KR20190121920A - Jumpping flapper robot - Google Patents

Abstract

The present invention relates to a jumping flying robot comprising: a first base; a jump part comprising a plurality of legs upright on the first base and supporting a vertical jump; a second base coupling the plurality of legs; a wing part comprising a plurality of flappers coupled to the second base; and a driving part disposed on the second base and simultaneously operating the plurality of legs and the plurality of flappers. Therefore, the jumping flying robot can perform both a jumping and a flying mechanism at the same time to quickly move in an atypical environment such an obstacle, a rough terrain, and the like, for example, in a disaster environment such as a collapsed wall.

Description

JUMPING FLAPPER ROBOT}

TECHNICAL FIELD The present invention relates to a hopping flying robot, and more particularly, to jump and fly simultaneously through a single driving mechanism to move more efficiently in atypical environments such as obstacles and rough terrain, for example, in a disaster environment such as a collapsed wall. To a flying robot that can jump.

Recently, robots are being developed for various purposes such as industry and education, and flying robots have been developed to perform specific purposes such as moving images while moving through a flight.

Flying robots can adopt a propeller model that mimics a helicopter, which can utilize existing helicopter technology, but can be difficult to operate efficiently in close proximity to ground.

In addition, ground mobile robots can be operated on the ground, but they efficiently move through obstacles such as obstacles and rough terrain, such as collapsed walls, and bypass obstacles to efficiently carry out tasks such as rescue activities and distress signals. It can be difficult to do.

Korean Patent No. 10-1489156 relates to an obstacle hopping robot, and a base frame for supporting a servomotor and one end of each of the first connecting portions of the base frame are overlapped and rotatably coupled, and the other ends thereof are symmetric. A first link member and a second link member which are formed, a second link member formed at the other end of the first link member and one end is hinged, and a third link member having a support portion at the other end thereof, and the second link member. And a third link member formed at the other end of the third linking portion and hinged, and having a fourth link member formed at the other end and a support portion formed at the other end thereof, and an elastic adjustment member formed at the second connection portion and the third connection portion. Four centers of each of the link members intersect to form an intersection, and the servomotor and the intersection are connected by a twist chamber.

Korean Patent No. 10-1766770 relates to an active clutch mechanism and a hopping robot having the same, which is connected to a motor and receives a driving force of the motor to rotate about a rotation axis; A planetary gear disposed to contact the sun gear and pivoting the sun gear, the planetary gear rotating about a rotation axis spaced apart from the rotation axis of the sun gear; And a winding gear selectively contacted with the planetary gear and configured to be rotatable about a rotation axis by the rotation of the planetary gear. When the sun gear is rotated in one direction, the planetary gear is in the one direction. Turning the sun gear to contact the winding gear to rotate the winding gear to wind a wire to store energy in an energy storage connected to the winding gear, and when the sun gear is rotated in the opposite direction to the one direction, The planetary gear may rotate the sun gear in a direction different from the one direction to release energy stored in the energy storage part spaced apart from the winding gear.

Korea Patent Registration No. 10-1489156 (2015.01.28 registration) Korea Patent Registration No. 10-1766770 (2017.08.03 registration)

One embodiment of the present invention is to provide a hopping flying robot that improves the hopping performance by simultaneously performing the hopping and wings through a single drive motor.

One embodiment of the present invention is to provide a flying robot including a jump for performing a vertical jump by folding (refolding) to the original length after folding a plurality of legs using a clutch mechanism with a single drive motor.

An embodiment of the present invention is to provide a flying robot including a wing that performs a plurality of flapper wings using a clutch mechanism as a single drive motor.

One embodiment of the present invention is to provide a hopping flying robot that includes a single drive motor and a drive unit using a clutch mechanism to selectively transfer the driving force of the first gear ratio and the second gear ratio to perform leap and wing at the same time.

Among the embodiments, the hopping flying robot includes a first base, a hop including a plurality of legs upright on the first base and supporting vertical hopping, a second base combining the plurality of legs, and the second base A wing including a plurality of flappers coupled to the upper portion, and a driving portion disposed on the second base for operating the plurality of legs and the plurality of flappers at the same time.

Each of the plurality of legs includes first and second links connected to the first and second bases, respectively, a joint disposed between the first and second links, controlled by the driving unit, And a winching cable that pulls the end to create a hopping force for the vertical hopping. In one embodiment, each of the plurality of legs further comprises a third link that is secured to the interruption of the second link and vertically reciprocates the interruption of the first link during the vertical hopping through the winching cable. In one embodiment, each of the plurality of legs further comprises at least one elastic body that generates a jumping force for vertical leap connected between the joints connecting the first and second links and the reciprocating end of the third link.

The driving unit includes a first gear for driving the plurality of legs and controlling the winching cable through a first gear ratio, and a second gear for driving the plurality of flappers through a second gear ratio. In one embodiment, the drive unit further comprises a third gear that is fastened or spaced apart through the clutch mechanism and the first gear and selectively drives the first and second gears. The driving unit may further include a driving motor and a fourth gear connected to the driving motor and driving the third gear at all times. In one embodiment, the drive unit engages the third gear to the first gear in the push state and the third gear to the second gear in the non-push state to support selective driving of the third gear. It further comprises a pushing lever. In one embodiment, the drive unit further comprises a roller unit including at least one roller for adjusting the direction of the force of the winching cable. In one embodiment, the drive unit further comprises a rack-pinion gear coupled to the second gear through a slider-crank to drive the plurality of flappers.

Among the embodiments, the hopping flying robot has a first base, upright on the first base and supports vertical hopping, each of which is fixed to the interruption of the second link and the first and second links interconnected via a joint. A jumper comprising a third link capable of reciprocating an interruption of the first link and a plurality of legs including an elastic body connected between the joint and the reciprocable end of the third link, a second coupling the plurality of legs A base is disposed on the second base and includes a drive unit for generating the elastic force of the elastic body by folding the first and second links through a drive motor and supporting vertical leap through the elastic force.

The disclosed technique can have the following effects. However, since a specific embodiment does not mean to include all of the following effects or only the following effects, it should not be understood that the scope of the disclosed technology is limited by this.

One embodiment of the present invention provides a hopping flying robot that improves hopping performance by simultaneously performing hopping and winging through a single drive motor.

One embodiment of the present invention provides a flying robot including a jumping part for folding a plurality of legs using a clutch mechanism with a single drive motor, and then restoring (unfolding) the original length to perform vertical leap.

One embodiment of the present invention provides a flying robot including a wing that wings the plurality of flappers using a clutch mechanism as a single drive motor.

One embodiment of the present invention provides a hopping flying robot that includes a single driving motor and selectively transfers the driving force of the first gear ratio and the second gear ratio to a drive unit using a clutch mechanism to simultaneously perform vertical leap and wing.

1 is a perspective view showing a hopping flying robot according to an embodiment of the present invention.
2A and 2B are side views illustrating a leap portion of the leap flying robot according to FIG. 1.
3A and 3B are side views illustrating a driving unit of the hopping flying robot according to FIG. 1.
4 is a side view illustrating a driving unit of the hopping flying robot according to FIG. 1.
5 is a perspective view illustrating a wing of the hopping flying robot according to FIG. 1.
6 is a view showing a simplified model of the hopping flying robot according to FIG.
FIG. 7 is a view illustrating a leap velocity and a leap force simulation result of the leap flying robot according to FIG. 1.
8 is a view showing the results of the jump simulation according to the presence or absence of the wing portion of the hopping flying robot according to Figure 1 and the operating frequency by 15Hz, 19Hz.
FIG. 9 is a perspective view showing an assembled state of the hopping flying robot prototype in FIG. 1. FIG.
10 is a view showing the actual leap results according to the operation of the wing portion of the completed hopping flying robot in FIG. 9 and the operating frequency of 15Hz, 19Hz.
FIG. 11 is a view showing numerical comparisons between the presence or absence of a wing unit in the actual hopping flight of the completed hopping flying robot shown in FIG.

Description of the present invention is only an embodiment for structural or functional description, the scope of the present invention should not be construed as limited by the embodiments described in the text. That is, since the embodiments may be variously modified and may have various forms, the scope of the present invention should be understood to include equivalents capable of realizing the technical idea. In addition, the objects or effects presented in the present invention does not mean that a specific embodiment should include all or only such effects, the scope of the present invention should not be understood as being limited thereby.

On the other hand, the meaning of the terms described in the present application should be understood as follows.

Terms such as "first" and "second" are intended to distinguish one component from another component, and the scope of rights should not be limited by these terms. For example, the first component may be named a second component, and similarly, the second component may also be named a first component.

Singular expressions should be understood to include plural expressions unless the context clearly indicates otherwise, and terms such as "comprise" or "have" refer to a feature, number, step, operation, component, part, or feature thereof. It is to be understood that the combination is intended to be present and does not exclude in advance the possibility of the presence or addition of one or more other features or numbers, steps, operations, components, parts or combinations thereof.

All terms used herein have the same meaning as commonly understood by one of ordinary skill in the art unless otherwise defined. Generally, the terms defined in the dictionary used are to be interpreted to coincide with the meanings in the context of the related art, and should not be interpreted as having ideal or excessively formal meanings unless clearly defined in the present application.

Robots that simultaneously jump and fly corresponding to biological observations of multi-moving insects capable of integrated movement of jump and flight, such as grasshoppers, may have improved mobility effects by increasing the height of jump.

These robots can easily overcome obstacles that cannot be bypassed by natural disasters or accidents by leaping and flying, and the demand for these robots is increasing due to the increased efficiency in carrying out tasks such as saving lives and distress signals.

 Accordingly, the present invention is a leap inspired by the movement method that the grasshopper bends the legs to save the leap energy for the leap and then releases the leap energy in a short time to fly the wings at the same time as the leap to increase the leap height and moving distance. It's about a hopping flying robot that integrates the multi-movement capabilities of a flight.

1 is a perspective view showing a hopping flying robot according to an embodiment of the present invention.

Referring to FIG. 1, the hopping flying robot 100 includes a first base 110, a jump unit 120, a second base 130, a wing unit 140, and a driving unit 150.

The first base 110 may be in contact with the floor and is connected to the jumping part 120. In one embodiment, the first base 110 may be implemented in a circular shape for the fall prevention and the leap efficiency (leap and landing) of the leap flying robot 100.

The jump part 120 is designed for the hopping of the hopping flying robot 100 and includes a plurality of legs 122, and the plurality of legs 122 are erected on the first base 110 and the second legs. It is connected to the base 130.

The second base 130 is disposed between the jumping part 120 and the driving part 150, supports the wing part 140 and the driving part 150, and drives the driving part 150 and the jumping part through the winching cable 280. 120) is used to connect. In one embodiment, the second base 130 may be connected to the jumper 120 to be implemented as a skeleton for mounting the drive unit 150.

The wing 140 may be implemented with a plurality of flappers 142 that may be coupled to both sides of the driving unit 150, and may interlock with the driving unit 150 to perform front and rear reciprocating wings.

2A and 2B are side views illustrating a leap of the leap flying robot 100 according to FIG. 1.

2A and 2B, the jumper 120 includes a plurality of legs 122, a plurality of links 210, 220, and 230, a plurality of joints 240, 250, and 260, one or more elastic bodies 270, and a winching cable 280. ).

Each of the plurality of legs 122 may perform folding and restoration (ie, unfolding) to its original length through rotation of joints 240, 250, and 260 disposed between the plurality of links 210, 220, and 230.

The first link 210 is connected to the first base 110 at the first end and the second link 220 at the second end. The second link 220 is connected to the first link 210 at the first end and to the second base 130 at the second end. The first link 210 and the second link 220 are coupled through the first joint 240.

The third link 230 is connected via a second joint 250 in the middle of the second link 220 at the first end and is coupled to the first link 210 at the second end 260. It is connected through the first link 210 can move in the folding and un-folding process.

The elastic body 270 connects the first joint 240 between the first link 210 and the second link 220 and the third joint 260 between the first link 210 and the third link 230. And may be composed of one or more elastic modules (eg, springs).

The winching cable 280 may be connected to the distal end of the first link 210 and the driving unit 150 to pull the distal end of the first link 210 by the operation of the driving unit 150.

2B illustrates a folding state of the plurality of legs 122.

In FIG. 2B, the plurality of legs 122 are folded by the first link 210 pulled by the tension of the winching cable 280 in the jump 120. Thus, the distal end of the third link 230 moves along the third joint 260 toward the distal end of the first link 210 at the interruption of the first link 210.

As a result, the elastic body 270 is tensioned in the course of movement on the first link 210 through the third joint 260 of the second end of the third link 230, thereby allowing for the vertical leap of the jump part 120. The jumping force can be stored as elastic energy. The jumping unit 120 may perform vertical leaping by restoring (unfolding) the plurality of legs 122 to their original lengths for a short time by using elastic energy.

3A and 3B are side views illustrating the driving unit 150 of the hopping flying robot 100 according to FIG. 1.

3A illustrates a third gear 330 engaged with the first gear 310 in the driving unit 150 of the hopping flying robot 100 according to FIG. 1 to set the driving force of the driving motor 360 to the first gear ratio with the first gear ratio. Indicate a state of forwarding to 310.

Referring to FIG. 3A, the driving unit 150 includes a first gear 310, a second gear 320, a third gear 330, a fourth gear 340, a driving motor 360, and a control servo 370. It includes.

The third gear 330 is raised or lowered on the clutch shaft 350 by the control servo 370 and is selectively engaged or spaced apart from one of the first gear 310 or the second gear 320 via the clutch mechanism. The driving force of the driving motor 360 is transmitted to the first gear ratio or the second gear ratio to one of the first or second gears 310 and 320.

The fourth gear 340 is constantly engaged with the third gear 330 to transmit the driving force of the driving motor 360 to the third gear 330.

The driver 150 transmits the driving force to the first gear ratio to perform the hopping of the hop unit 120. On the other hand, the driving force is transmitted to the wing 140 with the second gear ratio to perform the wing of the wing 140.

The driving unit 150 is a clutch for raising or lowering the third gear 330 on the clutch shaft 350 through the control servo 370 to select and transfer the first gear ratio and the second gear ratio to the single drive motor 360. Use a mechanism.

 When the third gear 330 ascends on the clutch shaft 350, the third gear 330 is engaged with the first gear 310 to transmit the driving force at the first gear ratio. On the other hand, when the third gear 330 descends on the clutch shaft 350, the third gear 330 may be engaged with the dog-clutch mechanism to transmit the driving force of the second gear ratio.

In one embodiment, the third gear 330 may transmit a driving force to the first gear 310 in a 400: 1 gear ratio. In addition, the third gear 330 may transmit a driving force to the second gear 320 at a gear ratio of 16: 1.

The first gear 310 receives the driving force from the driving motor 360 and winds the winching cable 280 connected by rotating in one direction with the first gear ratio. The winching cable 280 is wound by the first gear 310, pulling the first link 210 to tension to bring the plurality of legs 122 into a folded state.

The control servo 370 includes a pushing lever 374 capable of raising or lowering the third gear 330 on the clutch shaft 350. The pushing lever 374 is raised or lowered by the pushing lever crank 372, and the control servo 370 may control the pushing lever crank 372. The control servo 370 may include a servo motor for controlling the pushing lever crank 372.

When the pushing lever 374 is lowered, the third gear 330 descends on the clutch shaft 350 in a pushed state and is engaged with the first gear 310. In contrast, the third gear 330 ascends on the clutch shaft 350 in a non-pushing state when the pushing lever 374 is raised, is spaced apart from the first gear 310, and the second gear 320 and the dog-clutch mechanism. Is fastened.

When the first gear 310 is converted from the push state to the non-push state, the first gear 310 rotates in the reverse direction of one direction and releases the winching cable 280. When the jumping unit 120 is converted from the push state to the non-push state, the legs 120 restore (unfold) the plurality of legs 122 to their original lengths in a short time by using the elastic energy stored in the folded state. A leap can be made.

FIG. 3B illustrates that the third gear 330 is engaged with the second gear 320 by the dog-clutch mechanism in the non-pushing state in the driving unit 150 of the hopping flying robot 100 according to FIG. 1. It indicates the transmission of the driving force of the second gear ratio.

The third gear 330 rotates in one direction in a non-push state and ascends on the clutch shaft 350 to engage the dog gear clutch with the second gear 320. The driving force of the single drive motor 360 is transmitted to the wing 140 through the second gear 320 at a second gear ratio. Therefore, the wing 140 performs a plurality of flaps 142 by the driving force of the second gear ratio transmitted.

As a result, the hopping flying robot 100 has a vertical lever when the pushing lever 374 is non-pushed to the control servo 370 so that the third gear 330 is dog-clutched with the second gear 320. And wing at the same time.

FIG. 4 illustrates that the first gear 310 is spaced apart from the third gear 330 in a non-pushing state in the driving unit 150 of the hopping flying robot 100 according to FIG. 1 so that the first gear 310 is in one direction. Rotation in the reverse direction shows the release state of the winching cable 280.

Referring to FIG. 4, the roller part 410 includes a plurality of rollers 420.

The roller unit 410 controls the direction of the track in which the winching cable 280 is wound or released according to the rotation of the first gear 310 in the push state and the non-push state using the plurality of rollers 420.

The third gear 330 engages the dog-clutch with the second gear 320 in the non-pushing state to drive the second gear 320 at the driving force of the second gear ratio.

 The wing 140 is configured to drive a plurality of flappers 142 based on a combination of a slider-crank 510 and a rack-pinion 520 mechanism by using a driving force converted into a second gear ratio through the second gear 320. Let the wings fly

5 is a perspective view showing a wing of the hopping flying robot 100 according to FIG. 1.

Referring to FIG. 5, the wing 140 includes a slider-crank gear 510 and a rack-pinion gear 520.

The rack-pinion gear 520 may drive a plurality of pinion gears on both sides due to the symmetrical rack gear arrangement, and operate the plurality of flappers 142 connected to the plurality of pinion gears.

The wing 140 wings the driving force transmitted from the second gear 320 to the plurality of flappers 142 using the slider-crank 510 and the rack-pinion 520 mechanism. In one embodiment, the plurality of flappers 142 may fly at an amplitude of about 140 °.

6 is a diagram illustrating a simplified model of the flying flight robot 100 according to FIG. 1.

The direction of the jumping force R may be the same as the velocity vector and the direction. The jumping angle θ may be perpendicular to the ground. Therefore, the hopping of the hopping flying robot 100 may be expressed as an angle δ formed at the first joint 240 between the first link 210 and the second link 220.

In one embodiment, the angle δ between the first link 210 and the second link 220 of the hopping flying robot 100 can be expressed by the following equation.

[Equation 1]

α is the angle between the second link 220 and the third link 230 at the second joint 250, a is the distance between the first joint 240 and the second joint 250, c is the third link ( Corresponds to the length of 230).

The speed of the hopping flying robot 100 according to FIG. 6 may be expressed by the following equation.

[Equation 2]

V corresponds to the speed of the hopping flying robot 100 and L corresponds to the length of the second link 220.

Acceleration of the hopping flying robot 100 according to Figure 6 can be expressed by the following equation.

[Equation 3]

In one embodiment, the hopping force of the hopping flying robot 100 can be expressed by the following equation.

[Equation 4]

R is the hopping force of the hopping flying robot, b is the length of the elastic body 270 is extended in the folded state connected to the first joint 240 and the third joint 260, b ₀ is the first joint 240 and the third joint The length in a state before the plurality of legs 112 of the elastic body 270 connected to 260 (that is, unfolding), K, corresponds to the elastic modulus of the elastic body 270.

In one embodiment, the hopping motion equation of the hopping flying robot 100 according to FIG. 6 may be expressed by the following equation.

[Equation 5]

m corresponds to the mass of the hopping flying robot.

In one embodiment, the flight motion equation of the hopping flying robot 100 according to Figure 6 can be expressed by the following equation.

[Equation 6]

Use the Oξη coordinate system to find flight motion equations. ξ represents the horizontal axis η represents the vertical axis. A is the cross-sectional area of the hopping flying robot 100, ρ _air is 1.225kg / m ³ , the air density of the sea surface, the drag coefficient C _D is 1.3 and F _T corresponds to the propulsion by the wing of the hopping flying robot (100).

FIG. 7 is a view illustrating a jump speed and a jump force simulation result of the jump flight robot 100 according to FIG. 1.

For example, to simulate the hopping flying robot 100 using Equation 6, b ₀ = 0.018 m, m = 0.023 kg, K = 850 N / m, L = 0.04 m, a = 0.01 m, c = 0.025 m and δ = 20 ° were set as conditions. The simulations were performed using Matlab (Release 2015) and ODE45 solver (Shampine et al., 2003).

As a result of the hopping speed and the hopping force simulation, the hopping speed of the hopping flying robot 100 increased linearly with a constant acceleration of about 176 m / s ² . The plurality of legs 122 of the hopping flying robot 100 are restored to their original length for a short time of about 0.025 seconds. The hopping flying robot 100 reaches a maximum speed of 4.4 m / s in 0.025 seconds. The hopping force of the hopping flying robot 100 increases during the initial 0.015 seconds and then decreases to become “0”. At time “t = 0”, an elastic force 270 generates a jumping force of 1.6N. The hopping force of the hopping flying robot 100 has a maximum value of 0.015 seconds with a force of 2.78N.

8 is a view showing the results of the jump simulation according to the presence or absence of the operation of the wing 140 of the hopping flying robot 100 according to FIG.

In FIG. 8, the results of the leap simulation without the take-off of the wing (Without FW), the leap and the 15 Hz wing, and the leap and the 19 Hz wing are shown. Each simulation example was simulated with the same weight as the actual weight of the robot. The 15 Hz wing propulsion F _T = 5.83 gf and the 19 Hz wing propulsion F _T = 10.34 gf of the hopping flying robot were measured experimentally. The hopping simulation result of the hopping flying robot 100 without wing wing performance was about 0.72 m.

The hopping flying robot 100 performing the hopping and the 15 Hz wing jumped to a height of 0.89m, which showed an increase of about 23.6% from the hopping without the winging of the wing. The leap and the hopping flying robot 100 performing the 19 Hz leap to the height of 1.00m showed an increase of about 38.9% than the leap without the wing performance. Therefore, the hopping flight mechanism of the hopping flight robot 100 shows a simulation result to improve the hopping height.

FIG. 9 shows a state in which the prototype of the hopping flying robot 100 according to FIG. 1 is assembled.

In one embodiment, the hopping flying robot 100 is designed with Computer Aid Design (CAD) to enable CNC machines (MM-30S, resolution 10μm, MANIX, Korea) and 3D printers (3DWOX DP200, layer thickness 0.05-0.4 mm, Sindoh , Korea).

Gears of the wing 140 may be made of an epoxy glass sheet. The plurality of links 210, 220, 230 and the frame constituting the plurality of legs 122 of the jumping part 120 may be assembled with a 0.8 mm carbon epoxy sheet. Four springs (Misumi, WFSP4-0.5) can be used to store elastic energy for vertical leap with elastomer 270.

The hopping flying robot 100 uses an R / C 900 MHz band receiver (Hip-hop II RC receiver, Micro Flier Radio) as a signal receiver and a DC motor (Didel MK-07, Switzerland) as a driving motor 360. A micro servo (HK5320, HobbyKing, Hong Kong) may be used as the servo motor of the control servo 370.

The first small 50 mAh lithium polymer battery (1.7 g) for operating the 15 Hz wing 140 and the second small 30 mAh lithium polymer battery (1.2 g) for operating the 19 Hz wing 140 may be supplied. .

The push lever crank 372 connecting the control servo 370 and the push lever 374 may use a steel rod and the nominal cable 280 may use a high strength cable.

The plurality of flappers 142 may be designed to reduce the influence of wing inertia during the wing operation. The front edges of the plurality of flappers 142 may be a carbon rod having a diameter of 1 mm and a length of 80 mm. The flapper membrane constituting the plurality of flappers 142 is composed of polyethylene terephthalate (PET) and can be reinforced with one layer of carbon strip and the area is about 20 cm ^2. And an aspect ratio of about 3. Each flapper 142 weighs approximately 0.12 g.

FIG. 10 shows the difference in the height of the jump according to whether the wing unit 140 is operated and the wing unit 140 is operated at a frequency of 15 Hz and 19 Hz.

The hopping flying robot 100 which performed only the hopping operation of the hopping part 120 without operating the wing 140 had a maximum hopping height of 0.67 m and a maximum hopping height reaching time of 0.38 s. The hopping flying robot 100 operating the wing 140 at 15 Hz simultaneously with the hopping of the hopping part 120 recorded a maximum hopping height of 0.77 m and a maximum hopping height reaching time of 0.55 s. The hopping flying robot 100 operating the wing 140 at 19 Hz simultaneously with the hopping of the hopping part 120 recorded a maximum hopping height of 0.85 m and a maximum hopping height reaching time of 0.56 s.

As a result, the winging operation of the wing 140 operating simultaneously with the leap of the leap 120 greatly improved the maximum leap height of the leap flying robot 100.

FIG. 11 is a diagram comparing and comparing numerically tracking the leap records according to whether or not the wing 140 is operated and 15 Hz and 19 Hz for each operating frequency in the actual leap flight of the completed flying flight robot 100 according to FIG. 9.

In FIG. 11, in the actual hopping process of the hopping flying robot 100, rotation was reduced by 8.3% to 14.0% than the other hopping simulation results of FIG. 8. Leap flying robot that operates the wing unit 140 at 15 Hz and 19 Hz at the same time as the leaping unit 120 leaps, compared to the leap flying robot 100 that makes only the leap of the leaping unit 120 without operating the wing unit 140. (100) showed significant jump height increases of 18.2% and 30.3%, respectively.

The hopping flying robot 100 transmits the power of the single drive motor 360 to the first gear ratio to simultaneously perform the hopping of the hopping part 120 and the wing of the wing 140 through one driving motor 360. It includes a drive unit 150 using a clutch mechanism that can be selected and switched among the second gear ratio.

The flying flight robot 100 uses the nominal cable 280 to fold the plurality of legs 122 of the jumping part 120 through the driving part 150 including the single driving motor 360 in the elastic body 270. By performing the vertical leap by restoring to the original length in a short time using the elastic force stored in the) and at the same time performing a plurality of flapper 142 of the wing 140 wings more than when performing the leap of the leap 120 Can jump to jump height.

Although described above with reference to a preferred embodiment of the present application, those skilled in the art various modifications of the present invention without departing from the spirit and scope of the invention described in the claims below And can be changed.

100: Leap Flying Robot
110: first base 120: jump part
122: plurality of legs 130: second base
140: wing 142: a plurality of flappers
150: drive unit
210: first link 220: second link
230: third link 240: first joint
250: second joint 260: third joint
270: a plurality of elastomers 280: winching cable
310: first gear 320: second gear
330: third gear 340: fourth gear
350: clutch shaft 360: drive motor
370: control servo 372: pushing lever crank
374: pushing lever 410: roller portion
420: a plurality of rollers
510: sliding-crank gear 520: rack-pinion gear

Claims (11)

A first base;
A jump portion comprising a plurality of legs upright on the first base and supporting vertical jumps;
A second base coupling the plurality of legs;
A wing portion including a plurality of flappers coupled on the second base; And
And a driving part disposed on the second base and simultaneously operating the plurality of legs and the plurality of flappers.
The method of claim 1, wherein each of the plurality of legs
First and second links connected to the first and second bases, respectively;
A joint disposed between the first and second links; And
And a winching cable controlled by the drive unit and capable of pulling the end of the first link.
The method of claim 2, wherein each of the plurality of legs
And a third link connected to the interruption of the second link during the vertical hopping through the winching cable and capable of reciprocating the interruption of the first link.
The method of claim 3, wherein each of the plurality of legs
And at least one elastic body for generating a jumping force for vertical leap connected between the joint connecting the first and second links and the reciprocating end of the third link.
The method of claim 1, wherein the driving unit
A first gear for driving the plurality of legs and controlling a winching cable through a first gear ratio;
And a second gear for driving the plurality of flappers through a second gear ratio.
The method of claim 5, wherein the driving unit
And a third gear engaged or spaced through the clutch mechanism and the first and second gears and selectively driving the first and second gears.
The method of claim 6, wherein the driving unit
Drive motors; And
And a fourth gear connected to the drive motor and driving the third gear at all times.
The method of claim 6, wherein the driving unit
And a pushing lever which engages the third gear to the first gear in a push state and engages the third gear to the second gear in a non-push state to support selective driving of the third gear. Featuring a flying flight robot.
The method of claim 5, wherein the driving unit
The hopping flying robot, characterized in that it further comprises a roller unit including at least one roller for adjusting the direction of the force of the winching cable.
The method of claim 5, wherein the driving unit
And a rack-pinion gear engaged with the second gear and a slider-crank to drive the plurality of flappers.
A first base;
A third upright on the first base and supporting a vertical leap, each of the first and second links interconnected via a joint, fixed to the interruption of the second link and capable of reciprocating the interruption of the first link A jumping portion comprising a link and a plurality of legs including an elastic body connected between the joint and the reciprocating end of the third link;
A second base coupling the plurality of legs;
And a driving part disposed on the second base and folding the first and second links through a driving motor to generate an elastic force of the elastic body and to support vertical leap through the elastic force.

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