KR200169065Y1 - an fall preventing apparatus of an airplane - Google Patents
an fall preventing apparatus of an airplane Download PDFInfo
- Publication number
- KR200169065Y1 KR200169065Y1 KR2019990017141U KR19990017141U KR200169065Y1 KR 200169065 Y1 KR200169065 Y1 KR 200169065Y1 KR 2019990017141 U KR2019990017141 U KR 2019990017141U KR 19990017141 U KR19990017141 U KR 19990017141U KR 200169065 Y1 KR200169065 Y1 KR 200169065Y1
- Authority
- KR
- South Korea
- Prior art keywords
- plane
- airplane
- crash
- present
- fall prevention
- Prior art date
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
Abstract
본 고안은 비행기의 추락방지장치에 관한 것으로서, 비행기의 추락사고 발생시 동체내부에 내장된 기구(氣求)가 펼쳐짐으로써 충격을 완화시킴과 함께 안정성을 증가시킬 수 있도록 하는 비행기의 추락방지장치에 관한 것이다.The present invention relates to a fall prevention device of an airplane, and to a fall prevention device of the plane to reduce the impact and increase the stability by expanding the mechanism built into the fuselage in the event of a crash of the plane. will be.
본 고안에 따르면 비행기의 동체상부에 내장되어 추락사고 발생시 동체상단에 형성된 개구부(4)로 돌출되어 펼쳐질 수 있는 기구(10)와, 상기 기구(10)의 부양에 필요한 공기보다 가벼운 기체를 발생시키는 기체발생기(2)를 포함하여 구성된 것을 특징으로 하는 비행기의 추락방지장치가 제공된다.According to the present invention, the built-in upper body of the plane and the mechanism 10 that can be expanded to protrude into the opening (4) formed on the upper body in the event of a crash, and generates a lighter gas than the air required for the support of the instrument (10) Provided is a fall prevention apparatus for an airplane, comprising a gas generator (2).
Description
본 고안은 비행기의 추락방지장치에 관한 것으로서, 보다 상세하게는 비행기의 추락사고 발생시 동체내부에 내장된 기구(氣求)가 펼쳐짐으로써 충격을 완화시킴과 함께 안정성을 증가시킬 수 있도록 하는 비행기의 추락방지장치에 관한 것이다.The present invention relates to a fall prevention device of an airplane, and more specifically, the fall of the plane to reduce the impact and increase the stability by spreading the mechanism built into the fuselage in the event of a crash of the plane. It relates to a prevention device.
일반적으로, 비행기는 안전성이 매우 중요하기 때문에 장비가 고장나면 자동적으로 다른 장비로 교체될 수 있도록 되어 있고, 비행기가 파손된 경우에라도 비행을 계속할 수 있도록 동체구조가 손상허용성을 갖도록 제작되며, 비상착륙시 높은 감속도에도 견딜수 있도록 객석을 만든다. 그러나, 갑작스러운 기상악화나 기타의 이유등으로 비행기의 추락사고가 발생하게 되면 비행고도와 비행기무게 때문에 상기의 안전장치들이 효과적으로 기능을 발휘하지 못하여 인명피해가 큰 실정이다.In general, because the safety of the aircraft is very important, if the equipment breaks down, it can be automatically replaced with other equipment, and the fuselage structure is designed to allow damage in order to continue the flight even if the airplane is damaged. The seats are built to withstand high decelerations during landing. However, if a plane crash occurs due to sudden bad weather or other reasons, the above safety devices do not function effectively due to the flight altitude and the weight of the plane, causing a great loss of life.
또한, 근래에 들어서 비행기를 이용하는 승객들이 많아짐에 따라 그 안전성이 더욱 절실한 상황이지만, 비행기 추락사고에 대비한 안전장치는 미비한 실정이어서 대형참사의 위험이 높고 비행기 추락에 대한 승객들의 불안이 높다.In addition, in recent years, as the number of passengers using airplanes is more urgent, the safety situation is more urgent, but the safety device for the plane crash is inadequate, so the risk of catastrophic disaster is high and the passengers' anxiety about the plane crash is high.
본 고안은 전술한 바와 같은 문제점을 해결하기 위한 것으로서, 본 고안의 목적은 운행중인 비행기의 추락사고 발생시 동체상부에 내장된 기구가 펼쳐짐으로서 비행기의 안전성을 높이고 충격으로 인한 인명피해를 줄일 수 있도록 하는 비행기의 추락방지장치를 제공하는 것이다.The present invention is to solve the problems as described above, the purpose of the present invention is to expand the mechanism built in the upper part of the plane in the event of a crash of a running plane to increase the safety of the plane and to reduce the casualties due to impact It is to provide a fall prevention device of the plane.
도 1은 본 고안의 실시예에 따른 기구가 비행기의 동체내에 내장된 상태를 나타낸 도면.1 is a view showing a state in which the mechanism according to an embodiment of the present invention is embedded in the body of the airplane.
도 2는 본 고안의 실시예에 따른 추락사고 발생시 기구가 비행기의 동체외부로 펼쳐진 상태를 나타낸 도면.Figure 2 is a view showing a state in which the mechanism unfolded outside the fuselage of the plane when a crash occurs according to an embodiment of the present invention.
＜도면의 주요부분에 대한 부호의 설명><Explanation of symbols for main parts of the drawings>
2. 기체발생기 4. 개구부2. Gas Generator 4. Opening
10. 기구10. Appliance
본 고안에 따르면, 비행기의 동체상부에 내장되어 추락사고 발생시 동체상단에 형성된 개구부(4)로 돌출되어 펼쳐질 수 있는 기구(10)와, 상기 기구(10)의 부양에 필요한 공기보다 가벼운 기체를 발생시키는 기체발생기(2)를 포함하여 구성된 것을 특징으로 하는 비행기의 추락방지장치가 제공된다.According to the present invention, a mechanism (10) that is built in the upper body of the plane can be expanded to protrude into the opening (4) formed on the upper body when a crash occurs, and generates a lighter gas than the air required for the support of the device (10) Provided is a fall prevention device for an airplane comprising a gas generator (2).
이하, 본 고안의 바람직한 실시예를 첨부한 도면에 의거하여 설명하면 다음과 같다. 도 1은 본 고안의 실시예에 따른 기구가 비행기의 동체내에 내장된 상태를 나타낸 도면이고, 도 2는 본 고안의 실시예에 따른 추락사고 발생시 기구가 비행기의 동체외부로 펼쳐진 상태를 나타낸 도면이다.Hereinafter, described with reference to the accompanying drawings, preferred embodiments of the present invention is as follows. 1 is a view showing a state in which the mechanism according to an embodiment of the present invention is built in the body of the plane, Figure 2 is a view showing a state in which the mechanism is unfolded out of the body of the plane when a crash occurs according to an embodiment of the present invention. .
도 1와 도 2에 의하면, 비행기의 추락상황 발생시, 비행기의 추락상태를 감지하여 신호를 발생하는 추락감지센서의 신호 또는 조종사에 의한 수동조작에 의해서 비행기 동체의 상단부분에 구비된 개구부(4)가 열리게 되면 비행기 동체의 상측부분에 내장된 기구(10)가 외부로 펼치지게 된다.1 and 2, an opening 4 provided in the upper part of the aircraft body by manual operation by a pilot or a signal of a fall detection sensor that detects a crash state of the plane and generates a signal when a crash situation of the plane occurs When opened, the mechanism 10 embedded in the upper portion of the aircraft fuselage is unfolded to the outside.
이와 더불어, 상기 추락감지센서에서 발생된 신호 또는 조종사의 수동조작이 비행기 동체의 상측부분에 구비된 기체발생기(2)로 보내지게 되면 상기 기체발생기(2)에서 공기보다 가벼운 수소등의 기체를 발생하여 상기 기구(10)에 주입함으로써 순간적으로 에어백이 부풀어 오르듯이 상기 기구에 수소가 채워져 부풀어 올라 비행기에 양력이 작용될 수 있게 된다.In addition, when the signal generated by the fall detection sensor or the manual operation of the pilot is sent to the gas generator 2 provided in the upper portion of the aircraft body, the gas generator 2 generates gas such as hydrogen that is lighter than air. By injecting into the device 10 is instantaneously inflated as if the air bag is inflated by the hydrogen filled in the balloon can be lifted to act on the plane.
이와 같이 구성된 비행기의 추락방지장치는 비행기의 추락상황 발생시 비행기에 양력이 작용될 수 있는 기구를 설치함으로써 비행기 추락속도를 감속시켜 충격을 완화시키고, 비행기의 급감속 추락으로 발생될 수 있는 대형참사의 위험을 방지하며, 안전하게 착륙할 수 있도록 한 추락사고에 대비한 비행기 안전장치이다.The fall prevention device of the plane configured as described above is a large disaster that can be caused by the rapid deceleration fall of the plane by slowing down the plane's crash speed by installing a mechanism that can lift the plane in the event of a plane crash. It is an airplane safety device in case of a crash that prevents danger and allows you to land safely.
이상에서와 같이 본 고안에 의하면, 비행기의 추락사고 발생시 양력이 작용될 수 있는 기구가 펼쳐짐으로서 추락속도가 감속되어 충격이 완화되고 비행기가 안전하게 착륙될 수 있어 급격한 추락으로 인한 인명피해를 막고 비행기의 파손으로 인한 손실을 방지할 수 있는 비행기의 추락방지장치를 제공할 수 있다.As described above, according to the present invention, the mechanism that can lift the lift in the event of a plane accident is unfolded, the fall speed is reduced, the impact can be alleviated and the plane can be safely landed, preventing the casualties caused by the sudden fall and The fall prevention device of the plane which can prevent the loss by a damage can be provided.
Claims (1)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019990009719U KR19990035150U (en) | 1999-06-03 | 1999-06-03 | an fall preventing apparatus of an airplane |
Related Parent Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019990009719U Division KR19990035150U (en) | 1999-06-03 | 1999-06-03 | an fall preventing apparatus of an airplane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| KR200169065Y1 true KR200169065Y1 (en) | 2000-02-15 |
Family
ID=19577330
Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019990009719U KR19990035150U (en) | 1999-06-03 | 1999-06-03 | an fall preventing apparatus of an airplane |
| KR2019990017141U KR200169065Y1 (en) | 1999-06-03 | 1999-08-19 | an fall preventing apparatus of an airplane |
Family Applications Before (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019990009719U KR19990035150U (en) | 1999-06-03 | 1999-06-03 | an fall preventing apparatus of an airplane |
Country Status (1)
| Country | Link |
|---|---|
| KR (2) | KR19990035150U (en) |
-
1999
- 1999-06-03 KR KR2019990009719U patent/KR19990035150U/en active IP Right Review Request
- 1999-08-19 KR KR2019990017141U patent/KR200169065Y1/en not_active IP Right Cessation
Also Published As
| Publication number | Publication date |
|---|---|
| KR19990035150U (en) | 1999-09-06 |
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| T201 | Request for technology evaluation of utility model | ||
| REGI | Registration of establishment | ||
| FPAY | Annual fee payment |
Payment date: 20041020 Year of fee payment: 6 |
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| LAPS | Lapse due to unpaid annual fee |