KR20170017365A - Air Bag of Drone or Quad Cop for safe Landing - Google Patents
Air Bag of Drone or Quad Cop for safe Landing Download PDFInfo
- Publication number
- KR20170017365A KR20170017365A KR1020150111176A KR20150111176A KR20170017365A KR 20170017365 A KR20170017365 A KR 20170017365A KR 1020150111176 A KR1020150111176 A KR 1020150111176A KR 20150111176 A KR20150111176 A KR 20150111176A KR 20170017365 A KR20170017365 A KR 20170017365A
- Authority
- KR
- South Korea
- Prior art keywords
- drone
- landing
- cop
- quad
- air bag
- Prior art date
Links
- 239000007789 gas Substances 0.000 claims description 7
- 239000001307 helium Substances 0.000 claims description 5
- 229910052734 helium Inorganic materials 0.000 claims description 5
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims description 5
- PXIPVTKHYLBLMZ-UHFFFAOYSA-N Sodium azide Chemical compound [Na+].[N-]=[N+]=[N-] PXIPVTKHYLBLMZ-UHFFFAOYSA-N 0.000 claims description 4
- 239000002775 capsule Substances 0.000 claims description 2
- 238000001514 detection method Methods 0.000 claims 1
- 230000006378 damage Effects 0.000 abstract description 4
- 230000007547 defect Effects 0.000 abstract description 3
- 208000027418 Wounds and injury Diseases 0.000 abstract 1
- 210000001015 abdomen Anatomy 0.000 abstract 1
- 230000002159 abnormal effect Effects 0.000 abstract 1
- 208000014674 injury Diseases 0.000 abstract 1
- 230000007613 environmental effect Effects 0.000 description 2
- 238000009835 boiling Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000009958 sewing Methods 0.000 description 1
Images
Classifications
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- 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
- B64D17/80—Parachutes in association with aircraft, e.g. for braking thereof
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/02—Aircraft not otherwise provided for characterised by special use
- B64C39/024—Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
-
- 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
- B64D17/62—Deployment
- B64D17/72—Deployment by explosive or inflatable means
-
- 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
- B64D45/00—Aircraft indicators or protectors not otherwise provided for
- B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
-
- B64C2201/185—
-
- B64D2700/62578—
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
Description
Drones, safe landings.
In recent years, the drones have been applied to various fields such as aerial photography, low-speed reconnaissance search, light cargo transportation, disaster relief work, etc. because of their light weight, easy to carry, quickness and economical efficiency. However, frequent crashes due to flight defects or external environmental causes during flight. Among the causes, inadequate manipulation of flight manipulation and inexperienced flight occupy the largest portion. Next, because the aircraft is operated by electric motor, it is possible to be out of control due to an electronic error. I came up with the idea of attaching an airbag or a parachute in case this happened, and I started to research about it.
Frequent crashes due to flight defects or external environmental causes during flight. Among the causes, inadequate manipulation of flight manipulation and inexperienced flight occupy the largest portion. Next, because the aircraft is operated by electric motor, it is possible to be out of control due to an electronic error. I came up with the idea of attaching an airbag or a parachute in case this happened, and I started to research about it.
If the flying drones are flying for arbitrary destination or arbitrary flight, if one or more parts of the internal parts fail, it is necessary to make an emergency landing or landing. And thus the operation principle of the drone's wireless transmitting / receiving device and the operation device using the sensor, which is necessary for the control of the flying object and emergency situation, And a system
The present invention minimizes the damage of the flying body caused by the fall and the damage of the enemy and the object by operating the safety landing pack and system when the drone freely falls in the uncontrollable state due to power failure due to malfunction or wind speed, There is a purpose.
drawing. 1 is an embodiment of the present invention.
The atomic weight of helium gas is 4.00260, melting point is -272.2, boiling point is -268.9, and specific gravity is 0.1785g / l. Because of its high buoyancy characteristics, helium gas is charged into buoyant buoys and buoyant bodies made by heat-joining method instead of sewing, so that life is rescued and used for new creative activities and various environments. It is activated after sensing the sensor by filling with sodium azide used for airbeck. The helicopter gas capsule is exploded and forced into the parachute, and the safety landing pack is packed with compressed helium gas and parachute.
The ground controller has a transmitter and operates the safety landing pack through the receiving device attached to the airplane when the airplane is unable to operate due to wind speed or external environment during flight
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Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150111176A KR20170017365A (en) | 2015-08-06 | 2015-08-06 | Air Bag of Drone or Quad Cop for safe Landing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
KR1020150111176A KR20170017365A (en) | 2015-08-06 | 2015-08-06 | Air Bag of Drone or Quad Cop for safe Landing |
Publications (1)
Publication Number | Publication Date |
---|---|
KR20170017365A true KR20170017365A (en) | 2017-02-15 |
Family
ID=58112290
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
KR1020150111176A KR20170017365A (en) | 2015-08-06 | 2015-08-06 | Air Bag of Drone or Quad Cop for safe Landing |
Country Status (1)
Country | Link |
---|---|
KR (1) | KR20170017365A (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101972784B1 (en) | 2017-11-09 | 2019-04-29 | 안진섭 | Evaluation System for Performance Safety of Drone |
KR20190052897A (en) | 2017-11-09 | 2019-05-17 | 안진섭 | Drone with Safety Monitoring Function |
KR20190092752A (en) | 2018-01-31 | 2019-08-08 | 공주대학교 산학협력단 | safety landing gear of drones |
CN110155351A (en) * | 2019-04-24 | 2019-08-23 | 台州学院 | A kind of unmanned plane with air bag |
KR102149504B1 (en) * | 2019-04-10 | 2020-08-31 | (주)한국플랜트관리 | Drone Safety Control System to Reduce Drone Fall Damage |
WO2021196137A1 (en) * | 2020-03-31 | 2021-10-07 | 南京达索航空科技有限公司 | Convenient protection box for unmanned aerial vehicle |
CN113815845A (en) * | 2021-08-19 | 2021-12-21 | 嘉应学院 | Emergency parachute landing and airbag mixed use device suitable for multi-rotor unmanned aerial vehicle |
KR20220151271A (en) * | 2021-05-06 | 2022-11-15 | 차대선 | A method to prevent the loss of drones in the marine area using a floating system that can be attached to a drone, and the drone |
KR20230116411A (en) | 2022-01-28 | 2023-08-04 | 현대모비스 주식회사 | System and method for controlling safety devices of rotorcraft aircraft |
-
2015
- 2015-08-06 KR KR1020150111176A patent/KR20170017365A/en unknown
Cited By (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
KR101972784B1 (en) | 2017-11-09 | 2019-04-29 | 안진섭 | Evaluation System for Performance Safety of Drone |
KR20190052897A (en) | 2017-11-09 | 2019-05-17 | 안진섭 | Drone with Safety Monitoring Function |
KR20190092752A (en) | 2018-01-31 | 2019-08-08 | 공주대학교 산학협력단 | safety landing gear of drones |
KR102149504B1 (en) * | 2019-04-10 | 2020-08-31 | (주)한국플랜트관리 | Drone Safety Control System to Reduce Drone Fall Damage |
CN110155351A (en) * | 2019-04-24 | 2019-08-23 | 台州学院 | A kind of unmanned plane with air bag |
WO2021196137A1 (en) * | 2020-03-31 | 2021-10-07 | 南京达索航空科技有限公司 | Convenient protection box for unmanned aerial vehicle |
KR20220151271A (en) * | 2021-05-06 | 2022-11-15 | 차대선 | A method to prevent the loss of drones in the marine area using a floating system that can be attached to a drone, and the drone |
CN113815845A (en) * | 2021-08-19 | 2021-12-21 | 嘉应学院 | Emergency parachute landing and airbag mixed use device suitable for multi-rotor unmanned aerial vehicle |
KR20230116411A (en) | 2022-01-28 | 2023-08-04 | 현대모비스 주식회사 | System and method for controlling safety devices of rotorcraft aircraft |
US11981425B2 (en) | 2022-01-28 | 2024-05-14 | Hyundai Mobis Co., Ltd. | System and method for controlling safety devices of rotary-wing aircraft |
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