KR20210000395U - Rocket Booster Recovery Device - Google Patents
Rocket Booster Recovery Device Download PDFInfo
- Publication number
- KR20210000395U KR20210000395U KR2020190003315U KR20190003315U KR20210000395U KR 20210000395 U KR20210000395 U KR 20210000395U KR 2020190003315 U KR2020190003315 U KR 2020190003315U KR 20190003315 U KR20190003315 U KR 20190003315U KR 20210000395 U KR20210000395 U KR 20210000395U
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- South Korea
- Prior art keywords
- rocket booster
- wing
- drone
- rocket
- recovery device
- Prior art date
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- 238000011084 recovery Methods 0.000 title claims abstract description 15
- 238000000034 method Methods 0.000 claims description 10
- 238000005516 engineering process Methods 0.000 description 3
- 235000015842 Hesperis Nutrition 0.000 description 1
- 235000012633 Iberis amara Nutrition 0.000 description 1
- 230000001133 acceleration Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C3/00—Wings
- B64C3/38—Adjustment of complete wings or parts thereof
- B64C3/56—Folding or collapsing to reduce overall dimensions of aircraft
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/50—Foldable or collapsible UAVs
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U30/00—Means for producing lift; Empennages; Arrangements thereof
- B64U30/10—Wings
- B64U30/12—Variable or detachable wings, e.g. wings with adjustable sweep
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- B64C2201/021—
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- B64C2201/102—
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Toys (AREA)
Abstract
로켓 부스터 회수장치는 로켓 부스터는 로켓 부스터의 내측에 형성되어 회수가 될 시에 로켓 부스터 내측에 형성된 드론 즉 1개 이상의 관절이 형성된 팔(ARM)이 펼쳐 지게 되며 팔의 일측에는 프로펠러가 형성되며 공기 저항을 고려하여 내측에 형성된 드론의 외측에 공기저항을 받지 않도록 덮개가 형성되는 것이다.As for the rocket booster recovery device, the rocket booster is formed inside the rocket booster, and when it is recovered, the drone formed inside the rocket booster, that is, one or more articulated arms (ARM) is unfolded, and a propeller is formed on one side of the arm. In consideration of resistance, a cover is formed so as not to receive air resistance outside of the drone formed inside.
Description
본 고안은 로켓 부스터 회수 장치에 관한 것으로서 기존 기술은 로켓 부스터를 회수하기 위하여 로켓 부스터가 로켓엔진의 추력을 감소시키면서 착륙지점에 착륙하는 방법을 사용하고 있다.The present invention relates to a rocket booster recovery device, and the existing technology uses a method in which the rocket booster lands at the landing point while reducing the thrust of the rocket engine to recover the rocket booster.
본 고안의 배경이 되는 기술은 드론의 기술이다.The technology behind the present invention is the technology of drones.
부스터 로켓 [booster rocket]Booster rocket
항공기, 미사일 등에 일시적인 추력(推力)을 주어 고도 또는 스피드를 증대시킬 목적으로 장착된 보조적 로킷 엔진으로서, 항공기, 미사일 등의 이륙시나 램 제트 엔진의 초기 가속시에 사용된다. 다단 로킷의 제1단을 부스터라고 하는 경우도 있다. 또 제어용 로킷을 제외하고 추력올 주는 모든 로킷을 통틀어 부스터라고 할 때도 있다.It is an auxiliary rocket engine installed for the purpose of increasing altitude or speed by providing temporary thrust to aircraft and missiles, and is used during take-off of aircraft, missiles, etc. or during initial acceleration of ram jet engines. The first stage of a multi-stage rocket is sometimes called a booster. In addition, except for the control rocket, all rockets that give thrust are sometimes referred to as boosters.
본 고안이 해결하고자 하는 과제는 로켓 부스터를 저렴한 비용으로 회수하는 장치에 관한 것이다.The problem to be solved by the present invention relates to a device for recovering a rocket booster at low cost.
본 과제의 해결 수단은 사용하여 회수할 로켓 부스터의 일측에 드론을 장착하고 날개와 바퀴를 로켓 부스터 내측에 형성하며 외측에 덮개를 형성하는 것이다.The solution to this problem is to install a drone on one side of the rocket booster to be used and to form wings and wheels on the inside of the rocket booster, and a cover on the outside.
본 고안의 효과는 사용하여 회수할 로켓 부스터를 저렴한 비용으로 회수하는 것이다.The effect of the present invention is to recover a rocket booster to be recovered using at low cost.
도 1은 로켓 부스터의 외측에 드론 덮개가 형성된 것을 도시한 사시도이고
도 2는 로켓 부스터의 외측 드론 덮개가 열리고 드론의 접혔던 날개와 ㅂ바퀴가 펼쳐 지는 것을 도시한 사시도이다.1 is a perspective view showing that a drone cover is formed on the outside of a rocket booster
Figure 2 is a perspective view showing that the outer drone cover of the rocket booster is opened, and the folded wings and wheels of the drone are unfolded.
본 고안을 실시하기 위한 구체적인 내용을 도면을 사용하여 간략히 설명하면 When briefly explaining the specific details for carrying out the present invention using the drawings
도 1은 본 고안의 사시도로서1 is a perspective view of the present invention
회수할 로켓 부스터의 일측에 드론을 장착한 것을 도시한 사시도로서As a perspective view showing a drone mounted on one side of the rocket booster to be recovered
도 1은 로켓 부스터의 외측에 드론 덮개가 형성된 것을 도시한 사시도이고1 is a perspective view showing that a drone cover is formed on the outside of a rocket booster
도 2는 로켓 부스터의 외측 드론 덮개가 열리고 드론의 접혔던 날개와 ㅂ바퀴가 펼쳐 지는 것을 도시한 사시도이다.Figure 2 is a perspective view showing that the outer drone cover of the rocket booster is opened, and the folded wings and wheels of the drone are unfolded.
로켓 부스터는 로켓 부스터의 내측에 형성되어 회수가 될 시에 로켓 부스터 내측에 접이식 날개가 형성되고 접이식 날개의 일측에 구멍이 형성되어 접이식 날개 구멍 내측에 모터나 엔진과 일체가 된 프로펠러가 형성되거나 접이식 날개 앞측에 모터 또는 엔진과 일체로 된 프로펠러가 형성되며 공기 저항을 고려하여 내측에 형성된 접이식 드론 날개의 외측에 공기저항을 받지 않도록 덮개가 형성되는 것이며 로켓 부스터 내측에 접이식 날개가 형성되고 접이식 날개의 일측에 구멍이 형성되어 접이식 날개 구멍 내측에 모터나 엔진과 일체가 된 프로펠러가 형성되는 경우에 날개의 구멍외의 부분은 태양전지가 부착되게 되는 것을 특징으로 하는 것이며The rocket booster is formed inside the rocket booster, and when it is recovered, a folding wing is formed inside the rocket booster, and a hole is formed on one side of the folding wing, so that a propeller integrated with the motor or engine is formed inside the folding wing hole or folded. A propeller integrated with a motor or engine is formed on the front side of the wing, and a cover is formed on the outside of the folding drone wing formed on the inside in consideration of air resistance, and a folding wing is formed inside the rocket booster and When a hole is formed on one side and a propeller integrated with the motor or engine is formed inside the folding wing hole, the part outside the hole of the wing is characterized in that solar cells are attached.
접이식 날개 앞측에 모터 또는 엔진과 일체로 된 프로펠러가 형성되는 경우에 날개의 상부에 태양전지가 부착되게 되는 것이며When a propeller integrated with a motor or engine is formed in front of the folding wing, the solar cell is attached to the upper part of the wing.
로켓 부스터의 일측의 외측에는 덮개가 형성되고 내측에는 바퀴가 형성되어 착륙시에 외측 덮개가 열리고 내측 바퀴가 외부로 나와서 착륙하게 되는 것것이며A cover is formed on the outside of one side of the rocket booster, and a wheel is formed on the inside.
로켓 부스터 회수장치는 GPS와 도착예정지를 입력함에 의하여 날개 달린 로켓부스터 회수 장치을 이동시켜서 착륙 예정지에 착륙하게 하는 것이다.The rocket booster retrieval device moves the winged rocket booster retrieval device by inputting the GPS and the expected destination to land at the intended landing site.
1 : 회수할 로켓 부스터
2 : 날개
3 : 날개 덮개
10 : 바퀴1: Rocket booster to be recovered
2: wings
3: wing cover
10: wheels
Claims (10)
접이식 날개 앞측에 모터 또는 엔진과 일체로 된 프로펠러가 형성되는 경우에 날개의 상부에 태양전지가 부착되게 되는 것을 특징으로 하는 드론이 형성된 로켓 부스터 회수 장치. In paragraph 1
A rocket booster recovery device with a drone, characterized in that when a propeller integrated with a motor or an engine is formed in front of the folding wing, a solar cell is attached to the upper portion of the wing.
로켓 부스터의 일측의 외측에는 덮개가 형성되고 내측에는 바퀴가 형성되어 착륙시에 외측 덮개가 열리고 내측 바퀴가 외부로 나와서 착륙하게 되는 것을 특징으로 하는 로켓 부스터 회수 장치.The method according to any one of claims 1 to 3
A rocket booster recovery device, characterized in that a cover is formed on the outside of one side of the rocket booster and a wheel is formed on the inside, so that the outer cover is opened when landing, and the inner wheel comes out to land.
로켓 부스터 회수장치는 GPS와 도착예정지를 입력함에 의하여 날개 달린 로켓부스터 회수 장치을 이동시켜서 착륙 예정지에 착륙하게 하는 것을 특징으로 하는 드론이 형성된 로켓 부스터 회수 장치.The method according to any one of claims 1 to 4
The rocket booster recovery device is a rocket booster recovery device with a drone, characterized in that by moving the winged rocket booster recovery device by inputting the GPS and the expected arrival point to land at the intended landing site.
접이식 날개 앞측에 모터 또는 엔진과 일체로 된 프로펠러가 형성되는 경우에 날개의 상부에 태양전지가 부착되게 되는 것을 특징으로 하는 드론이 형성된 로켓 부스터 회수 방법.In paragraph 6
A method of recovering a rocket booster with a drone, characterized in that when a propeller integrated with a motor or an engine is formed in front of the folding wing, a solar cell is attached to the upper portion of the wing.
로켓 부스터의 일측의 외측에는 덮개가 형성되고 내측에는 바퀴가 형성되어 착륙시에 외측 덮개가 열리고 내측 바퀴가 외부로 나와서 착륙하게 되는 것을 특징으로 하는 로켓 부스터 회수 방법.The method according to any one of claims 6 to 8
A rocket booster recovery method, characterized in that a cover is formed on the outside of one side of the rocket booster and a wheel is formed on the inside, so that the outer cover is opened when landing, and the inner wheel comes out to land.
로켓 부스터 회수장치는 GPS와 도착예정지를 입력함에 의하여 날개 달린 로켓부스터 회수 장치을 이동시켜서 착륙 예정지에 착륙하게 하는 것을 특징으로 하는 드론이 형성된 로켓 부스터 회수 방법.
The method according to any one of claims 6 to 9
The rocket booster recovery device is a rocket booster recovery method with a drone, characterized in that by moving the winged rocket booster recovery device by inputting the GPS and the expected arrival point to land at the intended landing site.
Priority Applications (1)
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KR2020190003315U KR20210000395U (en) | 2019-08-10 | 2019-08-10 | Rocket Booster Recovery Device |
Applications Claiming Priority (1)
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KR2020190003315U KR20210000395U (en) | 2019-08-10 | 2019-08-10 | Rocket Booster Recovery Device |
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- 2019-08-10 KR KR2020190003315U patent/KR20210000395U/en unknown
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