KR20170017365A - Air Bag of Drone or Quad Cop for safe Landing - Google Patents

Air Bag of Drone or Quad Cop for safe Landing Download PDF

Info

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
Application number
KR1020150111176A
Other languages
Korean (ko)
Inventor
장성훈
Original Assignee
장성훈
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by 장성훈 filed Critical 장성훈
Priority to KR1020150111176A priority Critical patent/KR20170017365A/en
Publication of KR20170017365A publication Critical patent/KR20170017365A/en

Links

Images

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/80Parachutes in association with aircraft, e.g. for braking thereof
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C39/00Aircraft not otherwise provided for
    • B64C39/02Aircraft not otherwise provided for characterised by special use
    • B64C39/024Aircraft not otherwise provided for characterised by special use of the remote controlled vehicle type, i.e. RPV
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00Parachutes
    • B64D17/62Deployment
    • B64D17/72Deployment by explosive or inflatable means
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00Aircraft indicators or protectors not otherwise provided for
    • B64D45/04Landing 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

The present invention relates to an operation device using a sensor and an operating principle of a wireless transmitting and receiving device of a drone, minimizing damage to products, an injury of a person, and safety of a fuselage of a rotary drone required for an emergency situation and a non-controllable situation of an aerial vehicle since casualties are generated by a significantly dangerous situation caused by abnormal landing where the flying drone has to unavoidably perform emergency landing or belly landing when one or a plurality of components among the multiple inner components have a defect while the drone flies to destination or randomly flies.

Description

Drones or Quadcob safety landings. {Air Bag of Drone or Quad Cop for safe Landing}

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

skip

Claims (1)

Helium gas or sodium azide used for airbeck is charged and operated after detection of the sensor. The helicopter gas capsule is exploded and forced into the parachute, and the safety landing pack is packed in a pack containing compressed helium gas and parachute. Only for equipment.
KR1020150111176A 2015-08-06 2015-08-06 Air Bag of Drone or Quad Cop for safe Landing KR20170017365A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (10)

* Cited by examiner, † Cited by third party
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

Similar Documents

Publication Publication Date Title
KR20170017365A (en) Air Bag of Drone or Quad Cop for safe Landing
EP3741683B1 (en) Impact protection apparatus
KR20140038495A (en) The rotor blade drone safety landing pack
CN107922051B (en) Safety device reaches unmanned aerial vehicle including its accident of preventing falling
CN107161328B (en) Projectile type disaster rescue and fire extinguishing unmanned aerial vehicle
CN203753400U (en) Unmanned scouting and rescuing aircraft for fire fighting
CN204998780U (en) Parachute for unmanned aerial vehicle
RU2381959C1 (en) Aircraft system of rescue operations support
JP2017095010A (en) Unmanned aircraft, unmanned aircraft control method and unmanned aircraft control program
Iqbal et al. Selection of unmanned aerial system (uas) for disaster relief operations: A comparison
KR20170114353A (en) Multi-rotor drone
JP2016516627A (en) Helicopter exterior life raft pod
CN1962362A (en) Light airplane safe life-saving system
CN104875889B (en) Navigation-type fall sea personnel's salvage helicopter
CN113453983A (en) Parachute device, flying device, and flying body launching mechanism
KR102263343B1 (en) Drone attachable mission apparatus using moving pin and system thereof
CN204998779U (en) Descending system for unmanned aerial vehicle
KR20160106826A (en) quantity flight
US20130200206A1 (en) Aircraft rescue device
Gupta Aerial delivery systems and technologies
CN207759011U (en) A kind of water resource detection unmanned plane water intaking mechanism
CN105882937A (en) Foldable drone
KR20180024731A (en) The rotor blade Drone safety landing pack
CN203767066U (en) Unmanned aerial vehicle with grounded buffering fairing
WO2018204826A1 (en) Valve assembly