KR101882226B1 - Training Apparatus and Method for Emergency in Deploying Parachute - Google Patents

Training Apparatus and Method for Emergency in Deploying Parachute Download PDF

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Publication number
KR101882226B1
KR101882226B1 KR1020160136625A KR20160136625A KR101882226B1 KR 101882226 B1 KR101882226 B1 KR 101882226B1 KR 1020160136625 A KR1020160136625 A KR 1020160136625A KR 20160136625 A KR20160136625 A KR 20160136625A KR 101882226 B1 KR101882226 B1 KR 101882226B1
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South Korea
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parachute
preliminary
deployment
trainee
sensor
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KR1020160136625A
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Korean (ko)
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KR20180043646A (en
Inventor
염도호
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주식회사 에이스카이
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Priority to KR1020160136625A priority Critical patent/KR101882226B1/en
Priority to PCT/KR2016/011879 priority patent/WO2018074635A1/en
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    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63GMERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
    • A63G1/00Roundabouts
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63GMERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
    • A63G31/00Amusement arrangements
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D23/00Training of parachutists
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/04Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes for measuring tension in flexible members, e.g. ropes, cables, wires, threads, belts or bands
    • GPHYSICS
    • G08SIGNALLING
    • G08BSIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
    • G08B21/00Alarms responsive to a single specified undesired or abnormal condition and not otherwise provided for
    • G08B21/18Status alarms
    • GPHYSICS
    • G09EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09BEDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00Simulators for teaching or training purposes
    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63GMERRY-GO-ROUNDS; SWINGS; ROCKING-HORSES; CHUTES; SWITCHBACKS; SIMILAR DEVICES FOR PUBLIC AMUSEMENT
    • A63G31/00Amusement arrangements
    • A63G2031/005Skydiving

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Business, Economics & Management (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Management (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

An emergency response coping training device and method in a parachute deployment is disclosed. The emergency response coping training apparatus according to an embodiment of the present invention includes a support having an initial state parallel to the installation surface, a harness to be worn on the body of the trainee, and a plurality of harnesses for connecting the harness and the support to the support, A first sensor installed on the connecting string to sense the degree of performance in performing the operation of unscrewing the twisted connecting string, and a second sensor mounted on the connecting string, And a control unit for deciding whether or not to unlock.

Description

Technical Field [0001] The present invention relates to an emergency response apparatus and method for emergency deployment in a parachute deployment,

The present invention relates to an emergency response coping training apparatus and method in a parachute deployment, and more particularly, to an emergency response coping training apparatus and method capable of coping with a twist of a connecting string and deployment of a parachute during deployment of a parachute.

Generally, a parachute deployment training, a parachute descent training, etc., are trained in a flight or a helicopter, and a drop trainer (hereinafter referred to as a "trainer") at a certain altitude will jump over the parachute and land on the ground.

This training is most desirable when a drop trainer rides on a real aircraft or a helicopter and trains at a certain altitude or above. However, since the cost of flying an aircraft or a helicopter is high, it is difficult to frequently operate an aircraft or a helicopter. It is hard to practice dropping training practically. In addition, it is not possible to perform such training because it is impossible to take off and land the aircraft or helicopter under the weather conditions such as bad weather.

In addition, if an unskilled drop trainer is dropped on an actual aircraft or helicopter, it can be dangerous for a momentary mistake. Therefore, I need a mock drop training.

To solve these problems, there have been developed simulated drop training apparatuses capable of performing parachute deployment training and drop training under conditions similar to those of actual announcement on the ground without using aircraft or helicopter.

The simulator for the parachute descent training is designed to be able to train under the actual conditions without having to operate the aircraft or helicopter by installing a virtual simulator on the ground. It makes it possible to train in situations that can not be done. In addition, the simulator can prevent an accident that may occur during a parachute descent training on an aircraft or a helicopter, and can save fuel due to the operation of an aircraft or a helicopter.

However, at present, a number of drop descenders have been developed, but the development of a training device capable of coping with the unfolding of the main parachute due to the twist of the connecting string during deployment of the parachute is insufficient.

Korean Patent No. 0402933 Korean Patent Publication No. 10-2007-0083510

SUMMARY OF THE INVENTION The present invention has been made to overcome the above-mentioned problems, and an object of the present invention is as follows.

First, the present invention is to provide an emergency response coping training device and method capable of normally deploying a main parachute in response to a twist of a connecting string when a parachute is deployed.

Second, the present invention provides an emergency response coping training apparatus and method for deploying a parachute in case the main parachute is not deployed properly during deployment of the parachute.

The problems of the present invention are not limited to the above-mentioned problems, and other problems not mentioned can be clearly understood by those skilled in the art from the following description.

According to an aspect of the present invention, there is provided an emergency response coping training apparatus including a support unit, a parachute unit, a first sensor, and a control unit.

The support portion is installed so as to have an initial state parallel to the installation surface.

The parachute unit includes a harness to be worn on the body of a trainee and a plurality of connecting strings connecting the harness and the support to each other to suspend the trainee to the support.

The first sensor is installed in the connection string, and when performing the operation of releasing the twisted connection string, the first sensor senses the degree of performance.

The control unit determines whether the connection string is released according to a value input from the first sensor. This allows training to twist the connecting string.

More specifically, when the value input from the first sensor is equal to or greater than a predetermined value, the controller determines that the trainer releases the connection string and unfolds the main parachute. If the value input from the first sensor is greater than a preset value , It is determined that the trainer has failed to deploy the main chute, and the preliminary parachute deployment signal can be output.

For example, the first sensor may measure a compressive force or a tensile force applied to the connection string and transmit the measurement result to the controller.

Alternatively, the first sensor may measure the distance between adjacent connection strings and transmit the measured distance to the controller.

The harness may be provided with a preliminary parachute knob, and the preliminary parachute knob may be provided with a second sensor for detecting whether the preliminary parachute knob is detached. The control unit may determine whether the preliminary parachute deployment signal is developed according to the value input from the second sensor after the preliminary parachute deployment signal is output.

Meanwhile, the emergency response coping training method according to an embodiment of the present invention includes a preparation step, a main parachute re-deployment step, and a main parachute re-deployment determination step.

In the preparation step, the trainer wears a harness and lifts the support portion in a state where the trainer is connected to the support portion by the connection string, floats the trainee, and judges the state in which the connection string is twisted as an initial state.

In the main parachute re-development step, the trainer pulls the connecting string or changes the positions of the plurality of connecting strings to perform the operation of releasing the connecting string.

In the main parachute re-deployment determination step, the distance between the adjacent string strings is measured by a tensile force applied to the connecting string by the trainee in the main parachute re-deployment step. If the measured value is greater than a preset value, It can be decided that it has been developed and the training can be terminated. On the other hand, if the measured value is less than the predetermined value, it is determined that the main parachute deployment has failed and a preliminary parachute deployment signal is output.

The emergency response coping training method of the present embodiment may further include a preliminary parachute deployment step and a preliminary parachute deployment determination step.

In the preliminary parachute deployment step, when the preliminary parachute deployment signal is outputted in the main parachute deployment determination step, the trainee can pull the preliminary parachute handle to perform the preliminary deployment.

In the preliminary parachute deployment determination step, it may be determined whether or not the preliminary parachute deployment is developed depending on whether the trainer has properly separated the preliminary parachute handle in the preliminary parachute deployment stage.

The effects of the present invention will be described below.

First, according to an emergency response coping training apparatus and method according to an embodiment of the present invention, a first sensor provided in a connecting string senses the extent to which a trainer performs an operation of releasing a twisted connecting string, By comparing the input value with the predetermined value, it is possible to determine whether the trainer has performed the operation of releasing the connection string properly, thereby coping with the twist of the connecting string during the deployment of the parachute, so that the emergency response training can be performed so that the main parachute can be normally deployed.

Second, according to the emergency response coping training apparatus and method according to an embodiment of the present invention, the second sensor provided in the preliminary parachute handle senses the extent to which the trainee performs the preliminary parachute deployment operation, It is possible to determine whether or not the trainee has successfully performed the preliminary parachute deployment operation by comparing the preliminary parachute deployment value with the predefined value so that the emergency parachute deployment training can be performed when the main parachute is not properly deployed during the parachute deployment.

The effects of the present invention are not limited to the effects mentioned above, and other effects not mentioned can be clearly understood by those skilled in the art from the description of the claims.

The foregoing summary, as well as the detailed description of the preferred embodiments of the present application set forth below, may be better understood when read in conjunction with the appended drawings. For the purpose of illustrating the invention, there are shown preferred embodiments in the figures. It should be understood, however, that this application is not limited to the precise arrangements and instrumentalities shown.
FIG. 1 is a view showing a trainer performing training to solve a connection string in an emergency response coping training apparatus according to an embodiment of the present invention;
2 is a view showing a trainee performing a preliminary parachute deployment training in an emergency response coping training apparatus according to an embodiment of the present invention; And
3 is a flowchart illustrating an emergency response coping training method according to an embodiment of the present invention.

Hereinafter, embodiments of the present invention will be described in detail with reference to the accompanying drawings. It is to be understood, however, that the appended drawings illustrate the present invention in order to more easily explain the present invention, and the scope of the present invention is not limited thereto. You will know.

In describing the embodiments of the present invention, it is to be noted that elements having the same function are denoted by the same names and numerals, but are substantially not identical to elements of the prior art.

Also, the terms used in the present application are used only to describe certain embodiments and are not intended to limit the present invention. The singular expressions include plural expressions unless the context clearly dictates otherwise. In the present application, the terms "comprises" or "having" and the like are used to specify that there is a feature, a number, a step, an operation, an element, a component or a combination thereof described in the specification, But do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, or combinations thereof.

Hereinafter, an emergency response coping training apparatus according to an embodiment of the present invention will be described with reference to FIGS. 1 and 2. FIG.

FIG. 1 is a view showing a trainee 10 performing training to solve a connection string in an emergency response coping training apparatus according to an embodiment of the present invention. FIG. 2 is a view showing an emergency response coping training FIG. 10 is a view showing a trainer 10 performing a preliminary parachute deployment training in the apparatus.

1 and 2, an emergency response coping and training apparatus according to an embodiment of the present invention includes a support frame 110, a driving unit 120, a support unit 130, a parachute unit 140, a first sensor 152, a second sensor 154, and a control unit 156.

The supporting frame 110 is a component that is fixed to the mounting surface and supports other components on the mounting surface. In this embodiment, the supporting frame 110 includes a pair of vertical frames 112, And a horizontal frame 114 disposed between the frame 112 and the horizontal frame 114.

The driving unit 120 is disposed between the horizontal frame 114 and the supporting unit 130 and controls the inclination and elevation of the supporting unit 130 according to a signal output from the control unit 156. [

In general, the driving unit 120 is a device that gives the trainee 10 an actual experience sense in a situation in which the driving unit 120 is in a state of being created. The driving unit 120 is tilted or moved up and down to cause the trainee 10 to actually race a car, You can experience the same thing. For this purpose, operations that can be perceived when actually riding a car or when riding in a fighter plane are implemented using mechanical degrees of freedom. The driving force for driving the driving unit 120 may be a hydraulic pressure, an electric motor, or a pneumatic pressure.

Specifically, the driving unit 120 of the present embodiment transmits a human response similar to an emergency situation such as deployment of a preliminary parachute or the like to the trainee 10 when the connecting string 144 is not properly released during deployment of the main parachute. In this embodiment, the driving unit 120 is a motion base comprising six actuators 122, and is connected to the horizontal frame 114 such that the tip of the actuator 122 connected to the supporting unit 130 faces downward. Respectively. The side surface of the horizontal frame 114 is stably supported by the outer frame 110.

The six actuators 122 are configured such that the two ends of the six actuators 122 are connected to each other so that the bottom ends of the six actuators 122 are connected to the horizontal frame 114, The tip ends of the three sets of actuators 122 are connected to three points of the supporter 130 by a hinge axis.

However, the present invention is not limited thereto. For example, the four-axis, eight-axis, and nine-axis drive driving units 120 may be applied to the present invention. Since the driving unit 120 is a publicly known technique in general, the detailed description of the configuration will be omitted.

The support part 130 is installed in the horizontal frame 114 by the driving part 120 so as to be parallel to the installation surface in the initial state. The tilting and elevation of the support part 130 are controlled by the driving part 120 so that the human body similar to the actual emergency situation can be delivered to the trainee 10 by the operation of the driving part 120. [ Although the front view of the supporting part 130 is shown in the drawing of the present embodiment, the shape of the supporting part 130 may be variously formed such as a triangular, square, hexagonal, etc. square or circular shape.

The parachute unit 140 includes a harness 142 and a plurality of connecting strings 144. The harness 142 is worn on the body of the trainee 10 to connect the trainee 10 to the parachute. The connecting string 144 connects the harness 142 to the parachute so that the trainer 10 can be connected to the parachute. In this embodiment, the connecting string 144 is connected at one end to the supporting portion 130, And the other end is connected to the harness 142 so that the trainee 10 can hang on the support portion 130. The connecting strings 144 are generally placed before, after, left, and right of the trainer 10, respectively. At this time, the connecting string 144 may be a parachute riser. The number and position of the connecting strings 144 are not limited to those described above and can be arranged without regard to the number of the connecting strings 144 if they can stably support the trainee 10.

Accordingly, the operation of the driving unit 120 is transmitted to the trainee 10 through the supporting string 130 and the harness 142 via the connecting string 144 and the trainee 10, It can be performed realistically on the ground.

At least one first sensor 152 may be provided for each of the plurality of connecting strings 144. The first sensor 152 senses the degree of performance when the trainer 10 performs an operation of untwisting the twisted connection string 144. [

For example, as the first sensor 152, a tensile force measuring sensor may be applied. In order to release the connection string 144, the connection string 144 must be pulled strongly. Accordingly, the first sensor 152, which is a tensile force measuring sensor, can measure the tensile force applied by the trainee 10 to the connecting string 144 and output the measured value to the control unit 156.

Alternatively, as the first sensor 152, a distance measuring sensor may be applied. If the connecting strings 144 are twisted, the distance between the adjacent connecting strings 144 is very close, but in a normal state where the connecting strings 144 are not twisted, a certain distance may be secured between the adjacent connecting strings 144 . Therefore, the first sensor 152, which is a distance measuring sensor, measures the distance between adjacent connecting strings 144 and outputs the measured value to the controller 156.

Alternatively, both the tension measuring sensor and the distance measuring sensor may be applied to the first sensor 152.

The control unit 156 determines whether the connection string 144 is released according to the value input from the first sensor 152.

For example, if the measured value inputted from the first sensor 152, that is, the tensile force applied to the connecting string 144 or the distance between adjacent connecting strings 144 is equal to or greater than a predetermined value, ) Loosens the twisted connection string 144 and correctly deploys the main parachute.

On the other hand, if the measured value input from the first sensor 152 is less than a predetermined value, the controller 156 may determine that the trainer 10 failed to unfold the twisted connection string 144 and fails to deploy the main chute . In this case, the control unit 156 can output the preliminary parachute deployment signal. The preliminary parachute deployment signal may be an auditory signal or a visual signal.

On the other hand, the parachute unit 140 may further include a preliminary parachute knob 146. The preliminary parachute knob 146 may be provided to be connected to the harness 142 and the preliminary parachute handle 146 may be located at the top of the chest of the trainer 10 in general.

The trainer 10 can perform the operation of deploying the preliminary parachute by pulling the preliminary parachute knob 146 when the preliminary parachute deployment signal is outputted. Here, when the trainee 10 performs the preliminary parachute deployment operation, the preliminary parachute knob 146 may be provided with a second sensor 154 for detecting whether the preliminary parachute knob 146 is detached.

For example, the second sensor 154 may be a button switch or a magnet switch. (Not shown) in which one side of the preliminary parachute knob 146 is inserted when the button switch is applied, and whether or not the preliminary parachute knob 146 is detached is detected on the inside of the holder can do. In the case where the magnet switch is applied, magnets are provided on the inside of the holder (not shown) and the portions of the preliminary parachute knob 146 that are in contact with each other to detect whether or not the preliminary parachute knob 146 is detached . The control unit 156 can determine whether the preliminary parachute is properly deployed according to whether or not the preliminary parachute knob 146 input from the second sensor 154 is detached. That is, if the preliminary parachute knob 146 is disengaged, it is determined that the preliminary parachute is deployed. If the preliminary parachute knob 146 is not removed, it can be determined that the preliminary parachute is not deployed.

Alternatively, a tension sensor may be used as the second sensor 154. To deploy the reserve parachute, the reserve parachute handle 146 must be strongly pulled. Accordingly, the second sensor 154, which is a tensile force measuring sensor, can measure the tensile force applied by the trainee 10 to the preliminary parachute knob 146 and output the measured value to the control unit 156. Alternatively, as the second sensor 154, a distance measuring sensor may be applied. Before the preliminary parachute knob 146 is pulled, the preliminary parachute knob 146 is located very close to the body of the trainer 10, but when the preliminary parachute knob 146 is pulled so that the preliminary parachute is deployed, (10) is distanced beyond a certain distance. Therefore, the second sensor 154, which is a distance measuring sensor, measures the distance between the preliminary parachute knob 146 and the body of the trainee 10 and outputs the measured value to the control unit 156.

The control unit 156 determines whether the value inputted from the second sensor 154 after the preliminary parachute deployment signal is outputted or the tension applied to the preliminary parachute knob 146 or the preliminary parachute knob 146 and the body of the trainer 10 It is possible to determine whether or not the preliminary parachute knob 146 has been removed. For example, the control unit 156 determines that the preliminary parachute knob 146 is disconnected by the trainee 10 when the measured value input from the second sensor 154 is equal to or greater than a preset value, The trainer 10 can determine that the preliminary parachute knob 146 has not been disconnected.

The emergency escape training apparatus of the present embodiment may further include a simulation image reproducing unit 160 for enhancing the realism. Here, the simulation image reproducing unit 160 may include a virtual reality (VR), a goggle with a built-in monitor, a large screen provided on the front of the trainee 10, or a plurality of monitors surrounding the trainee 10. This gives the trainee 10 the same sense of presence as training in actual highs.

The simulation image reproducing unit 160 may be electrically connected to the controller 156 to reproduce an image according to the training condition. When a signal suitable for an image reproduced from an external input device is inputted, an image corresponding to the input signal can be reproduced.

For example, at the time of training using the emergency response coping training apparatus of the present embodiment, the simulation image reproducing unit 160 can reproduce a falling image by failing to deploy the main parachute.

At this time, when the trainer 10 pulls the connection string 144 or adjusts the position thereof, the signal is inputted to the control unit 156 by the first sensor 152, and the control unit 156, according to the input signal, If the connection string 144 is released and the main parachute is properly deployed, the simulation image playback unit 160 can play back the main deployed video image. On the other hand, when the control unit 156 determines that the main parachute has not been properly deployed, the simulation image playback unit 160 can play back the video that continues to fall.

Here, the simulation image reproducing unit 160 may be coupled to the driving unit 120 by the control unit 156, and the driving unit 120 may transmit vibration, shock, tilt, and the like corresponding to the simulation image to the trainee.

The emergency response coping training apparatus according to an embodiment of the present invention has been described above.

Hereinafter, an emergency response coping training method according to an embodiment of the present invention will be described with reference to FIG.

3 is a flowchart illustrating an emergency response coping training method according to an embodiment of the present invention.

The emergency response coping training method of the present embodiment is performed by using the simulation image reproducing unit 160. Here, the simulation image reproducing unit 160 may be applied to a VR (virtual reality), a goggle with a built-in monitor, or the like. 3, the emergency response coping training method according to an embodiment of the present invention includes a preparatory step S110, a main parachute deployment determination step S120, a main parachute re-deployment step S130, Determination step S140, a preliminary parachute deployment step S210, and a preliminary parachute deployment determination step S220.

In the preparation step S110, the trainer 10 wears the harness 142 and lifts the support part 130 in a state where the support string 130 is connected to the support part 130 by the connection string 144, so that the trainee 10 can be raised. Although not shown in the drawings, in the preparation step, an image such as a trainee 10 deploying a parachute can be reproduced.

In the main parachute deployment determination step (S120), an image succeeding to the main parachute deployment may be reproduced, or an image in which the connection string 144 is twisted or the connection string 144 is caught in the main parachute and the parachute deployment fails may be reproduced . In the main parachute deployment determination step S120, the trainee 10 can determine whether or not the main parachute is properly deployed in the image.

If it is determined in step S120 that the main parachute is not properly deployed in the main parachute deployment step S130, the trainee 10 floats in the air and is connected to the support part 130 by the connection string 144 It is possible to perform an operation of pulling the connecting string 144 or changing the positions of the plurality of connecting strings 144 to loosen the connecting string 144 (see FIG. 1).

In the main parachute re-deployment determining step S140, the distance between the connecting string 144 and the tensile force applied to the connecting string 144 by the trainee 10 in the main parachute re-deployment step S130 is measured, It is judged that the main parachute has been developed, so that the main parachute can reproduce the properly developed image and terminate the training.

If the measured value is less than the predetermined value, it is determined that the main parachute expansion has failed and the preliminary parachute expansion signal can be outputted.

When the preliminary parachute deployment signal is output in the main parachute re-deployment determination step (S140), the trainee 10 can perform the preliminary parachute deployment step S210 in which the preliminary parachute knob 146 is pulled to expand the preliminary parachute 2).

In the preliminary parachute deployment determination step S220, when the trainee 10 pulls the preliminary parachute knob 146 in the preliminary parachute deployment step S210, it is detected whether or not the preliminary parachute knob 146 is detached, When the handle 146 is detached, it is judged that the preliminary parachute has been deployed, so that the image of the preliminary parachute can be reproduced properly and the training can be terminated.

Alternatively, in the preliminary parachute deployment determination step S220, a tensile force applied to the preliminary parachute knob 146 by the trainee 10 in the preliminary parachute deployment step S210 or the tension applied to the preliminary parachute handle 146 and the body of the trainer 10 Can be measured. Here, if the measured value is equal to or greater than a predetermined value, it is determined that the preliminary parachute is deployed, and the video with the preliminary parachute developed properly can be reproduced and the training can be terminated.

On the other hand, if the preliminary parachute knob 146 is not detached or if the measured value is less than the predetermined value, it is determined that the preliminary parachute has not been deployed, and the trainer 10 can repeat the preliminary parachute deployment step S210 again.

It will be apparent to those skilled in the art that the present invention can be embodied in other specific forms without departing from the spirit or scope of the invention as defined in the appended claims. It is obvious to them. Therefore, the above-described embodiments are to be considered as illustrative rather than restrictive, and the present invention is not limited to the above description, but may be modified within the scope of the appended claims and equivalents thereof.

10: trainer 110: support frame
112: vertical frame 114: horizontal frame
120: driving part 122: actuator
130: Support part 140: Parachute unit
142: harness 144: connecting string
146: Preliminary parachute handle 152: First sensor
154: second sensor 156:
160:

Claims (7)

A support having an initial state parallel to the mounting surface;
A parachute unit comprising a harness to be worn on the body of a trainee and a plurality of connecting strings connecting the harness and the support to each other to suspend the trainee to the support;
A preliminary parachute handle provided on the harness;
A first sensor installed in the connecting string to detect the degree of performance when the trainer performs an operation of releasing the connecting string;
A second sensor provided on the preliminary parachute handle to detect whether the preliminary parachute handle is detached; And
If the value inputted from the first sensor is equal to or greater than a predetermined value, it is determined that the trainer releases the connection string and unfolds the main parachute, and if the value input from the first sensor is less than a preset value, A control unit for outputting a preliminary parachute deployment signal after determining that the preliminary parachute deployment signal has not been expanded and determining whether the preliminary parachute deployment is developed according to the value input from the second sensor after the preliminary parachute deployment signal is outputted;
Emergency response trainers that can be trained to deal with emergencies in which the main parachute is not deployed properly.
delete The method according to claim 1,
Wherein the first sensor measures a compressive force or a tensile force applied to the connection string and transmits the measurement result to the controller.
The method according to claim 1,
Wherein the first sensor measures the distance between the adjacent strings and transmits the measured distance to the controller.
delete In an emergency situation coping training method using a simulation image reproducing unit,
A preparation step of lifting the trainee by raising the support part while the trainee wears the harness and is connected to the support part by the connection string;
A main parachute expansion determining step of determining whether the main parachute is properly developed in the simulation image of the trainee;
A main parachute development step of performing an operation of pulling the connecting string or changing a position of the plurality of connecting strings to untie the connecting string when the main parachute is not properly deployed in the main parachute deployment determination step ;

A tension is applied to the connecting string by the trainee in the main parachute expansion step or a distance between adjacent connecting strings is measured. If the measured value is greater than a predetermined value, it is determined that the main parachute has been deployed and the training is terminated Determining if the measurement value is less than a predetermined value, and outputting a preliminary parachute deployment signal when it is determined that the main parachute deployment has failed;
A preliminary parachute deployment step of performing a preliminary parachute deployment operation by the trainee pulling the preliminary parachute handle when the preliminary parachute deployment signal is outputted in the main parachute re-deployment determination step; And
A preliminary parachute deployment determination step of determining whether or not the preliminary parachute is deployed according to whether the trainee properly dismounts the preliminary parachute handle in the preliminary parachute deployment step; And an emergency response coping training method.
delete
KR1020160136625A 2016-10-20 2016-10-20 Training Apparatus and Method for Emergency in Deploying Parachute KR101882226B1 (en)

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KR1020160136625A KR101882226B1 (en) 2016-10-20 2016-10-20 Training Apparatus and Method for Emergency in Deploying Parachute
PCT/KR2016/011879 WO2018074635A1 (en) 2016-10-20 2016-10-21 Training apparatus and method for responding to emergency during parachute deployment

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CN112591109B (en) * 2020-12-22 2024-04-16 长沙理工大学 Parachuting whole-course simulation training platform

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101473291B1 (en) * 2013-04-24 2014-12-16 주식회사 에이스카이 Parachute training simulator with human induce effect

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH08244691A (en) * 1995-03-09 1996-09-24 Ishikawajima Harima Heavy Ind Co Ltd Simulator for parachute manufacturing training
KR101230192B1 (en) * 2011-03-23 2013-02-27 염도호 A Parachute Descent Training Simulation System and Method of The Same
KR20150087043A (en) * 2014-01-21 2015-07-29 대우조선해양 주식회사 Apparatus for cable twist detecting and method thereof
KR101551827B1 (en) * 2014-02-14 2015-09-11 에이에프티코리아 주식회사 Air-borne simulation apparatus

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR101473291B1 (en) * 2013-04-24 2014-12-16 주식회사 에이스카이 Parachute training simulator with human induce effect

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