KR200166363Y1 - Deployment bag with pilotchute for rescue parachute - Google Patents
Deployment bag with pilotchute for rescue parachute Download PDFInfo
- Publication number
- KR200166363Y1 KR200166363Y1 KR2019990015654U KR19990015654U KR200166363Y1 KR 200166363 Y1 KR200166363 Y1 KR 200166363Y1 KR 2019990015654 U KR2019990015654 U KR 2019990015654U KR 19990015654 U KR19990015654 U KR 19990015654U KR 200166363 Y1 KR200166363 Y1 KR 200166363Y1
- Authority
- KR
- South Korea
- Prior art keywords
- parachute
- bag
- deployment bag
- mountain
- deployment
- Prior art date
Links
- 230000006698 induction Effects 0.000 abstract description 4
- 238000000034 method Methods 0.000 description 2
- 241001417539 Liza Species 0.000 description 1
- 239000004677 Nylon Substances 0.000 description 1
- 230000002411 adverse Effects 0.000 description 1
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 description 1
- 239000004744 fabric Substances 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229920001778 nylon Polymers 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D17/00—Parachutes
- B64D17/02—Canopy arrangement or construction
- B64D17/025—Canopy arrangement or construction for gliding chutes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C31/00—Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
- B64C31/028—Hang-glider-type aircraft; Microlight-type aircraft
- B64C31/036—Hang-glider-type aircraft; Microlight-type aircraft having parachute-type wing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Emergency Lowering Means (AREA)
Abstract
본 고안은 낙하산과 연결되어 유도산 기능을 하는 전개낭에 관한 것이다.The present invention relates to a deployment bag that is connected to the parachute to function as a guided mountain.
본 고안에 따르면, 하늘을 나는 행글라이더나 패러글라이더에 사용하는 구조용낙하산을 전개하는 전개낭에 있어서, 상기 전개낭에는 상기 구조용낙하산과 산줄로 연결되어 유도산역활을 하는 유도산겸용 전개낭이다.According to the present invention, a developmental parachute for deploying a rescue parachute for use in a flying hang glider or a paraglider, wherein the developmental sac is a combined induction mountain deployment bag that is connected to the rescue parachute and a line and serves as an induction mountain.
Description
본 고안은 유도산겸용 전개낭에 관한 것으로서, 보다 상세하게는 낙하산과 연결되어 유도산 역할을 하는 전개낭에 관한 것이다.The present invention relates to a combined delivery bag, and more particularly to a development bag connected to the parachute serves as a guided mountain.
일반적으로, 행글라이더나 패러글라이더는 래져스포츠로 하늘을 나는 기구이다. 비행중 추락이나 급회전 하강에 대비하여 낙하산이 장착된다. 행글라이더나 패러글라이더를 탈려면 도 1에 도시한 바와같이 사람의 몸을 담아주는 하네스(2)가 필요하고, 이 하네스 등쪽에 Out Container(14)가 있고 Out Container 속에 전개낭(26)이 있고 이 속에 낙하산이 포장된 상태에서 라이자(6)로 하네스 어깨부분에 연결되어있다. 또 개방손잡이(4)는 전개낭(26)과 연결되어 하네스 옆쪽에 붙어있다.In general, hang glider or paraglider is a flying sport for leisure sports. A parachute is mounted in case of a fall or a sharp descent in flight. In order to ride a hang glider or paraglider, as shown in Fig. 1, a harness (2) for holding a human body is required, and there is an Out Container (14) on the back side of the harness and a deployment bag (26) in the Out Container. With a parachute inside, it is connected to the harness shoulder with a lie (6). In addition, the open handle (4) is connected to the deployment bag 26 is attached to the side of the harness.
낙하산을 전개하기 위해서는 도 1에 도시한 개방손잡이(4)를 잡아당겨서 1차로 하네스 Out Container(14)로 부터 전개낭(26)을 분리시켜야 한다. 다시 2차로 전개낭(26)을 힘차게 던져야 한다. 이던져진 힘에 의해서 도 5에 도시한 바와같이 산줄(8)이 전개낭 루푸(24)에서 빠지고(B) 전개낭(26)이 분리된다(C,D). 다시 추락하는 속도에의해 낙하산 스커트(30)쪽으로 바람이 들어가서 낙하산이 산개된다.In order to deploy the parachute, it is necessary to pull out the opening handle 4 shown in FIG. 1 to separate the deployment bag 26 from the harness Out Container 14. Again, the deployment bag 26 should be vigorously thrown. As shown in Fig. 5, the ridge 8 is removed from the developmental bag loop (24) and the developmental bag 26 is separated (C, D) by the thrown force. By the speed of falling again, the wind enters the parachute skirt 30, and the parachute is spread out.
그래서 전개낭을 얼마나 잘 던지느냐에 산개 속도가 좌우된다. 글라이더를 타는 비행자의 기능과 악조건에서 전개낭을 잘던지기는 변수가 많다. 멀리 던지지 못했을 경우 추락하는 속도에의해 전개낭이 벗겨지고 낙하산 하부 스커트로 바람이 들어가기까지 침하 고도가 많아 낮은 고도에서 사고시 상당히 위험하다.(낙하산이 산개되기전에 지상에 추락)So, how fast you throw your development bag depends on your speed. The glider's ability to throw the deployment bag well under the aviator's ability and adverse conditions is often variable. If you don't throw it far, the deployment bag is peeled off by the speed of falling and the altitude is high until the wind enters the parachute lower skirt, which is quite dangerous in case of accident at low altitude.
그리고, 낙하산 산개시 전개낭(26)은 분리되어 재사용할수없다.(분실)In addition, the deployment bag 26 cannot be reused when the parachute is opened.
본 고안의 목적은 낙하산 상부와 연결되어 낙하산전개시 유도산 역할을하여 최악의 조건에서도 빠른 시간내에 낙하산을 산개할수있도록하고 재사용할수있도록 하기위한 것이다.The purpose of the present invention is to be connected to the upper part of the parachute to serve as a guided parachute when the parachute start, so that the parachute can be spread quickly and reused even in the worst conditions.
도 1은 종래의 (A)는 낙하산이 산개된 모양과 (B)는 낙하산이 포장된 사시도1 is a perspective view of a conventional parachute (A) and the parachute is packed (B)
도 2는 본 고안에 따른 낙하산이 산개된 사시도Figure 2 is a perspective view of the parachute spread in accordance with the present invention
도 3은 종래의 전개낭 평면도3 is a plan view of a conventional deployment bag
도 4는 본 고안에 따른 유도산겸 전개낭 (A)는 평면도 (B)는 정면도4 is a plan view (B) is a front view (B) is a front view
도 5는 종래의 낙하산이 전개되는 과정 사시도5 is a perspective view of a conventional parachute deployment process
도 6은 본 고안에 따른 낙하산이 전개되는 과정 사시도Figure 6 is a perspective view of the parachute deployment process according to the present invention
＜도면의 주요부분에 대한 부호의 설명＞<Description of the code | symbol about the principal part of drawing>
2. 하네스 4. 개방손잡이2. Harness 4. Open Handle
6. 라이자 8. 산줄6. Liza 8. Line
10.중심줄 12. 캐노피10.Centerline 12.Canopy
14.Out Container 16. 핀14.Out Container 16.Pin
18.웨빙(개방손잡이연결부) 20. 폴리카바나이트18.Webbing (open handle) 20.Polycarbanite
22.구멍쇠 24. 루프22. Hole 24. Loop
26.전개낭(Deployment Bag) 28. 유도산줄26.Deployment Bag 28. Guideline
본 고안에 따르면, 하늘을 나는 행글라이더나 패러글라이더에 사용하는 구조용낙하산을 전개하는 전개낭에 있어서, 상기 전개낭에는 상기 구조용낙하산과 산줄로 연결되어 유도산역활을 하는 유도산겸용 전개낭이다.According to the present invention, a developmental parachute for deploying a rescue parachute for use in a flying hang glider or a paraglider, wherein the developmental sac is a combined induction mountain deployment bag that is connected to the rescue parachute and a line and serves as an induction mountain.
이하, 본 고안의 바람직한 실시예를 첨부한 도면에 의거하여 설명하면 다음과 같다.Hereinafter, described with reference to the accompanying drawings, preferred embodiments of the present invention is as follows.
도 2는 본 고안에 따른 전개낭이 낙하산 상부쪽 중심줄과 연결된것으로서 , 도 4의 (A)(B)에 도시한 바와같이 유도산줄(28)과 회복성이 좋은 폴리카바나이트(20)가 부착된다. 이 폴리카바나이트(20)는 낙하산을 전개낭에 포장시 잘 구부러지고 전개낭이 개방시 회복성을 이용하여 잘 펼쳐질 수 있도록 하였다. 그리고, 상기 폴리카바나이트(20)는 전개낭원단에 나일론 테이프를 가장자리만 봉제하고 그 사이에 끼워 넣었다. 산줄은 도 4에 도시한 바와같이 전개낭 4곳에 지그재그 미싱으로 부착하였다. 이러한 전개낭의모양과 소재는 다양하게 바꿀 수도 있다.Figure 2 is that the deployment bag according to the present invention is connected to the parachute upper central row, as shown in Figure 4 (A) (B) is attached to the guide line 28 and the good recoverability polycarbane (20) do. The polycarbanite 20 allows the parachute to bend well when packaged in the development bag and to be well deployed using the resilience upon opening. In addition, the polycarbanite 20 sewn only the edge of the nylon tape in the developing bag fabric and sandwiched it therebetween. The lines were attached to the four developmental bags by zigzag sewing as shown in FIG. 4. The shape and material of the developing bag may vary.
이상에서와 같이 본 고안에 의하면, 행글라이더와 패러글라이더를 타는 비행자들에게 별도의 유도산이 필요없이 전개낭 만으로 유도산 역할을하는 기능과, 부피는 적고, 가격은싸고, 안전도는 높이는 유도산겸용 전개낭을 제공할수있다.As described above, according to the present invention, the passengers riding the hang glider and the paraglider do not need a separate guided mountain, which functions as a guided mountain by the deployment bag alone, and the volume is low, the price is low, and the safety is increased. You can provide a bag.
Claims (1)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019990015654U KR200166363Y1 (en) | 1999-07-27 | 1999-07-27 | Deployment bag with pilotchute for rescue parachute |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| KR2019990015654U KR200166363Y1 (en) | 1999-07-27 | 1999-07-27 | Deployment bag with pilotchute for rescue parachute |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| KR200166363Y1 true KR200166363Y1 (en) | 2000-02-15 |
Family
ID=19583207
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| KR2019990015654U KR200166363Y1 (en) | 1999-07-27 | 1999-07-27 | Deployment bag with pilotchute for rescue parachute |
Country Status (1)
| Country | Link |
|---|---|
| KR (1) | KR200166363Y1 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20210031045A (en) * | 2019-09-11 | 2021-03-19 | 주식회사 헥사팩토리 | Safety device of Drone, and Method for Controlling the Same |
-
1999
- 1999-07-27 KR KR2019990015654U patent/KR200166363Y1/en not_active IP Right Cessation
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20210031045A (en) * | 2019-09-11 | 2021-03-19 | 주식회사 헥사팩토리 | Safety device of Drone, and Method for Controlling the Same |
| KR102232489B1 (en) * | 2019-09-11 | 2021-03-26 | 주식회사 헥사팩토리 | Safety device of Drone, and Method for Controlling the Same |
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| REGI | Registration of establishment | ||
| LAPS | Lapse due to unpaid annual fee | ||
| T601 | Decision on revocation of utility model registration |