Reaction mechanism and flight system

Abstract

To provide a reaction mechanism by which an operator during flight can ensure freedom and naturalness of body motion, and a flight system.SOLUTION: A reaction mechanism 1, which is fitted to an operator equipped with a flight device, comprises: a first part 10 which is attached to a part of a leg of the operator; a second part 20 which is attached to an upper body or a waist of the operator; and a third part 30 which connects the first part 10 and the second part 20.SELECTED DRAWING: Figure 1

Description

Technical Field

[0001] The present invention relates to a reaction force mechanism and a flight system.

Background Art

[0002] Flight devices in which humans wear a propulsion system and fly have been developed (for example, Patent Documents 1, 2, and Non-Patent Document 1). The flight device is used, for example, for the purpose of assisting the movement of rescue team members for the purpose of contributing to rescue activities.

Prior Art Documents

Patent Documents

[0003]

Patent Document 1

Patent Document 2

Non-Patent Documents

[0004]

Non-Patent Document 1

Summary of the Invention

Problems to be Solved by the Invention

[0005] Each of the above-described flight devices is mainly worn on the upper body of the operator. Therefore, when flying by each of the above-described flight devices, the operator of the flight device has the lower body (especially the legs) in a suspended state in the air. For this reason, there is a problem that the degree of freedom and naturalness of body movement are greatly restricted, unlike when standing on the ground, for example.

[0006] The present invention has been made in view of the above-described circumstances, and an object thereof is to provide a reaction force mechanism and a flight system that enable a pilot in flight to ensure the freedom and naturalness of body movement.

Means for Solving the Problems

[0007] <1>The reaction force mechanism according to Aspect 1 of the present invention is a reaction force mechanism attached to a pilot wearing a flying device, and includes a first part attached to a part of the pilot's leg, a second part attached to the upper body or waist of the pilot, and a third part connecting the first part and the second part.

[0008] According to the invention according to Aspect 1, the reaction force mechanism is attached to a pilot wearing a flying device. Further, the reaction force mechanism includes a first part attached to a part of the pilot's leg, a second part attached to the upper body or waist of the pilot, and a third part connecting the first part and the second part. Thus, when the pilot to whom the reaction force mechanism is attached extends the leg, tension is generated in the third part. Due to this tension, the pilot can receive a reaction force from the first part to the leg. By this, for example, even when the pilot is flying by a flying device and the pilot's legs are in a suspended state in the air, that is, the pilot's feet are not in contact with the ground, when the pilot extends the legs, the pilot can receive a force similar to the reaction force received from the ground when standing on the ground. Therefore, even when the pilot's feet are not in contact with the ground, the pilot can apply force to the legs by using the reaction force mechanism to brace. Therefore, when the pilot is in flight, the freedom and naturalness of the pilot's body movement can be ensured. That is, for example, a pilot in flight can easily stabilize the posture. Or, a pilot in flight can easily change the posture. Further, by attaching such a reaction force mechanism to the pilot, the movement of the pilot's body can be easily utilized for instructions regarding the operation of the flying device.

[0009] <2>The reaction force mechanism according to aspect 2 of the present invention is characterized in that, in the reaction force mechanism according to aspect 1, the first part is fixed to the sole of the operator's foot.

[0010] According to the invention according to aspect 2, the first part is fixed to the sole of the operator's foot. Thereby, during flight, the operator can apply force to the leg as if standing on the ground, as if bracing. Therefore, it is easier to ensure the freedom and naturalness of the operator's body movement.

[0011] <3>The reaction force mechanism according to aspect 3 of the present invention is characterized in that, in the reaction force mechanism according to aspect 1 or aspect 2, the first part is fixed to the knee of the operator.

[0012] According to the invention according to aspect 3, the first part is fixed to the knee of the operator. Thereby, the number of instruments attached to the part below the operator's knee can be reduced. Therefore, for example, when the operator in flight lands, the sole of the foot can be used more freely.

[0013] <4>The reaction force mechanism according to aspect 4 of the present invention is characterized in that, in the reaction force mechanism according to any one of aspects 1 to 3, the second part is fixed to the shoulder of the operator.

[0014] According to the invention according to aspect 4, the second part is fixed to the shoulder of the operator. Thereby, the reaction force caused by the operator extending the leg is applied to the operator's shoulder via the second part. By this, for example, the back muscles can be assisted by the force of the operator's leg. Therefore, for example, when the operator's muscle strength is relatively low, it is easier to assist the body movement of the operator during flight.

[0015] <5>The reaction force mechanism according to aspect 5 of the present invention is characterized in that, in the reaction force mechanism according to any one of aspects 1 to 3, the second part is fixed to the waist of the operator.

[0016] According to the invention according to aspect 5, the second part is fixed to the waist of the operator. Thereby, for example, the size of the reaction force mechanism can be suppressed. Therefore, for example, the weight of the reaction force mechanism can be suppressed. In addition, it is possible to make it easier for the operator walking or flying on the ground to move the body.

[0017] <6>The reaction force mechanism according to aspect 6 of the present invention is the reaction force mechanism according to any one of aspects 1 to 3, characterized in that the second part is fixed to the flying device.

[0018] According to the invention according to aspect 6, the second part is fixed to the flying device. Thereby, for example, when the operator extends his legs, a pulling force can be applied to the flying device. In this way, the force applied by the operator to the flying device can be used, for example, for controlling the flying device. That is, for example, the thrust of the flying device can be changed according to the magnitude of the force with which the operator pulls the flying device via the reaction force mechanism. In addition, for example, the attitude of the flying device can be changed by the operator changing the attitude using the reaction force mechanism. In this way, by enabling the operator to control the flying device using his legs, the operator can use his hands freely during flight. Therefore, the operator can perform some work while staying in the air by the flying device.

[0019] <7>The reaction force mechanism according to aspect 7 of the present invention is the reaction force mechanism according to any one of aspects 1 to 3, characterized in that the second part is fixed to the full harness worn by the operator.

[0020] Here, the operator may wear the flying device via a full harness. At this time, the operator in flight is in a suspended state by the full harness. Then, the weight of the operator is added to the base of the operator's legs via the full harness. This compresses the base of the operator's legs, and the operator may feel pain. In addition, due to the long-term continuation of the suspended state, congestion may occur at the base of the operator's legs. Therefore, according to the invention related to Aspect 7, the second part of the reaction force mechanism is attached to the full harness worn by the operator. As a result, when the operator with the reaction force mechanism attached stretches their legs, the weight of the operator added to the base of the operator's legs can be added to the first part of the reaction force mechanism. Thus, it is possible to suppress the compression of the base of the operator's legs. Therefore, it is possible to suppress the operator from feeling pain and the occurrence of congestion at the base of the operator's legs. In addition, by attaching such a reaction force mechanism to the operator, it is possible to suppress the burden on the operator's body and contribute to extending the flightable time. In addition, by the operator wearing the flying device via the full harness, it is possible to facilitate the attachment and detachment of the flying device.

[0021] <8>The flight system according to Aspect 8 of the present invention is characterized by comprising a flying device and a reaction force mechanism according to any one of Aspects 1 to 7.

[0022] According to the invention related to Aspect 8, the flight system includes a flying device and a reaction force mechanism according to the present invention. Thereby, for example, the degree of freedom and naturalness of the body movement of the operator during flight can be ensured. That is, for example, the operator during flight can easily change their posture. Therefore, for example, the movement of the operator's body can be easily utilized for instructions related to the operation of the flying device. Alternatively, other various above-described effects can be enjoyed.

Effects of the Invention

[0023] According to the present invention, it is possible to provide a reaction force mechanism and a flight system that enable a pilot during flight to ensure the degree of freedom and naturalness of body movement.

Brief Description of the Drawings

[0024]

Figure 1

Figure 2

Figure 3

Figure 4

Figure 5

Figure 6

Figure 7

Figure 8

Figure 9

Figure 10

Figure 11

Figure 12

Mode for Carrying Out the Invention

[0025] Hereinafter, with reference to the drawings, a flight system and a reaction force mechanism 1 according to an embodiment of the present invention will be described. As shown in FIG. 1, the flight system according to the present embodiment includes a flying device F and a reaction force mechanism 1. The flying device F is a device that enables the operator P to fly by being worn by the human operator P. In the present embodiment, the flying device F is worn on the upper body of the operator P. That is, in the flying device F in the present embodiment, during flight, the body below the waist of the operator P (especially the legs L) is in a suspended state.

[0026] In the flight system according to this embodiment, by the operator P wearing the reaction force mechanism 1, the reaction force received by the operator P from the reaction force mechanism 1 is utilized, and the flying device F can be operated by the force of the legs of the operator P. That is, the reaction force mechanism 1 is preferably connected to and used with the flying device F. Further, the reaction force mechanism 1 is preferably provided with, for example, a bending sensor (not shown) capable of detecting the state of the leg L of the operator P, that is, the bending angle of the leg L of the operator P. In this way, it is preferable to be able to process the state of the leg L of the operator P as information related to the operation of the flying device F.

[0027] For the flying device F, for example, any arbitrary known one is preferably used. That is, for example, the flying device F is, for example, a jet pack (registered trademark) of Jetpack Aviation. Alternatively, the flying device F may be, for example, a jet suit of Gravity Industries. Alternatively, any other arbitrary one may be used for the flying device F. The flying device F may fly by being appropriately operated by the operator P, or may fly by automatic control. Further, in this embodiment, as shown in FIGS. 10 to 12 for example, the flying device F is attached to a full harness H worn by the operator P via a buckle BC.

[0028] The reaction force mechanism 1 is attached to the operator P wearing the flying device F. The reaction force mechanism 1 enables the operator P in flight by the flying device F to apply a force as if stepping firmly on the legs. In this way, the reaction force mechanism 1 has a function of enabling the operator P in flight to ensure the freedom and naturalness of body movement.

[0029] (Outline of the reaction force mechanism) As shown in FIG. 1, the reaction force mechanism 1 includes a first part 10, a second part 20, and a third part 30. The first part 10 is attached to a part of the leg L of the operator P. The second part 20 is attached to the upper body or waist of the operator P. The third part 30 connects the first part 10 and the second part 20. For example, when the operator P to whom the first part 10 and the second part 20 are attached extends the leg L, the third part 30 is pulled by the first part 10 and the second part 20 to generate tension.

[0030] With the above-described configurations, when the operator P to whom the reaction force mechanism 1 is attached extends the leg L, tension is generated in the third part 30. Due to this tension, the operator P can receive a reaction force on the leg L via the first part 10. Therefore, even when the foot Ft of the operator P is not in contact with the ground during flight by the flight system, the foot Ft can be braced in the same manner as when standing on the ground. This enables, for example, the operator P during flight to easily stabilize the posture. Alternatively, the operator P during flight can easily change the posture. Hereinafter, the details of the first part 10, the second part 20, and the third part 30 will be described.

[0031] (Details of the first part) The first part 10 is attached to a part of the leg L of the operator P. Also, one end of the third part 30 is connected to the first part 10. The first part 10 is attached, for example, so as to be wound around a part of the leg L of the operator P. That is, the first part 10 is, for example, a belt-like member made of cloth or rubber. The first part 10 may be attached, for example, so as to be hooked on a part of the leg L of the operator P. That is, the first part 10 may be formed of, for example, a wire 10W or a plate 10B made of metal or resin. Not limited to the above, any other material may be used for the first part 10 as long as it has sufficient strength against the force of the leg of the operator P. Hereinafter, several examples of the fixing position of the first part 10 on the operator P will be described.

[0032] (First example of the first part) As a first example, the first part 10 is fixed, for example, to the back of the foot Ft of the operator P. Specifically, for example, as shown in FIG. 2, the strip-shaped first part 10 is fixed so as to be wound around the tip of the foot Ft of the operator P. At this time, for example, the toe may be passed through the first part 10 formed in an annular shape by a strip-shaped material. Alternatively, the first part 10 formed by providing hook-and-loop fasteners (not shown) at both ends of the strip may be wound around the foot Ft and the hook-and-loop fasteners may be adhered to each other. Alternatively, as shown in FIG. 3, the first part 10 formed by the plate 10B, the wire 10W, etc. may be fixed so that the foot Ft of the operator P is hooked. In this case, for example, as shown in FIG. 3, the portion in contact with the back of the foot Ft of the operator P may be formed by the plate 10B, and the portion connecting the plate 10B and the third part 30 may be formed by the wire 10W. In this case, the plate 10B is preferably, for example, rectangular and the longitudinal direction thereof preferably follows the width direction of the foot Ft. The first part 10 formed as described above is preferably in contact with, for example, the vicinity of the ball of the foot of the foot Ft of the operator P, particularly as shown in FIG. 2 or FIG. 3. By this, in the state where the first part 10 is attached, it is preferable that the operator P can easily move the ankle. Alternatively, the first part 10 may be in contact with, for example, the vicinity of the toe of the foot Ft of the operator P, particularly on the back of the foot. By this, the operator P may be able to easily step on the first part 10 using the strength of the ankle.

[0033] (Second Example of the First Part) As a second example, the first part 10 is fixed to the knee K of the operator P, for example. Specifically, for example, as shown in FIG. 4, the first part 10 formed in the shape of a knee supporter is fixed so as to be wound around the knee K of the operator P. At this time, a hole 10H may be formed in the first part 10 to facilitate bending and extending of the knee by exposing the knee joint. At this time, for example, the leg L may be passed through the first part 10 formed in a cylindrical shape by a strip-shaped material. Alternatively, the first part 10 formed by providing hook-and-loop fasteners (not shown) at both ends of the strip may be wound around the foot Ft and the hook-and-loop fasteners may be adhered to each other. Also, as shown in FIG. 5, the first part 10 formed in a hook shape may be fixed so as to catch on the knee K of the operator P. At this time, it is preferable that a hook 10F made of metal or cloth is provided at a portion of the clothing of the operator P that is located at the knee K. Also, as shown in FIG. 6, the first part 10 which is a belt may be fixed so as to catch on the knee K of the operator P. At this time, it is preferable that a belt hook 10BF made of metal or cloth is provided at a portion of the clothing of the operator P that is located at the knee K. Also, as shown in FIG. 7, the first part 10 which is a buckle may be fixed so as to be assembled with the knee K of the operator P. At this time, it is preferable that one side 10BC of the buckle is provided in advance at a portion of the clothing of the operator P that is located at the knee K. Note that, with the structures shown in FIGS. 5 to 7, the first part 10 may be fixed to the calf, shin, or ankle of the operator P.

[0034] (Details of the second part) The second part 20 is attached to the upper body or waist of the operator P. Also, the other end of the third part 30 is connected to the second part 20. The second part 20 is formed in a corset shape, for example, and is attached so as to wrap around the waist of the operator P or the like. That is, the second part 20 is a belt-like member made of cloth or rubber, for example. The second part 20 may be attached so as to catch on any part of the upper body of the operator P, for example. That is, the second part 20 may be formed by a wire 10W or a plate 10B made of metal or resin, for example. Not limited to the above, any other material may be used for the second part 20 as long as it has sufficient strength against the force of the legs of the operator P. Hereinafter, several examples will be described regarding the fixing position of the second part 20 on the operator P.

[0035] (First example of the second part) As a first example, the second part 20 is fixed to the shoulder of the operator P. Specifically, for example, as shown in FIG. 8, the second part 20 formed in the shape of a nameplate is fixed so that the operator P wears it. At this time, the third part 30 is connected to the shoulder portion of the operator P wearing the second part 20. In the present embodiment, the second part 20 being fixed to the shoulder of the operator P includes the other end of the third part 30 being fixed to the shoulder of the operator P in this way. Note that, similar to the first part 10 described in FIGS. 5 to 7, hooks, belts, or buckles may be used for the second part 20. At this time, it is preferable that a hook hanger 10F, a belt hanger 10BF, or one side 10BC of a buckle is provided on the shoulder portion of the clothing of the operator P.

[0036] (Second example of the second part) As a second example, the second part 20 is fixed to the waist of the operator P. Specifically, for example, as shown in FIG. 9, the second part 20 formed in the shape of a corset is fixed so as to be wound around the waist of the operator P. At this time, for example, the body may be passed through the second part 20 formed in a tubular shape by a strip-shaped material. Alternatively, the second part 20 formed by providing hook-and-loop fasteners (not shown) at both ends of a strip may be wound around the waist and the hook-and-loop fasteners may be bonded to each other. Note that, similar to the first part 10 described in FIGS. 5 to 7, hooks, belts, or buckles may be used for the second part 20. At this time, it is preferable that a hook hanger 10F, a belt hanger 10BF, or one side 10BC of a buckle is provided on the waist portion of the clothing of the operator P.

[0037] (Third example of the second part) As a third example, the second part 20 is fixed to the flying device F. Specifically, as shown in FIG. 10, the second part 20 formed in the shape of a hook is fixed so as to be hooked on the flying device F worn by the operator P. Note that in FIG. 10, only the framework of the flying device F is schematically illustrated, and other components including the thrust mechanism are not shown. Alternatively, instead of the hook, the second part 20 formed in a bracket shape may be fixed to the flying device F worn by the operator P by bolting.

[0038] (Fourth example of the second part) As a fourth example, the second part 20 is fixed to, for example, a full harness H worn by the operator P. The full harness H is preferably any known one, for example. Here, the operator P may wear the flying device F via the full harness H. The second part 20 according to the fourth example is preferably used when the operator P wears the full harness H. Specifically, as shown in FIG. 11, the second part 20 is fixed to the waist of the full harness H. Alternatively, as shown in FIG. 12, the second part 20 may be fixed to the shoulder of the full harness H. Here, when the operator P wears the flying device F via the full harness H, the weight of the operator P is added to the base of the legs L of the operator P via the full harness H. By this, the base of the legs L of the operator P is compressed. When the second part 20 is fixed to the full harness H, by the operator P pressing down on the first part 10 by stepping on the legs, the weight of the operator P added to the base of the legs L of the operator P can be added to the first part 10 of the reaction mechanism 1. By this, it may be possible to suppress the compression of the base of the legs L of the operator P. The second part 20 according to the fourth example is used by appropriately selecting any one of a hook, a belt, or a buckle, similar to the first part 10 described in FIGS. 5 to 7. Alternatively, as the second part 20, the other end of the third part 30 may be sewn to the full harness H. In this case, the second part 20 may be regarded as the connection between the third part 30 and the full harness H.

[0039] (Details of the third part) The third part 30 connects the first part 10 and the second part 20. For example, when the operator P to whom the first part 10 and the second part 20 are attached extends the leg L, the third part 30 is pulled by the first part 10 and the second part 20 to generate tension. In this way, as described above, when the operator P to whom the reaction force mechanism 1 is attached extends the leg L, the operator P can receive a reaction force on the leg L via the first part 10. The third part 30 is, for example, a belt-shaped member made of cloth or rubber. This makes it possible for the third part 30 to easily follow the movement of the leg L of the operator P. Therefore, it is easier to ensure the degree of freedom of movement of the leg L of the operator P. The third part 30 may be, for example, a plate-shaped member. Thereby, for example, it is possible to easily and surely generate a reaction force when the operator P extends the leg L. Also, for example, since the third part 30 connecting the first part 10 and the second part 20 is a plate-shaped member, it is possible to easily and stably support the leg L of the operator P during flight. That is, for example, when the body of the operator P is flying along the horizontal direction, it is possible to easily keep the state where the operator P extends the leg L without applying force to the leg. Therefore, it is possible to easily stabilize the posture of the operator P. Also, for example, it is possible to easily reinforce the leg L of the operator P. That is, for example, when the operator P falls to the ground, the reaction force mechanism 1 receives the impact of the fall, so that it is possible to prevent the operator P from being injured such as a fracture. Not limited to the above, any other material may be used for the third part 30 as long as it has sufficient strength against the force of the leg of the operator P.

[0040] As described above, according to the reaction force mechanism 1 according to the present embodiment, it is attached to the operator P wearing the flying device F. The reaction force mechanism 1 includes a first part 10 attached to a part of the leg L of the operator P, a second part 20 attached to the upper body or waist of the operator P, and a third part 30 connecting the first part 10 and the second part 20. Thereby, when the operator P to whom the reaction force mechanism 1 is attached extends the leg L, tension is generated in the third part 30. Due to this tension, the operator P can receive a reaction force on the leg L from the first part 10. In this way, for example, even when the operator P is flying by the flying device F and the legs L of the operator P are in a suspended state, that is, the feet Ft of the operator P are not in contact with the ground, by extending the legs L, the operator P can receive a force similar to the reaction force received from the ground when standing on the ground. Therefore, even when the feet Ft of the operator P are not in contact with the ground, the operator P can apply force to the legs by using the reaction force mechanism 1 to brace himself. Therefore, when the operator P is flying, the degree of freedom and naturalness of the body movement of the operator P can be ensured. That is, for example, the operator P in flight can easily stabilize his posture. Or, the operator P in flight can easily change his posture. Also, by attaching such a reaction force mechanism 1 to the operator P, the movement of the body of the operator P can be easily utilized for instructions related to the operation of the flying device F and the like.

[0041] Further, the first part 10 is fixed to the sole of the foot Ft of the operator P. Thereby, the operator P in flight can apply force to the legs in a bracing manner with the same feeling as when standing on the ground. Therefore, it is easier to ensure the degree of freedom and naturalness of the body movement of the operator P.

[0042] Also, the first part 10 is fixed to the knee K of the operator P. Thereby, the number of instruments attached to the part below the knee K of the operator P can be reduced. Therefore, for example, when the operator P in flight lands, the sole of the foot Ft can be used more freely.

[0043] Further, the second part 20 is fixed to the shoulder of the operator P. Thereby, the reaction force generated when the operator P extends the legs L is applied to the shoulder of the operator P via the second part 20. By this, for example, the back muscles can be assisted by the force of the legs of the operator P. Therefore, for example, when the muscle strength of the operator P is relatively low, it is easier to assist the body movement of the operator P in flight.

[0044] Further, the second part 20 is fixed to the waist of the operator P. Thereby, for example, the size of the reaction force mechanism 1 can be suppressed. Thus, for example, the weight of the reaction force mechanism 1 can be suppressed. Also, the operator P walking or flying on the ground can move the body more easily.

[0045] Further, the second part 20 is fixed to the flying device F. Thereby, for example, when the operator P extends the leg L, a pulling force can be applied to the flying device F. The force applied by the operator P to the flying device F in this way can be used, for example, for the control of the flying device F. That is, for example, the thrust of the flying device F can be changed according to the magnitude of the pulling force applied by the operator P to the flying device F via the reaction force mechanism 1. Also, for example, when the operator P changes the posture using the reaction force mechanism 1, the posture of the flying device F can be changed. In this way, by enabling the operator P to control the flying device F using the leg L, the operator P can use the hands freely during flight. Therefore, the operator P can perform some work while staying in the air by the flying device F.

[0046] Here, the operator P may wear the flying device F via the full harness H. At this time, the operator P during flight is in a suspended state by the full harness H. Then, the weight of the operator P is added to the base of the leg L of the operator P via the full harness H. This compresses the base of the leg L of the operator P, and the operator P may feel pain. Also, due to the suspended state continuing for a long time, congestion may occur at the base of the leg L of the operator P. Therefore, the second part 20 of the reaction force mechanism 1 is attached to the full harness H worn by the operator P. As a result, when the operator P to whom the reaction force mechanism 1 is attached extends the leg L, the weight of the operator P applied to the root of the leg L of the operator P can be applied to the first part 10 of the reaction force mechanism 1. Therefore, it is possible to suppress the root of the leg L of the operator P from being compressed. Accordingly, it is possible to suppress the operator P from feeling pain and the occurrence of congestion at the root of the leg L of the operator P. Further, by attaching such a reaction force mechanism 1 to the operator P, it is possible to suppress the burden on the body of the operator P and contribute to lengthening the flightable time. In addition, by the operator P wearing the flying device F via the full harness H, it is possible to facilitate the attachment and detachment of the flying device F.

[0047] Further, according to the flight system according to the present embodiment, the flying device F and the reaction force mechanism 1 according to the present invention are provided. Thereby, for example, it is possible to ensure the degree of freedom and naturalness of the body movement of the operator P during flight. That is, for example, the operator P during flight can easily change the posture. Therefore, for example, the movement of the body of the operator P can be easily used for instructions related to the operation of the flying device F or the like. Alternatively, the above-described various operational effects can be enjoyed.

[0048] Note that the technical scope of the present invention is not limited to the above-described embodiment, and various modifications can be made without departing from the spirit of the present invention. For example, the reaction force mechanism 1 according to the present embodiment may be used for persons other than the operator P of the flying device F. For example, the reaction force mechanism 1 according to the present embodiment may be used by a high-altitude worker, a stuntman, or the like.

[0049] In addition, within the scope not departing from the spirit of the present invention, it is possible to appropriately replace the components in the above-described embodiment with well-known components, and the above-described modification examples may be appropriately combined.

Explanation of Reference Numerals

[0050] 1 Reaction mechanism 10 First part 10B Plate 10BC One side of the piece 10H Hole 10W Wire 20 Second part 30 Third part F Flying device H Full harness P Operator

Claims

1. A reaction force mechanism attached to a pilot wearing a flying device, comprising: a first part attached to a part of the pilot's leg; a second part attached to the pilot's upper body or waist; a third part connecting the first part and the second part. The reaction force mechanism is characterized by the above.

2. The reaction force mechanism according to Claim 1, wherein the first part is fixed to the sole of the pilot's foot.

3. The reaction force mechanism according to Claim 1, wherein the first part is fixed to the pilot's knee.

4. The reaction force mechanism according to Claim 1, wherein the second part is fixed to the pilot's shoulder.

5. The reaction force mechanism according to Claim 1, wherein the second part is fixed to the pilot's waist.

6. The reaction force mechanism according to Claim 1, wherein the second part is fixed to the flying device.

7. The reaction force mechanism according to Claim 1, wherein the second part is fixed to the full harness worn by the pilot.

8. A flight system, comprising: a flying device; the reaction force mechanism according to any one of Claims 1 to 7. The flight system is characterized by the above. ​ ​ ​ ​ ​ ​ ​

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