KR100833982B1 - Lifestyle exchange equipments connecting line for aviation pilot - Google Patents

Abstract

A survival equipment connection wire for an aviation pilot is provided to attenuate impact applied to the pilot and to prevent the survival equipment connection wire from being broken. A survival equipment connection wire for an aviation pilot includes a first fixing part(140), a second fixing part(141), a third fixing part(240), a first attachment part(130), and a second attachment part(131). The first fixing part is fixed to one side of the survival equipment connection wire. The second fixing part is fixed to the other side of the survival equipment connection wire. The third fixing part is formed on one side of the connection wire to be connected to a life belt. The first attachment part and the second attachment part are attached to each other by stitches.

Description

Life Style Exchange Equipments Connecting Line for Aviation Pilot

1 is a block diagram showing a front injection seat of a general aircraft cockpit

Figure 2 is a perspective view showing a state connected to the live pilot equipment using the aviation pilot using the living room equipment box according to the prior art

Figure 3 is a block diagram showing a connecting line of a living pilot using a flight control according to a first embodiment of the present invention

Figure 4 is a block diagram showing a connecting line for a living pilot using the air pilot according to a second embodiment of the present invention

Figure 5 is a block diagram showing a connecting line for a living pilot using a flight control according to a third embodiment of the present invention

Figure 6 is a block diagram showing a connecting line for a living pilot using a pilot aircraft according to a fourth embodiment of the present invention

Figure 7 is a block diagram showing a connecting line of a living pilot using a flight control according to a fifth embodiment of the present invention

Figure 8 is a block diagram showing a live pilot tool connecting line using the air pilot according to a sixth embodiment of the present invention

Figure 9 is a block diagram showing a connecting line for a living pilot using the air pilot according to the seventh embodiment of the present invention

Figure 10 is a block diagram showing a connecting line for a living pilot using the air pilot according to the eighth preferred embodiment of the present invention

Figure 11 is a perspective view showing the arrowhead lug of the live connective ties used in the present invention

Figure 12 is a perspective view showing a state connected to the live test equipment connection box according to the present invention

Figure 13 is a use state showing the state that the mounting and detachment of the arrowhead lug of the head of the live connective device connection line according to the present invention

[Description of Code for Major Parts of Drawing]

6: left guide rail 10: sticker clip

50: live return box

110: arrow head lug or engaging member 111: engaging projection

113: connecting hole 115: coupling hole

120: connecting line living unit 130: the first binding portion

131: second binding portion 132: thread

140: first fixing portion 141: second fixing portion

142: fixing hole 150: luminous material

160: buffer member 240: third fixing portion

241: fixing hole 242: burst prevention

260: protective cover

BACKGROUND OF THE INVENTION 1. Field of the Invention [0001] The present invention relates to a survival kit connecting line (Lowering Line), and more particularly, to a pilot connecting live pilot device connecting pilot and pilot living equipment when an emergency escape of the aircraft.

In general, the aviation pilot's live rig connection line serves to connect the pilot's live rig box hidden behind the pilot and the cockpit when the pilot and the pilot are separated in an emergency escape of the aircraft.

In the emergency escape situation of the aircraft, the cockpit and the pilot are separated, and the vital device connection cord is unfolded at the moment, the other device operation line (beacon automatic operation line: PCB line, etc.) that is normally connected is pulled out and necessary for the pilot's rehabilitation. Start the equipment (Becon, etc.).

In addition, the internal contents of the living equipment box, which is normally mounted under the cockpit in an emergency escape situation of the aircraft, may be internally damaged even if the outer case is damaged or dislodged, regardless of whether the outer case of the soft case or the hard case is soft. It holds more to prevent the loss of contents when the pilot lands or sleeps.

1 is a block diagram showing a front injection seat of a general aircraft cockpit.

The front injection seat of the aircraft cockpit has a parachute stack (1), a left upper latch device (2), a left shoulder strap lug spring clip (3), a harness reel (4), and a left guide rail top, as shown in FIG. Mounting bracket (5), left guide rail (6), back pad (7), left shoulder strap (8), left crotch strap (9), sticky clip (10), tether connector (11), Left Lap Strap (12), Emergency Oxygen Manual Control Handle (13), Go-forward Control Handle (14), Left Guide Rail Lower Mounting Bracket (15), Rocket Motor (16) ), Comfort Pad, SAFE / ARMED Handle 18, V-Strap 19, Knuckle Knob 20 on Left Snubber Release Lever, Right Seat Igniter 21, Right The knuckle knob 22 of the snubber release lever, the injection steering wheel 23, the negative-g strap 24, the quick release box 25, the right shoulder strap 26, etc. are comprised.

The front injection seat with this configuration allows for quick escape from the fuselage of the plane with the pilot sitting in the cockpit in an emergency.

That is, when the aircraft enters an emergency during flight and the pilot operates the injection lever, the canopy that covers the cockpit (cockpit) of the aircraft is opened and at the same time the rocket motor 16 installed below the injection seat operates to eject the injection seat. To disengage from the cockpit of the aircraft. After the ejection seat is separated from the aircraft, the parachute installed in the pilot is unfolded while the pilot is released, and the pilot descends a certain speed by the parachute to escape. At this time, the pilot's body escaped from the aircraft is connected to the equipment connected to the pilot's life (Becon: beacon, etc.) connected to the life-changing equipment.

Figure 2 is a perspective view showing a state connected to the air pilot using the live pilot equipment linkage box according to the prior art.

As shown in FIG. 2, the conventional aviation pilot using live return device connection string 30 is fixed to one side of the arrow head lug 40 coupled to the sticker clip 10 of the cockpit, and a live return box (the other side) It is composed of a fixing portion 31 for connecting and fixing 50. At this time, the life-changing equipment box 50 is a lifeboat is stored on one side, the emergency food, emergency medicine, compasses, maps, pistols, etc. are stored on the other side that is necessary for living.

On the other hand, since the conventional flight pilot using the living ring connection string 30 having the configuration is composed of a line-shaped line, when the emergency escape from the aircraft dropping the live ring device box 50, the live ring device 30 There was a problem of giving a strong impact to the pilot by generating a strong tensile force through, and also because of the falling speed and weight of the living equipment box 50 there was a problem that the living equipment connection line 30 is broken.

In addition, the conventional live connection device 30 is not made of luminous material, so the rescue team could not quickly find a pilot in an emergency situation when the pilot escaped to the ground or the sea at night. In addition, it is difficult to quickly move to the lifeboat or lifejacket fixed to the living hook, because the pilot must find the hook at the night to find the living hook, and it is difficult to quickly find the box of the hook connected to the hook. There was a difficult problem.

In addition, the conventional live-changer connection line 30, when the pilot fell on the surface of the sea, river or lake, the live-changer connection line is immersed in water, so that the pilot in an emergency situation is quick It was hard to find.

Therefore, the present invention has been made to solve the above problems, and a first object of the present invention is to fold at least one or more live connection equipment connecting line to overlap and then to bind the overlapping parts with a seal between the pilot and the live recovery equipment box during emergency escape from the aircraft The present invention provides an air pilot connecting line that mitigates the impact transmitted to the pilot and prevents the live connecting line from being disconnected by releasing the bound portion of the thread when a strong tensile force is generated.

In addition, a second object of the present invention is to fold at least one or more places living hooks connected to overlap and then bound or bonded by using a plurality of shock absorbing members in the overlapped portion to ensure a strong connection between the pilot and the living equipment box during emergency escape from the aircraft When the tensile force is generated by the buffer member to be torn in sequence to alleviate the impact to mitigate the impact transmitted to the pilot, and to provide a live pilot equipment connecting line for preventing the disconnection of the live connector kit.

In addition, a third object of the present invention is to provide a living pilot connecting line using the flight control to include a luminous material in the live connecting device linkage to easily identify at night.

In addition, the fourth object of the present invention is to produce a live test equipment connecting line with buoyant material floating in the water when the emergency escape from the aircraft when the drop in the sea, river or lake, etc. The live test equipment used for the air pilot used to float without submerging in water To provide a connection line.

In addition, a fifth object of the present invention is to provide a living pilot connection line for the use of the air pilot is fixed to the lifeboat or lifeboat and the bioremoval equipment box is tied to the living ring kit used in the first to fourth purposes, respectively.

Aviation pilot use living ring device connecting line according to the present invention for achieving the above object, the arrow head lug 110 is configured on one side of the living ring device connecting line 120 and mounted on a sticker clip 10 installed on the side of the cockpit A first fixing part 140 fixed to and coupled to the first fixing part 140; A second fixing part 141 configured to be connected to the other side of the living ring device connection line 120 and fixed to the living ring device box 50; And at least one or more sides between the one side and the other side of the living unit connection line 120 and folded to overlap a predetermined length, and then bound the overlapped portions with the seal 132 so that the pilot and the living unit box at the time of emergency escape from the aircraft ( It characterized in that it comprises a; a binding portion for mitigating impact while the portion to which the binding is actually broken when the strong tensile force occurs between 50).

In addition, the aviation pilot use live ring device connecting line according to the present invention for achieving the above object, the arrow head lug is configured on one side of the live ring device connecting line 120 and mounted on a sticker clip 10 installed on the side of the cockpit ( A first fixing part 140 coupled to and fixed to the 110; A second fixing part 141 configured to be connected to the other side of the living ring device connecting line 120 and fixed by connecting the living box device 50; And at least one or more sides between the one side and the other side of the living unit connection line 120 and fold to overlap a predetermined length, and then bind the overlapped portions with a plurality of shock absorbing members 160 to rescue the pilot and the living body during emergency escape from the aircraft. Characterized in that it comprises a; binding portion to mitigate the impact while the shock absorbing member 160 is torn sequentially when a strong tensile force occurs between the gear box (50).

The live connective connection line 120 is characterized in that formed in a zigzag stitch when binding the overlapped portion with a thread.

The live connective device connecting line 120 is characterized in that the sewing through the live connective device connecting line from one side direction of the overlapped portion to the other side when the binding to the overlapped portion thread in the form of moxibustion.

The live connective device connection line 120 is configured on one side of the live connective device connection line 120, characterized in that further comprises a third fixing part 240 for fixing by connecting to the lifeboat or lifeboat.

The second fixing part 141 or the third fixing part 240 folds the living device connection line 120 to overlap a predetermined length, and then binds the overlapped parts to form a fixing hole 241 on one side. And it is characterized in that it is provided with a burst prevention portion 242 bound to the other side to prevent the bound yarn from being torn by the tensile force.

The burst prevention part 242 is characterized in that it is sewn with thread using a synthetic fiber or cloth material.

The buffer member is characterized in that composed of an elastic material.

The buffer member is characterized in that composed of PVC.

One side of the first fixing part 140 is characterized in that it is further provided with a protective cover 260 surrounding the outside to protect the live connective hook.

The live connective device connection line 120 is characterized in that all or part of the dyeing with luminous material.

The live connective device connection line 120 is characterized in that the whole or part of the painting with luminous material.

The live ring connection line 120 is characterized in that it is manufactured using a buoyancy material.

The live ring connection line 120 is characterized in that manufactured using a luminous material.

The live ring connection line 120 is characterized in that manufactured using a luminous material and buoyancy material.

The live connective device connection line 120 is characterized by consisting of a fluorescent color, including white, orange, red, yellow.

Therefore, at least one live line connection cord is folded to overlap and then the overlapped portion is bound with a seal or a cushioning member so that when a strong tension force occurs between the pilot and the live return box during an emergency escape from the aircraft, By sequential tearing of the parts, the shock can be prevented from breaking, as well as the impact on the pilot.

Hereinafter, embodiments of the present invention will be described in more detail with reference to the accompanying drawings.

First embodiment

Figure 3 is a block diagram showing a connecting line of a living pilot using the air pilot according to a first embodiment of the present invention.

As shown in FIG. 3, the first pilot unit (not shown; see 140 of FIG. 4) may be used for connecting the pilot and the pilot's live return tool 50 during an emergency escape of the aircraft. The second fixing part 141, the first binding part 130, and the second binding part 131 are configured to be included.

The first fixing part 140 is fixed to the arrowhead lug 110 is configured on one side of the living hook connection string 120 and mounted on a sticker clip 10 installed on the side of the cockpit.

The second fixing part 141 is configured on the other side of the live connective device connection line 120 and is fixed to the live connective device box (50). At this time, the life-changing equipment box 50 is a lifeboat is stored on one side, the other side, emergency food, emergency medicine, compasses, maps, pistols, etc. are stored in the pilot necessary for rehabilitation.

The first and second binding parts 130 and 131 are configured between one side and the other side of the living device connecting line 120, and folded to overlap a predetermined length, and then the overlapping portion is bound with the thread 132. When the emergency escape from the aircraft when the strong tensile force occurs between the pilot and the life-changing gear box 50 is configured to mitigate the impact while the portion is actually broken by tearing sequentially.

The first fixing part 140 is fixed to the connection hole 113 of the arrowhead lug 110. The first fixing part 140 further includes a protective cover 260 made of a cloth material wrapped around the outside on one side to protect the live connection device 120 from being broken when the first body 140 is rubbed with the body of the aircraft.

The first and second fastening parts 130 and 131 are fastened so that the stitches are formed in a zigzag form, with the thread 131 being fastened to a portion where the live connective connection strings 120 overlap each other. At this time, the thread sewn in the form of a stitch is preferably sewed so as to be torn when a strong tensile force between the pilot and live return gear box during emergency escape.

The second fixing part 141 is tightly sewn so as not to be torn by the thread 131 overlapped with the living hook device connection line 120, the fixing hole, 142 to connect and fix the living equipment box 50 ).

Therefore, the air pilot using the life-changing device connecting line 120 according to the first embodiment having the above configuration, by folding at least one or more of the living ring and the connection line to overlap the actual overlapping portion to seal the pilot at the time of emergency escape from the aircraft When a strong tensile force occurs between the life-changing device box to loosen the impact of the part bound by the seal can be alleviated the impact transmitted to the pilot and can prevent the life-changing connection line 120 is broken.

Meanwhile, in the first embodiment of the present invention, the example in which the first and second binding parts 130 and 131 are configured in two has been described. However, two or more of the first and second binding parts 130 and 131 may be implemented as necessary.

Here, the live connective device connection line 120 is preferably composed of a fluorescent color including white, orange, red, yellow.

Second embodiment

Figure 4 is a block diagram showing a connecting line of a living pilot using the air pilot according to a second embodiment of the present invention.

As shown in FIG. 4, the first pilot part 140, the second anchoring part 141, and the third anchoring part 240 are used for the aviation pilot use live return device connection cord 120 according to the second embodiment of the present invention. , Including the first binding unit 130 and the second binding unit 131. According to the second embodiment of the present invention, the third fixing part 240 is additionally configured in the connecting line 120 for the aviation pilot use live return apparatus of the first embodiment.

The third fixing part 240 is configured on one side of the live connective device connecting line 120 and is fixed by connecting a lifeboat or lifejacket. As shown in FIG. 4, the third fixing part 240 folds the living device connecting line 120 to overlap a predetermined length, and then binds the overlapping part with a thread to form a fixing hole 241 at one side. It is provided with a burst prevention portion 242 bound to the other side to prevent the bound thread from being torn by the tensile force. At this time, the burst prevention part 242 is firmly sewn with a thread using a synthetic fiber material, for example.

Therefore, the air pilot using the life-changing tool connecting line 120 according to the second embodiment of the present invention is fixed by connecting the live-changing equipment box 50 to the second fixing part 141, the third fixing part 240 It can be fixed by attaching a lifeboat or a lifeboat.

Third and fourth embodiments

5 and 6 is a block diagram showing the connecting line of the living pilot using the air pilot according to the third and fourth preferred embodiments of the present invention.

According to the third and fourth embodiments of the present invention, as shown in FIG. 5 and FIG. 6, the aviation pilot using the live ring connector string is different from one side direction of the overlapped portions of the live ring connector string 120 to the other direction. It is sewn in the moxibustion through the live connection device connecting line. At this time, the thread sewn in the moxibustion form is preferably sewed so as to be torn when a strong tensile force between the pilot and the live return gear box during emergency escape.

Therefore, the aviation pilot use live ring device connecting line 120 according to the third and fourth embodiments of the present invention, when the emergency return connection line is folded at least one or more places and then overlap the overlapping part with a thread when emergency escape from the aircraft When a strong tensile force occurs between the pilot and the life-changing box, the portion bound to the thread is torn off to mitigate the impact to mitigate the impact transmitted to the pilot and the live-changing device connecting line 120 can be prevented from breaking.

5th and 6th embodiment

7 and 8 is a block diagram showing the connecting line of the live pilot using the air pilot according to the fifth and sixth preferred embodiment of the present invention.

According to the fifth and sixth embodiments of the present invention, as shown in FIGS. 7 and 8, the aviation pilot use live return device connection cord has a luminous material 150 dyed or painted on a part of the live return connector linkage 120. It is configured to include.

On the other hand, in the present invention, the luminous material 150 may be configured by dyeing or painting the whole of the live connective device connecting line 120.

Therefore, since the living pilot connecting string according to the fifth and sixth embodiments of the present invention is configured to include the luminous material 150 in the living ring connecting string 120, it can be easily identified at night.

Seventh embodiment

Figure 9 is a block diagram showing a connecting line of a living pilot using the air pilot according to the seventh embodiment of the present invention.

As shown in FIG. 9, the aviation pilot use live return device connection cord according to the seventh embodiment of the present invention is configured at one side of the live return connector linkage 120 and mounted on a sticker clip 10 installed at the side of the cockpit. The first fixing part 140 is coupled to the arrow head lug 110 and fixed, and the second fixing part 141 which is configured at the other side of the living connector connecting line 120 and connects and fixes the living connector box 50. ), And between the one side and the other side of the live connection device connecting line 120 and folded to overlap a predetermined length and then bound to the overlapping portion with a plurality of shock absorbing member 160 in the emergency escape from the aircraft pilot and living equipment When the strong tensile force occurs between the box 50 is configured to include the first and second binding portions 130, 131 to mitigate the shock while the buffer member 160 is torn in sequence.

At this time, the shock absorbing member 160 is preferably composed of an elastic material or PVC, which is torn by the falling speed and weight of the biological return box 50 when a strong tensile force occurs between the pilot and the biological return device box (50). Do.

Therefore, the aviation pilot using the live ring device connecting line 120 according to the seventh embodiment having the above configuration, by folding at least one or more of the live ring device connecting line to overlap the overlapping portion by the buffer member 160 to the aircraft In the emergency escape at the time when a strong tensile force between the pilot and the life-changing box, the shock absorbing member 160 is torn off to mitigate the impact to reduce the impact transmitted to the pilot and the life-changing connection line 120 is broken Can be prevented.

Meanwhile, in the seventh embodiment of the present invention, an example in which the first and second binding parts 130 and 131 are configured in two has been described. However, two or more of the first and second binding parts 130 and 131 may be implemented as necessary.

Eighth embodiment

10 is a block diagram showing the connection line of the living pilot using the air pilot according to the eighth preferred embodiment of the present invention.

As shown in FIG. 10, the first pilot part 140, the second anchor part 141, and the third anchor part 240 are used for the aerial pilot's live return device connection cord 120 according to the eighth embodiment of the present invention. , Including the first binding unit 130 and the second binding unit 131. In the eighth exemplary embodiment of the present invention, the third fixing part 240 is additionally configured in the live pilot tool connecting line 120 of the seventh exemplary embodiment.

The third fixing part 240 is configured on one side of the live connective device connecting line 120 and is fixed by connecting a lifeboat or lifejacket. As shown in FIG. 10, the third fixing part 240 folds the living device connecting line 120 to overlap a predetermined length, and then binds the overlapped parts to form a fixing hole 241 at one side. It is provided with a burst prevention portion 242 bound to the other side to prevent the bound yarn from being torn off by the tensile force. At this time, the burst prevention part 242 is firmly sewn with a thread using a synthetic fiber material, for example.

Accordingly, the live pilot tool connection line 120 using the aviation pilot according to the eighth embodiment of the present invention is fixed by connecting the live switch box 50 to the second fixing part 141, and the third fixing part 240. It can be fixed by attaching a lifeboat or a lifeboat.

9th embodiment

The aviation pilot use live ring device connecting line 120 according to the ninth embodiment of the present invention is manufactured by using the buoyant material (or buoyancy material) floating in the water in the living ring device connection line 120.

Therefore, when the live escape gear is manufactured by buoyancy material, when the emergency escape from the aircraft, such as when falling on the sea, river or lake, the live return device can be easily found in the night because the connection line floats on the water without submerging in water.

10th embodiment

Aviation pilot-operated living ring device connecting line 120 according to the tenth embodiment of the present invention is configured by manufacturing the living ring device connecting line 120 using a luminous material.

Therefore, since the live intestine connection line is made of luminous material, the live intestine connection line can be easily found even at night.

Eleventh embodiment

Aviation pilot-operated living ring device connecting line 120 according to the eleventh embodiment of the present invention is configured by using the luminous material and buoyancy material 120.

Therefore, when the live return line is composed of luminous material and buoyant material, when the emergency escape from the aircraft falls to the sea, river or lake, the live return line is not only submerged in water but also floats on the surface of the water and is luminous material. It is easy to find the live connective cord.

Arrowhead Lug of the Linkage

11 is a perspective view showing the arrowhead lug 110 of the live connective device connection line 120 used in the present invention.

The arrowhead lug 110, as shown in Figure 11, is formed of a cross-shaped clamp having a predetermined thickness, one side is formed with a coupling hole 115 in the inner side in the shape of an oval beam, the center portion is Two connection holes 113 are formed to fix the living ring connector connecting line 120, and the coupling protrusion 111 is connected to the pilot at the other side. At this time, the side of the arrow head lug 110, the coupling hole 115 is formed is mounted on the sticker clip 10 installed on the side of the cockpit.

Figure 12 is a perspective view showing the state connected to the live ring device 120 of the living ring device according to the present invention, 50, Figure 13 is the arrow head lug 110 of the live ring device connection line 120 according to the present invention It is a state diagram used to show the mounting and detachment to the clip (10).

The living unit tool box 50 connected to the living unit connection line 120 is loaded in the interior (bottom) of the seat of the cockpit, the lifeboat is stored on one side and the emergency food, emergency medicine, compass, on the other side, Maps, pistols, etc. are stored for the pilot's life.

The arrowhead lug 110 of the live connective device connection line 120 is mounted / removed to the ejection seat sticker clip 10 of the aircraft, thereby connecting the live test equipment box 50 and the pilot.

On the other hand, the live connective connection line 120 used in the present invention is composed of a fluorescent color, such as white, orange or red or luminous material to improve the visibility to search the rescue team's search conditions to quickly find the pilot in an emergency situation There is a characteristic to enhance.

In addition, the live connective connection line 120 must withstand a temporary load (for example, 600 to 1500p) when detached from the ejected seat.

In addition, when the seat is ejected, the live connector cable is separated from the seat and connected to the pilot, so that the pilot, cockpit, and the live connector cable do not collide with each other. In order to prevent the impact, the speed of the live connector cord is folded by folding the live connector cord with a stitch or other type of joint once or several times. And adjust the load.

In addition, the rubber ring should be able to move only when a constant load is applied without easily passing through or leaving the position.

In addition, the arrowhead lug 110 portion should not be easily corroded or damaged by water, moisture, temperature changes, and the like.

As described above, specific embodiments of the present invention have been described in detail, but those skilled in the art will appreciate that various changes and modifications can be made without departing from the scope of the present invention. Therefore, the scope of the present invention should not be limited to the above-described embodiments, but should be determined not only by the claims below but also by the equivalents of the claims.

As described above, according to the air pilot using the live test equipment linkage according to the present invention, at least one or more of the live test equipment connection line is folded to overlap, and then the overlapping portion is bound with a seal to ensure a strong connection between the pilot and the live test equipment box during an emergency escape from the aircraft When the tensile force is generated, the thread-bound portion is torn off to alleviate the impact, thereby reducing the impact on the pilot and preventing the live-intestinal connection line from breaking.

In addition, by folding at least one live line connecting line overlapping at least one place and then binding or binding by using a plurality of buffer members in the overlapped portion to bind the buffer when a strong tensile force between the pilot and the live intestine box during emergency escape from the aircraft By alleviating the impact as the members are torn in sequence, the impact to the pilot can be mitigated and the live linkage can be prevented from breaking.

In addition, the inclusion of the luminous material in the living ring connection line can be easily identified even at night, and produced a living ring connection line with buoyant material floating in the water when the emergency escape from the aircraft dropped to the sea, river or lake, etc. By floating without locking, there is an advantage that you can easily find the live connective line.

Claims (16)

In the aviation pilot using live return line, A first fixing part (140) configured to be coupled to the arrowhead lug (110) mounted on one side of the living ring connector string (120) and mounted on a sticker clip (10) installed at a side of a cockpit; A second fixing part 141 configured to be connected to the other side of the living ring device connection line 120 and fixed to the living ring device box 50; And At least one between the side and the other side of the living unit connection line 120 is folded and folded to a predetermined length and then bound to the overlapping portion with the seal 132 pilot and live equipment box when exiting the aircraft 50 When a strong tensile force occurs between) the binding portion to the sequential tearing of the binding portion to relieve the impact sequentially; aviation pilot using live connection equipment characterized in that it comprises a. In the aviation pilot using live return line, A first fixing part (140) configured to be coupled to the arrowhead lug (110) mounted on one side of the living ring connector string (120) and mounted on a sticker clip (10) installed at a side of a cockpit; A second fixing part 141 configured to be connected to the other side of the living ring device connecting line 120 and fixed by connecting the living box device 50; And At least one or more sides between the side and the other side of the living unit connection line 120 is folded to a certain length and then overlap the overlapping portion with a plurality of buffer members 160 when the emergency escape from the aircraft pilot and living equipment When the strong tensile force occurs between the box 50, the buffer member 160 is torn off sequentially, the binding portion to mitigate the impact; Aviation pilot using live intestine connection line comprising a. According to claim 1, wherein the live connective line 120 is: When connecting the overlapped portion with a thread aviation pilot use live return gear, characterized in that formed in a zigzag stitch. According to claim 1, wherein the live connective line 120 is: When the superimposed portion of the overlapping thread seals through the living room ball connecting line from one side direction of the overlapping portion in the other direction from the side of the superimposed pilot using a living room equipment linkage. The method of claim 1 or 2, wherein the live connective cord 120 is: Combination line for the live pilot using the flight control, characterized in that further comprises a third fixing part 240 is configured on one side of the living ring connection line 120 and connected to the lifeboat or lifeboat. The method of claim 5, wherein The second fixing part 141 or the third fixing part 240 is: After folding the live connective connection line 120 to a certain length to overlap the fixed portion 241 to form a fixing hole 241 on one side is bound to the thread and bound to the other side to prevent the bound thread to be torn off by the tensile force Aviation pilot using live return device, characterized in that provided with a burst prevention portion (242). The method of claim 6, wherein the burst prevention portion 242 is: Live pilot equipment connection line for aviation piloting, characterized in that it is sewn with a synthetic fiber or cloth material. The method of claim 2, wherein the buffer member is: Aviation pilot use live return fittings characterized in that consisting of elastic material. The method of claim 2, wherein the buffer member is: Aviation pilot use live return equipment, characterized in that consisting of PVC. The method according to claim 1 or 2, One side of the first fixing portion 140, the air pilot using live return gear, characterized in that the protective cover 260 is further provided to surround the outside to protect the live connection device. The method of claim 1 or 2, wherein the live connective cord 120 is: Live pilot equipment connecting line, characterized in that all or part of the dyed with luminous material. The method of claim 1 or 2, wherein the live connective cord 120 is: Live pilot equipment leash for all or part of which is painted with luminous material. The method of claim 1 or 2, wherein the live connective cord 120 is: Live pilot equipment connecting line, characterized in that manufactured using buoyancy materials. The method of claim 1 or 2, wherein the live connective cord 120 is: Live pilot equipment connecting line, characterized in that manufactured by using the luminous material. The method of claim 1 or 2, wherein the live connective cord 120 is: Live pilot equipment connecting line, characterized in that manufactured using luminous and buoyant materials. According to claim 1, wherein the live connective line 120 is: Live pilot equipment connecting line for aviation piloting, characterized in that it consists of fluorescent colors including white, orange, red and yellow.

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