device of the second aspect, wherein the drive unit side limiting portion comprises a fixed cam portion that is immovable relative to the base, a movable cam portion that is connected to the connection portion and displaceable relative to the base, and an insertion portion that protrudes from the drive unit and is inserted into the fixed cam portion and the movable cam portion, and when the movable cam portion is positioned at a position where the movement of the insertion portion is restricted by both the fixed cam portion and the movable cam portion, operation of the drive unit is restricted, and when the movable cam portion is positioned at a position where the insertion portion can move along both the fixed cam portion and the movable cam portion, operation of the drive unit is permitted.

[0017] According to the luggage support device of the sixth aspect, the operation of the drive unit can be restricted by arranging the movable cam portion in a position where the movement of the insertion portion of the drive unit is restricted by both the fixed cam portion and the movable cam portion. On the other hand, the operation of the drive unit can be permitted by arranging the movable cam portion in a position where the insertion portion of the drive unit can move along both the fixed cam portion and the movable cam portion.

[0018] The seventh aspect of the unmanned luggage transporter comprises a small unmanned aerial vehicle, a base to which the small unmanned aerial vehicle is attached, a grounding section that contacts the landing surface when landed, a luggage support section provided on the lower side of the base and supports luggage, a drive section that operates in a first state to move the luggage support section toward the luggage side and operates in a second state to move the luggage support section to the opposite side to the luggage, and a limiting section that is provided independently of the drive section and allows operation of the drive section when the grounding section is in contact with the landing surface and limits operation of the drive section in at least the second state when the grounding section is separated from the landing surface.

[0019] According to the unmanned baggage transporter of the seventh aspect, the small unmanned aerial vehicle flies, thereby transporting the supported baggage. Also, according to the unmanned baggage transporter of the seventh aspect, when the ground contact portion is in contact with the landing surface, if the drive unit operates in the first state, the baggage support portion moves toward the baggage side. This allows the baggage to be supported by the baggage support portion. Also, when the ground contact portion is in contact with the landing surface, if the drive unit operates in the second state, the baggage support portion moves to the opposite side of the baggage. This allows the baggage to be separated from the baggage support portion. Here, when the ground contact portion is in contact with the landing surface, the limiting unit allows the drive unit to operate. On the other hand, when the ground contact portion is separated from the landing surface, the limiting unit limits the operation of the drive unit in at least the second state. This prevents or suppresses the baggage support portion from moving to the opposite side of the baggage when the ground contact portion is separated from the landing surface. As a result, it is possible to prevent or suppress the baggage from falling during flight. Effect of the Invention

[0020] The luggage support device and unmanned luggage transport vehicle according to the present invention have the excellent effect of preventing or suppressing the dropping of luggage during flight. [Brief description of the drawings]

[0021] [Figure 1] FIG. 2 is a perspective view showing an unmanned luggage transport vehicle. [Diagram 2] FIG. 2 is a perspective view showing the unmanned luggage transport vehicle, illustrating a state in which the luggage support device is supporting luggage. [Diagram 3] FIG. [Figure 4] 2 is a plan view of the luggage support device as seen from above, with the plate not shown. FIG. [Diagram 5] 2 is a perspective view of the luggage support device from above, with the plate not shown. FIG. [Figure 6] FIG. 4 is an enlarged perspective view showing the vicinity of a rotation support portion. [Figure 7] 1 is a perspective view showing the luggage support device and luggage before each leg supports the luggage. FIG. [Figure 8] 1 is a plan view of the luggage support device and luggage viewed from above, with the plates not shown, showing the state before each leg supports the luggage. FIG. [Figure 9] FIG. 2 is a perspective view showing the luggage support device and luggage, with each leg supporting the luggage; [Figure 10] 1 is a plan view of the luggage support device and luggage viewed from above, with the plates not shown, showing the state in which each leg is supporting the luggage. FIG. [Figure 11] 2 is a bottom view of the luggage support device and luggage as viewed from below. FIG. [Figure 12] FIG. 12 is a bottom view corresponding to FIG. 11, in which luggage is not shown. [Figure 13] 12 is an enlarged perspective view showing the vicinity of a rotation support part in the state shown in FIG. 11. [Figure 14] 2 is a bottom view of the luggage support device and luggage as viewed from below. FIG. [Figure 15]FIG. 15 is a bottom view corresponding to FIG. 14, in which luggage is not shown. [Figure 16] 15 is an enlarged perspective view showing the vicinity of a rotation support part in the state shown in FIG. 14. [Figure 17] 1 is an enlarged side view showing a portion of the luggage support device where a ground-side limiting portion is provided, illustrating a state in which the unmanned luggage transport vehicle has landed. FIG. [Figure 18] 1 is an enlarged plan view showing a portion of the luggage support device where a drive unit side limiting unit is provided, illustrating a state in which the unmanned luggage transport vehicle has landed. FIG. [Figure 19] 1 is an enlarged side view showing a portion of the luggage support device where a ground-side limiting portion is provided, illustrating a state in which the unmanned luggage transport vehicle is flying. FIG. [Figure 20] 1 is an enlarged plan view showing a portion of the luggage support device where a drive unit side limiting unit is provided, illustrating a state in which the unmanned luggage transport vehicle is flying. FIG. [Figure 21] 13 is a plan view showing a schematic view of a limiting portion of another embodiment, in which the first ratchet tooth and the second ratchet tooth are spaced apart from each other. FIG. [Figure 22] 11 is a plan view showing a schematic view of a limiting portion of another embodiment, in which the first ratchet teeth and the second ratchet teeth are engaged with each other. FIG. [Diagram 23] 13 is a perspective view showing a restricting portion of another embodiment, in which the movement of the insertion portion is restricted by a fixed cam portion and a movable cam portion. FIG. [Figure 24] FIG. 13 is a perspective view showing a restricting portion of another embodiment, in which the insertion portion is movable along the fixed cam portion and the movable cam portion. [Diagram 25] FIG. 13 is a perspective view showing a restricting portion of another embodiment, in which the insertion portion is movable along the fixed cam portion and the movable cam portion. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0022] An unmanned baggage transport vehicle 10 according to an embodiment of the present invention will be described with reference to Figs. 1 to 6.

[0023] As shown in Figures 1 and 2, the unmanned baggage transport vehicle 10 of this embodiment is composed of a small unmanned aerial vehicle 12 and a baggage support device 14 attached below the small unmanned aerial vehicle 12.

[0024] As shown in FIG. 1, FIG. 3, FIG. 4 and FIG. 5, the luggage support device 14 includes an aircraft fixing part 16 to which the small unmanned aerial vehicle 12 is fixed, and a pair of grounding parts 18 that are grounded on the landing surface when the luggage support device 14 is landed. In this embodiment, six small unmanned aerial vehicles 12 are fixed to the aircraft fixing part 16. The pair of grounding parts 18 include a grounding part main body 18A that extends horizontally and is grounded on the landing surface, and a central leg part 18B that extends upward from the center of the longitudinal direction of the grounding part main body 18A. The upper end part of the central leg part 18B is connected to the lower part of the aircraft fixing part 16. The landing surface is a surface on which the unmanned luggage transporter 10 lands, and is the ground, a drone port, the roof of a vehicle, a loading platform, etc.

[0025] The luggage support device 14 also includes a plate 20 serving as a base that is disposed below the aircraft fixing part 16 and is connected to the aircraft fixing part 16. The luggage support device 14 also includes four legs 22 serving as luggage support parts, four linear guides 24 serving as first support parts, a link mechanism 26, and an actuator 28.

[0026] 3, the plate 20 is formed in a plate shape with the thickness direction being the up-down direction, and is generally rectangular when viewed from above with each side of the rectangle curved inward. Legs 22 are attached to the four corners of the plate 20.

[0027] The leg 22 includes two abutment parts 22A spaced apart in the horizontal direction, which is a direction perpendicular to the vertical direction, an upper connecting part 22B connecting the upper ends of the two abutment parts 22A in the horizontal direction, and a lower connecting part 22C connecting the lower ends of the two abutment parts 22A in the horizontal direction. The two abutment parts 22A are formed in a round bar shape with the vertical direction as the axial direction. The upper connecting part 22B is formed in a plate shape extending horizontally with the vertical direction as the thickness direction. The upper end of one of the abutment parts 22A is fixed to one end of the upper connecting part 22B, and the upper end of the other abutment part 22A is fixed to the other end of the upper connecting part 22B. The lower connecting part 22C is formed in a plate shape extending horizontally with the vertical direction as the thickness direction. A lower end of one of the contact portions 22A is fixed to one end of the lower connecting portion 22C, and a lower end of the other contact portion 22A is fixed to the other end of the lower connecting portion 22C. As shown in Fig. 2, the lower connecting portion 22C serves as a portion that supports the luggage 30 from below. The two contact portions 22A serve as portions that support the luggage 30 from the lateral sides. Each of the four legs 22 has the same configuration.

[0028] As shown in Figs. 3 and 4, the linear guide 24 is formed in a plate shape extending in the horizontal direction with the thickness direction being the up-down direction. The linear guide 24 is rectangular when viewed from above. The four linear guides 24 are fixed to the plate 20 in a state in which they are respectively disposed below the four corners of the plate 20. When viewed from above, one side of the longitudinal direction of each of the four linear guides 24 faces the center (centroid) of the plate 20. The four linear guides 24 support four legs 22 via slide parts 42 and rotation support parts 44, which will be described later. Each leg 22 is movable along each linear guide 24 from the corner of the plate 20 toward the center, and from the center of the plate 20 toward the corner.

[0029] The link mechanism 26 includes a central link 32 disposed below the center of the plate 20 as viewed from above, and four outer links 34 each connected to the central link 32. As shown in FIG. 4 and FIG. 5, the central link 32 includes a rotating part 32A supported on the plate 20 so as to be rotatable with the vertical direction as the axial direction, and four protruding arms 32B protruding from the rotating part 32A toward the outside in the rotational radial direction of the rotating part 32A. The four protruding arms 32B are arranged at intervals in the rotational circumferential direction of the rotating part 32A. One end of each of the four outer links 34 is connected to the end of each of the four protruding arms 32B on the opposite side to the rotating part 32A via a ball joint. The other end of each of the four outer links 34 is connected to four slide brackets 46 (described later) via a ball joint.

[0030] As shown in FIG. 5, the actuator 28 is, for example, a motor actuator in which an output shaft 28A rotates. The actuator 28 is fixed to the plate 20 (see FIG. 3) in a state in which it is disposed on the upper side of the plate 20. A first rod 36 is fixed to the output shaft 28A of the actuator 28. The first rod 36 is inserted through an opening formed in the plate 20. As a result, the end of the first rod 36 opposite the output shaft 28A is located on the lower side of the plate 20. In addition, one end of a second rod 38 is connected to the end of the first rod 36 opposite the output shaft 28A via a ball joint. Furthermore, the other end of the second rod 38 is connected to the protruding arm portion 32B of the central link 32 via a ball joint. As a result, the output shaft 28A of the actuator 28 and the central link 32 are connected to each other via the first rod 36 and the second rod 38. As a result, the central link 32 rotates in conjunction with the rotation of the output shaft 28A of the actuator 28. Here, the actuator 28, the first rod 36, the second rod 38, the central link 32 and the four outer links 34 constitute a drive unit 40 that moves each leg 22 towards the luggage 30 or away from the luggage 30.

[0031] As described above, the leg 22 is supported by the linear guide 24 via the slide portion 42, the rotation support portion 44, and the like. More specifically, as shown in FIG. 6, the leg 22 is supported by the linear guide 24 via the slide portion 42, the slide bracket 46, and the rotation support portion 44. The slide portion 42 is engaged with the linear guide 24. This slide portion 42 is adapted to slide (move) along the longitudinal direction of the linear guide 24. In addition, the slide bracket 46 is fixed to the lower portion of the slide portion 42. As shown in FIG. 5, the other end of the outer link 34 is connected to the end of the slide bracket 46 on the opposite side to the slide portion 42 via a ball joint. In addition, the rotation support portion 44 as a second support portion protrudes downward from the lower portion of the slide bracket 46. This rotation support portion 44 engages with the longitudinal center portion of the upper connecting portion 22B of the leg 22, so that the leg 22 is supported by the rotation support portion 44 so as to be rotatable about the vertical direction as the axial direction.

[0032] A rotation limiting spring 48 is provided between the upper connecting portion 22B of the leg 22 and the slide bracket 46 as a rotation limiting portion. The rotation limiting spring 48 is, for example, a torsion spring. The rotation support portion 44 is inserted into the rotation limiting spring 48. One end 48A of the rotation limiting spring 48 is engaged with a hole formed in the upper connecting portion 22B. The other end 48B of the rotation limiting spring 48 is engaged with a hole formed in the slide bracket 46. The deformation of the rotation limiting spring 48 allows the leg 22 to rotate about an axial direction extending in the vertical direction.

[0033] (Actions and Effects of the Present Embodiment) Next, the operation and effects of this embodiment will be described.

[0034] As shown in Figures 1 and 2, in the unmanned baggage transport vehicle 10 of this embodiment, the luggage support device 14 can support luggage 30 when the ground contact portion 18 is in contact with the landing surface (when the unmanned baggage transport vehicle 10 is landing).

[0035] 7 and 8, a load 30 having a rectangular parallelepiped shape is placed below the plate 20, and each leg 22 is separated from the load 30. In this state, each leg 22 is held in a position determined by a rotation limiting spring 48 (see FIG. 6). This makes it possible to limit unnecessary rotation of each leg 22 about the vertical direction as the axial direction when each leg 22 is not supporting the load 30. The position of each leg 22 with respect to each linear guide 24 when each leg 22 is not supporting the load 30 is referred to as the "standard position A1."

[0036] Here, the luggage 30 has a rectangular upper surface 30A and a lower surface 30B (see FIG. 11), and four side surfaces 30C that connect the upper surface 30A and the lower surface 30B in the vertical direction. Two of the four side surfaces 30C that have a smaller horizontal dimension are called first side surfaces 30C1, and two of the four side surfaces 30C that have a larger horizontal dimension than the horizontal dimension of the first side surface 30C1 are called second side surfaces 30C2. The luggage 30 shown in FIG. 7 to FIG. 11 is a standard aspect ratio luggage 30 in which the ratio of the horizontal dimension of the first side surface 30C1 to the horizontal dimension of the second side surface 30C2 (hereinafter referred to as the "aspect ratio") is set to a predetermined aspect ratio.

[0037] 5, when the output shaft 28A of the actuator 28 rotates to one side (the direction of the arrow C1), the central link 32 rotates to one side (the direction of the arrow C2), and the four outer links 34 pull the four slide brackets 46. As a result, each leg 22 moves toward the load 30. The operating state of the drive unit 40 caused by the output shaft 28A of the actuator 28 rotating to one side (the direction of the arrow C1) is referred to as the "operating state when supporting a load" as a first state.

[0038] As shown in Figures 9 and 10, when each leg 22 moves toward the luggage 30, the two contact portions 22A of each leg 22 contact the adjacent first side surface 30C1 and second side surface 30C2, respectively. Here, as shown in Figures 10, 11, 12, and 13, in the case of luggage 30 having a standard aspect ratio, each leg 22 is designed to hardly rotate from the standard posture A1. That is, in this embodiment, the standard posture A1 of each leg 22 is set according to luggage 30 having a standard aspect ratio. Note that the luggage 30 is not shown in Figures 12 and 13.

[0039] 9, 11, and 12, when the two contact portions 22A of each leg 22 contact the adjacent first side surface 30C1 and second side surface 30C2, respectively, the lower connecting portion 22C of each leg 22 is disposed along the lower surface 30B of the luggage 30. As a result, the four corner portions 30D of the luggage 30 are supported by each leg 22.

[0040] 2, when each small unmanned aerial vehicle 12 is operated, each small unmanned aerial vehicle 12 flies together with the luggage support device 14. This allows the luggage 30 supported by the luggage support device 14 to be transported by air.

[0041] When the unmanned baggage transport vehicle 10 has landed, as shown in FIG. 5, the output shaft 28A of the actuator 28 rotates to the other side (opposite the direction of the arrow C1), causing the central link 32 to rotate to the other side (opposite the direction of the arrow C2), and the four outer links 34 push the four slide brackets 46. This causes each leg 22 to move to the side opposite the baggage 30. As a result, the baggage 30 supported by each leg 22 can be lowered from the baggage support device 14. The operating state of the drive unit 40 caused by the output shaft 28A of the actuator 28 rotating to the other side (opposite the direction of the arrow C1) is referred to as the "operating state when lowering the baggage" as a second state.

[0042] 14 shows luggage 30 with a flat aspect ratio in which the horizontal dimension of first side surface 30C1 is smaller than the horizontal dimension of first side surface 30C1 of luggage 30 with a standard aspect ratio. The movement of each leg 22 when each leg 22 supports luggage 30 with a flat aspect ratio will be described below.

[0043] As shown in Figures 14, 15 and 16, when each leg 22 moves toward the luggage 30, first, one abutment portion 22A of the leg 22 abuts against the first side surface 30C1. When each leg 22 further moves toward the luggage 30 with one abutment portion 22A of the leg 22 abutting against the first side surface 30C1, each leg 22 rotates from the standard position A1 to one side (the direction of the arrow C3). When each leg 22 rotates from the standard position A1 to one side, the rotation limiting spring 48 (see Figure 6) is deformed. When each leg 22 rotates from the standard position A1 to one side, the other abutment portion 22A of the leg 22 abuts against the second side surface 30C2. When the two contact portions 22A of each leg 22 contact the adjacent first side surface 30C1 and second side surface 30C2, respectively, the lower connecting portion 22C of each leg 22 is disposed along the lower surface 30B of the luggage 30 with a flat aspect ratio. As a result, the four corner portions 30D of the luggage 30 with a flat aspect ratio are supported by each leg 22.

[0044] As described above, the luggage support device 14 of the unmanned luggage transport vehicle 10 of this embodiment can support luggage 30 of different sizes and shapes (aspect ratios).

[0045] Furthermore, when the legs 22 move away from the luggage 30 with a flat aspect ratio, with the four corner portions 30D of the luggage 30 being supported by the legs 22, the luggage 30 with a flat aspect ratio supported by the legs 22 is lowered from the luggage support device 14. At this time, the legs 22 are returned to the standard position A1 by the restoring force (biasing force) of the rotation limiting springs 48. In this manner, in this embodiment, when the legs 22 move away from the luggage 30, the legs 22 can be returned to the standard position A1.

[0046] In this embodiment, an example is described in which the rotation limiting spring 48 is used to suppress unnecessary rotation of each leg 22, but the invention is not limited to this. For example, unnecessary rotation of each leg 22 may be suppressed by providing a rotation limiting part that generates friction between the upper connecting part 22B of the leg 22 and the slide bracket 46.

[0047] (Configuration for preventing or suppressing the dropping of baggage during flight) Next, a configuration for preventing or suppressing the dropping of the baggage 30 while the unmanned baggage transport vehicle 10 is flying will be described.

[0048] 17 and 18, the luggage support device 14 of the unmanned luggage transport vehicle 10 of the present embodiment described above includes a limiting section 50 for preventing or suppressing the dropping of the luggage 30 during flight. The limiting section 50 includes a ground contact section 52 provided on the ground contact section 18, a drive section 53 provided on the drive section 40 side, and a connecting section 54 connecting the ground contact section 52 and the drive section 53.

[0049] As shown in FIG. 17, the grounding portion side limiting portion 52 includes a base 56 fixed to the boundary between the grounding portion main body 18A and the central leg portion 18B of one of the grounding portions 18, and a grounding arm 58 supported by the base 56. The base 56 is provided with an outer tube locking portion 56A to which one end of an outer tube 64 (described later) is locked. One end of the grounding arm 58 is connected to the lower end of the base 56 via a pin (not shown) so as to be rotatable about the horizontal direction as the axial direction. In addition, one end of a cable 66 (described later) is locked to the other end of the grounding arm 58. A protruding portion 58A protruding downward is formed in the middle between the one end and the other end of the grounding arm 58.

[0050] As shown in FIG. 18, the drive unit side limiting portion 53 includes a pressing arm 60 supported by the plate 20 (see FIG. 3). The pressing arm 60 includes a pressing portion 60A formed in a substantially C-shape when viewed from above, and a tongue-shaped extending portion 60B extending from one end of the pressing portion 60A. The end of the extending portion 60B opposite the pressing portion 60A is connected to the plate 20 (see FIG. 3) via a pin (not shown) so as to be rotatable about the vertical direction as the axial direction. The pressing portion 60A is disposed opposite the rotating portion 32A of the central link 32 in the radial direction of the rotating portion 32A. The other end of the cable 66 described later is engaged with the end of the pressing portion 60A opposite the extending portion 60B. Furthermore, one end of a pressing spring 62 as a biasing member is engaged with the end of the pressing portion 60A opposite the extending portion 60B. The other end of the pressing spring 62 is engaged with a pressing spring engaging portion (not shown) provided on the plate 20 (see FIG. 3). As a result, the pressing arm 60 is constantly biased by the pressing spring 62 toward the rotating portion 32A of the central link 32.

[0051] As shown in Fig. 17 and Fig. 18, the connection part 54 includes an outer tube 64 formed in a tubular shape and a cable 66 inserted through the outer tube 64. As shown in Fig. 17, one end of the outer tube 64 is engaged with an outer tube engaging part 56A provided on the base 56. Also, as shown in Fig. 18, the other end of the outer tube 64 is engaged with an outer tube engaging part 68 fixed to the plate 20 (see Fig. 3). As shown in Fig. 17, one end of the cable 66 is engaged with the other end of the ground arm 58. Also, as shown in Fig. 18, the other end of the cable 66 is engaged with the end of the pressing part 60A of the pressing arm 60 opposite to the extension part 60B.

[0052] In this embodiment having the limiting unit 50 described above, as shown in FIG. 17, when the unmanned baggage transport vehicle 10 is in a landing state, the grounding unit body 18A of the grounding unit 18 is in contact with the landing surface, and the protruding portion 58A of the grounding arm 58 is in contact with the landing surface. When the protruding portion 58A of the grounding arm 58 is in contact with the landing surface, as shown in FIG. 17 and FIG. 18, the cable 66 of the connection portion 54 is sent from the grounding unit side limiting portion 52 side to the drive unit side limiting portion 53 side. As a result, as shown in FIG. 18, the cable 66 presses the pressing arm 60 toward the opposite side to the rotating portion 32A of the central link 32. As a result, the pressing portion 60A of the pressing arm 60 is separated from the rotating portion 32A of the central link 32. The position of the pressing arm 60 in this state is called the allowable position D1 as the second position. When the pressing arm 60 is positioned in the permissible position D1, the rotation of the central link 32 is not restricted by the pressing arm 60, so that by operating the drive unit 40, each leg 22 can be moved toward the luggage 30 or away from the luggage 30.

[0053] As shown in FIG. 19, when the unmanned baggage transport vehicle 10 is flying, the grounding part body 18A of the grounding part 18 is separated from the landing surface, and the protruding part 58A of the grounding arm 58 is separated from the landing surface. When the protruding part 58A of the grounding arm 58 is separated from the landing surface, as shown in FIG. 20, the pressing arm 60 moves from the allowable position D1 toward the rotating part 32A of the central link 32 by the biasing force of the pressing spring 62, and the pressing part 60A of the pressing arm 60 is pressed against the rotating part 32A of the central link 32. The position of the pressing arm 60 in this state is called the limiting position D2 as a first position. When the pressing arm 60 is located at the limiting position D2, the rotation of the central link 32 is limited by the pressing arm 60, so that even if the driving part 40 is operated, each leg 22 cannot be moved toward the baggage 30 or the opposite side to the baggage 30. This makes it possible to prevent or suppress the baggage 30 from falling while the unmanned baggage transport vehicle 10 is flying.

[0054] In this embodiment, the pressing spring 62 constantly urges the pressing arm 60 toward the limiting position D2. This makes it possible to prevent or suppress the baggage 30 from falling while the unmanned baggage transport vehicle 10 is flying, even if the ground-contact-portion-side limiting portion 52 or the like malfunctions.

[0055] In addition, in this embodiment, the limiting unit 50 is configured to be provided independently of the driving unit 40. This makes it possible to prevent or suppress the baggage 30 from falling while the unmanned baggage transport vehicle 10 is flying, while eliminating the need to separately control the driving unit 40.

[0056] In addition, by using a configuration that does not require an actuator, a controller, or an electrical system, such as the limiting unit 50 of this embodiment, it is possible to suppress an increase in the weight of the luggage support device 14 caused by providing the limiting unit 50. This makes it possible to suppress a decrease in the transportable weight of the unmanned luggage transport vehicle 10.

[0057] (Limiting portion 70 using ratchet mechanism) Next, the limiting portion 70 to which a ratchet mechanism is applied will be described with reference to FIGS.

[0058] 21, the limiting section 70 to which the ratchet mechanism is applied is configured similarly to the limiting section 50 of the above-described embodiment, except that the configurations of the driving section side limiting section 53 and the central link 32 are different. Therefore, in the following, the configurations of the driving section side limiting section 53 and the central link 32 will be described, and a description of the grounding section side limiting section 52 and the connection section 54 will be omitted. Also, the same reference numerals as the members and parts already described will be used for the members and parts already described, and the description thereof will be omitted.

[0059] The drive unit side limiting portion 53 includes a ratchet arm 72 supported by a plate 20 (see FIG. 3). The ratchet arm 72 includes a curved portion 72A that is curved in an arch shape when viewed from above, and a tongue-shaped extension portion 72B that extends from one end of the curved portion 72A. The end of the extension portion 72B opposite to the curved portion 72A is connected to the plate 20 (see FIG. 3) via a pin (not shown) so as to be rotatable about the vertical direction as the axial direction. The curved portion 72A is disposed opposite the rotating portion 32A of the central link 32 in the radial direction of the rotating portion 32A. The other end of the cable 66 (see FIG. 18) is engaged with the end of the extension portion 72B on the curved portion 72A side. Furthermore, one end of the pressing spring 62 (see FIG. 18) is engaged with the end of the extension portion 72B on the curved portion 72A side. As a result, the ratchet arm 72 is constantly biased toward the rotating part 32A of the central link 32 by the pressing spring 62. The ratchet arm 72 also has a plurality of first ratchet teeth 72C that protrude from the curved part 72A toward the rotating part 32A of the central link 32. The plurality of first ratchet teeth 72C are formed in a sawtooth shape.

[0060] The central link 32 includes a plurality of second ratchet teeth 32C that protrude from the outer circumferential surface of the rotating portion 32A toward the ratchet arm 72. The plurality of second ratchet teeth 32C are formed in a sawtooth shape.

[0061] In the configuration with the limiting unit 70 described above, when the unmanned baggage transport vehicle 10 is in a landed state, the cable 66 presses the ratchet arm 72 toward the opposite side to the rotating unit 32A of the central link 32. As a result, the first ratchet teeth 72C of the ratchet arm 72 are separated from the second ratchet teeth 32C of the central link 32. The position of the ratchet arm 72 in this state is referred to as the allowable position D1 as the second position. When the ratchet arm 72 is in the allowable position D1, the rotation of the central link 32 is not restricted by the ratchet arm 72, so that the drive unit 40 can be operated to move each leg 22 toward the baggage 30 or the opposite side to the baggage 30.

[0062] As shown in FIG. 22, when the unmanned baggage transporter 10 is flying, the ratchet arm 72 moves from the allowable position D1 toward the rotating part 32A of the central link 32 by the biasing force of the pressing spring 62, and the first ratchet teeth 72C of the ratchet arm 72 mesh with the second ratchet teeth 32C of the central link 32. The position of the ratchet arm 72 in this state is referred to as the limiting position D2 as the first position. When the ratchet arm 72 is located at the limiting position D2, the rotation of the central link 32 to the other side (opposite to the direction of the arrow C2) is limited by the ratchet arm 72, so that even if the drive unit 40 is operated, each leg 22 cannot be moved to the opposite side to the baggage 30. This makes it possible to prevent or suppress the drop of the baggage 30 during the flight of the unmanned baggage transporter 10.

[0063] In contrast, when the drive unit 40 is operated to rotate the central link 32 to one side (the direction of arrow C2) with the ratchet arm 72 located at the limiting position D2, the second ratchet teeth 32C of the central link 32 climb over the first ratchet teeth 72C of the ratchet arm 72. In this manner, the limiting unit 70 described above can permit the drive unit 40 to operate in a state in which each leg 22 moves toward the load 30.

[0064] (Limiting portion 74 using a cam mechanism) Next, the limiting portion 74 to which a cam mechanism is applied will be described with reference to FIGS.

[0065] 23, the limiting section 74 to which the cam mechanism is applied is configured similarly to the limiting section 50 of the above-described embodiment, except that the configurations of the driving section side limiting section 53 and the central link 32 are different. Therefore, in the following, the configurations of the driving section side limiting section 53 and the central link 32 will be described, and a description of the ground contact section side limiting section 52 and the connection section 54 will be omitted. Also, the same reference numerals as the members and parts already described will be used for the members and parts already described, and the description thereof will be omitted.

[0066] The drive unit side limiting portion 53 includes a fixed cam portion 76 that is immovable relative to the plate 20 (see FIG. 3), and a movable cam portion 78 that is connected to the connection portion 54 and is displaceable relative to the plate 20. The drive unit side limiting portion 53 also includes an insertion portion 32D that protrudes from the rotating portion 32A of the central link 32 and is inserted through the fixed cam portion 76 and the movable cam portion 78.

[0067] The fixed cam portion 76 is formed in an elliptical shape when viewed from above. A fixed cam hole 76A having an elongated hole shape is formed in the fixed cam portion 76. The fixed cam portion 76 is fixed to a fixed cam fixing portion (not shown) provided on the plate 20 (see FIG. 3).

[0068] The movable cam portion 78 is configured similarly to the fixed cam portion 76, and is formed in an elliptical shape when viewed from above. A long movable cam hole 78A is formed in the movable cam portion 78. The movable cam portion 78 is supported by a movable cam support portion (not shown) provided on the plate 20 (see FIG. 3). This allows the movable cam portion 78 to move in a predetermined position within a predetermined range. One end of the pressing spring 62 is engaged with the movable cam portion 78. This allows the movable cam portion 78 to be constantly biased in the direction opposite to the fixed cam portion 76.

[0069] The insertion portion 32D is formed in a cylindrical shape and protrudes upward from the upper surface of the rotating portion 32A of the center link 32. The insertion portion 32D is inserted into the fixed cam hole 76A of the fixed cam portion 76 and the movable cam hole 78A of the movable cam portion 78.

[0070] In the configuration with the limiting portion 74 described above, when the unmanned baggage transport vehicle 10 is in a landed state, as shown in Figs. 24 and 25, the cable 66 presses the movable cam portion 78 toward the fixed cam portion 76. As a result, the movable cam portion 78 is disposed at a position where the horizontal position of the movable cam portion 78 and the horizontal position of the fixed cam portion 76 coincide. The position of the movable cam portion 78 in this state is referred to as the allowable position D1 as a second position. When the movable cam portion 78 is disposed at the allowable position D1, the insertion portion 32D can move along the fixed cam hole 76A of the fixed cam portion 76 and the movable cam hole 78A of the movable cam portion 78. That is, the rotation of the central link 32 is not restricted by the fixed cam portion 76 and the movable cam portion 78. Therefore, by operating the drive portion 40, each leg portion 22 can be moved toward the baggage 30 or the opposite side to the baggage 30.

[0071] In contrast, when the unmanned baggage transport vehicle 10 is flying, as shown in FIG. 23, the biasing force of the pressing spring 62 causes the movable cam portion 78 to move from the permitted position D1 to the opposite side of the fixed cam portion 76, and the insertion portion 32D of the central link 32 is sandwiched between the inner edge of the fixed cam hole 76A of the fixed cam portion 76 and the inner edge of the movable cam hole 78A of the movable cam portion 78. The position of the movable cam portion 78 in this state is referred to as the limiting position D2 as the first position. When the movable cam portion 78 is located at the limiting position D2, the insertion portion 32D cannot move along the fixed cam hole 76A of the fixed cam portion 76 and the movable cam hole 78A of the movable cam portion 78. That is, the rotation of the central link 32 is limited by the fixed cam portion 76 and the movable cam portion 78. Therefore, even if the drive portion 40 is operated, each leg portion 22 cannot be moved toward the baggage 30 or the opposite side of the baggage 30. This makes it possible to prevent or suppress the baggage 30 from falling while the unmanned baggage transport vehicle 10 is flying.

[0072] Although one embodiment of the present invention has been described above, the present invention is not limited to the above, and it is of course possible to implement the present invention in various other modified forms without departing from the spirit and scope of the present invention. [Explanation of symbols]

[0073] 10. Unmanned baggage transport vehicle 12 Small unmanned aircraft 14 Luggage support device 18 Grounding part 20 Plate (base) 22 Legs (luggage support section) 30 Luggage 32C 2nd ratchet tooth 32D Insertion part 40 Drive unit 50 Restrictions 52 Ground side limiting section 53 Drive side limiting section 54 Connection 60A Pressing part 62 Pressurizing member 72 Restrictions 72C 1st ratchet tooth 74 Restrictions 76 Fixed cam part 78 Movable cam part D1 Permitted position (second position) D2 Restricted position (first position)

Claims

1. A base on which a small unmanned aerial vehicle can be attached, A grounding portion that touches the landing surface when the aircraft is landing; A luggage support portion provided below the base and supporting luggage; a drive unit that operates in a first state to move the luggage support unit toward the luggage and that operates in a second state to move the luggage support unit away from the luggage; a limiting unit that is provided independently of the drive unit, and that allows operation of the drive unit when the ground contact unit is in contact with the landing surface, and limits operation of the drive unit in at least the second state when the ground contact unit is separated from the landing surface; Equipped with the limiting portion includes a drive portion-side limiting portion that is displaceable between a first position that limits the operation of the drive portion in at least the second state and a second position that allows the operation of the drive portion, a ground portion-side limiting portion that is provided on the ground portion, and a connection portion that connects the drive portion-side limiting portion and the ground portion-side limiting portion, When the ground contact portion side limiting portion contacts the landing surface, the connection portion is displaced, and the drive portion side limiting portion is displaced from the first position to the second position, A luggage support device in which, when the ground contact portion side limiting portion moves away from the landing surface, the connection portion is displaced and the drive portion side limiting portion is displaced from the second position to the first position.

2. 2. The luggage support device according to claim 1, further comprising a biasing member that constantly biases the drive unit side limiting portion toward the first position.

3. the drive unit-side limiting portion includes a pressing portion that is pressed against a member constituting the drive unit when the drive unit-side limiting portion is located at the first position, The luggage support device according to claim 1 , wherein the pressing portion is pressed against a member constituting the drive portion, thereby restricting the operation of the drive portion.

4. The drive unit side limiting portion includes a first ratchet tooth protruding toward the drive unit side, the drive unit includes second ratchet teeth that protrude toward the drive unit side limiting portion and mesh with the first ratchet teeth of the drive unit side limiting portion that is located at the first position, When the first ratchet teeth and the second ratchet teeth are in mesh with each other, operation of the drive unit in the second state is restricted, 2. The luggage support device of claim 1, wherein when the drive unit operates in the first state with the first ratchet teeth and the second ratchet teeth engaged, the second ratchet teeth overcome the first ratchet teeth, thereby allowing the drive unit to operate in the first state.

5. the drive unit side limiting portion includes a fixed cam portion that is immovably provided with respect to the base, a movable cam portion that is connected to the connection portion and displaceable with respect to the base, and an insertion portion that protrudes from the drive unit and is inserted into the fixed cam portion and the movable cam portion, When the movable cam portion is disposed at a position where the movement of the insertion portion is limited by both the fixed cam portion and the movable cam portion, the operation of the drive portion is limited, 2. The luggage support device according to claim 1, wherein operation of the drive unit is permitted when the movable cam portion is positioned at a position where the insertion portion can move along both the fixed cam portion and the movable cam portion.

6. Small unmanned aerial vehicles and A base on which the small unmanned aerial vehicle is attached; A grounding portion that touches the landing surface when the aircraft is landing; A luggage support portion provided below the base and supporting luggage; a drive unit that operates in a first state to move the luggage support unit toward the luggage and that operates in a second state to move the luggage support unit away from the luggage; a limiting unit that is provided independently of the drive unit, and that allows operation of the drive unit when the ground contact unit is in contact with the landing surface, and limits operation of the drive unit in at least the second state when the ground contact unit is separated from the landing surface; Equipped with the limiting portion includes a drive portion-side limiting portion that is displaceable between a first position that limits the operation of the drive portion in at least the second state and a second position that allows the operation of the drive portion, a ground portion-side limiting portion that is provided on the ground portion, and a connection portion that connects the drive portion-side limiting portion and the ground portion-side limiting portion, When the ground contact portion side limiting portion contacts the landing surface, the connection portion is displaced, and the drive portion side limiting portion is displaced from the first position to the second position, When the ground contact portion side limiting portion separates from the landing surface, the connection portion is displaced and the drive portion side limiting portion is displaced from the second position to the first position.

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