B64D17/54

Device and method for ejecting a parachute
11142325 · 2021-10-12 · ·

The invention relates to a device (1) for ejecting a parachute, comprising a housing (2) with an ejection opening (3), wherein the housing (2) is suitable for at least partially accommodating the parachute. In order to enable a robust and repeated ejection of the parachute with a low weight of the device (1), according to the invention a movable base (4) is arranged within the housing (2), which base (4) is connected to the housing (2) via at least one spring element, wherein the base (4) can be releasably fixed in place within the housing (2) using a fixing means (5), wherein the device (1) is configured such that if a parachute is arranged within the housing (2), the base (4) is accelerated by the spring element when the fixing means (5) is released, so that the parachute is ejected through the ejection opening (3) by means of the base (4). Furthermore, the invention relates to a method for ejecting a parachute.

DRONE, PARACHUTE KIT FOR DRONES, AND METHOD OF CONTROLLING DRONES

The present disclosure relates to a drone including a drone body; a drone body battery provided in the drone body and responsible for supplying power to the drone body; a parachute kit detachably coupled to the drone body and including a parachute therein; a battery detector provided in the parachute kit and responsible for checking the state of the drone body battery; and a parachute controller for controlling the parachute kit depending on the state of the drone body battery detected by the battery detector, and to a parachute kit for drones. According to the present disclosure, the drone is configured so that, when the power of the parachute kit capable of being attached to or detached from the drone and the power of the drone body are cut off, the parachute is unfolded by spring elasticity or compressed air. Therefore, breakage of the drone may be prevented, and damage caused by drone crashes may be minimized.

DRONE, PARACHUTE KIT FOR DRONES, AND METHOD OF CONTROLLING DRONES

The present disclosure relates to a drone including a drone body; a drone body battery provided in the drone body and responsible for supplying power to the drone body; a parachute kit detachably coupled to the drone body and including a parachute therein; a battery detector provided in the parachute kit and responsible for checking the state of the drone body battery; and a parachute controller for controlling the parachute kit depending on the state of the drone body battery detected by the battery detector, and to a parachute kit for drones. According to the present disclosure, the drone is configured so that, when the power of the parachute kit capable of being attached to or detached from the drone and the power of the drone body are cut off, the parachute is unfolded by spring elasticity or compressed air. Therefore, breakage of the drone may be prevented, and damage caused by drone crashes may be minimized.

CRASH DETECTION DEVICE, FLYING BODY CRASH DETECTION METHOD, PARACHUTE OR PARAGLIDER DEPLOYMENT DEVICE, AND AIRBAG DEVICE
20200239136 · 2020-07-30 ·

Provided is a crash detection device, a method of detecting a crash of a flying object, a parachute or paraglider deployment device, and an airbag device that can improve the reliability in terms of safety. A device detecting a crash of a flying object includes a detection part capable of detecting a flying state of the flying object, a calculation section capable of determining whether the flying state of the flying object is abnormal based on data on the flying state of the flying object acquired by the detection part, and an abnormal signal output section capable of outputting an abnormal signal to the outside when the calculation section determines that the flying state of the flying object is abnormal. The calculation section acquires data from the detection part at a sampling frequency of 1 kHz or more, determines whether the data is data indicating that the flying state of the flying object is abnormal or noise that is unnecessary data when the data is equal to or greater than a predetermined threshold value, determines that the flying state of the flying object is abnormal when the data is determined to be the data indicating that the flying state of the flying object is abnormal.

CRASH DETECTION DEVICE, FLYING BODY CRASH DETECTION METHOD, PARACHUTE OR PARAGLIDER DEPLOYMENT DEVICE, AND AIRBAG DEVICE
20200239136 · 2020-07-30 ·

Provided is a crash detection device, a method of detecting a crash of a flying object, a parachute or paraglider deployment device, and an airbag device that can improve the reliability in terms of safety. A device detecting a crash of a flying object includes a detection part capable of detecting a flying state of the flying object, a calculation section capable of determining whether the flying state of the flying object is abnormal based on data on the flying state of the flying object acquired by the detection part, and an abnormal signal output section capable of outputting an abnormal signal to the outside when the calculation section determines that the flying state of the flying object is abnormal. The calculation section acquires data from the detection part at a sampling frequency of 1 kHz or more, determines whether the data is data indicating that the flying state of the flying object is abnormal or noise that is unnecessary data when the data is equal to or greater than a predetermined threshold value, determines that the flying state of the flying object is abnormal when the data is determined to be the data indicating that the flying state of the flying object is abnormal.

BIMODAL PARACHUTE DEPLOYMENT SYSTEM
20200207480 · 2020-07-02 ·

A parachute deployment system is disclosed. In various embodiments, the system includes an interface configured to receive sensor information; a parachute load limiting device; and a parachute load limiting device state controller. The parachute load limiting device state controller sets a state of the parachute load limiting device to a state associated with a corresponding amount of load based at least in part on the sensor information.

BIMODAL PARACHUTE DEPLOYMENT SYSTEM
20200207480 · 2020-07-02 ·

A parachute deployment system is disclosed. In various embodiments, the system includes an interface configured to receive sensor information; a parachute load limiting device; and a parachute load limiting device state controller. The parachute load limiting device state controller sets a state of the parachute load limiting device to a state associated with a corresponding amount of load based at least in part on the sensor information.

Lifesaving system using drone and lifesaving method using the same
10653900 · 2020-05-19 · ·

Disclosed is a lifesaving system using a drone and a lifesaving method using the lifesaving system. The lifesaving system includes: a lifesaving drone provided with a parachute, the drone approaching a victim by being remotely controlled and installed in the victim, and assisting rescuing the victim from a high-rise building by operating the parachute; and a disaster management center disposing a rescuing vehicle to a disaster occurrence area and remotely controlling the lifesaving drone when a disaster report is received, or a disaster occurrence area is recognized.

Lifesaving system using drone and lifesaving method using the same
10653900 · 2020-05-19 · ·

Disclosed is a lifesaving system using a drone and a lifesaving method using the lifesaving system. The lifesaving system includes: a lifesaving drone provided with a parachute, the drone approaching a victim by being remotely controlled and installed in the victim, and assisting rescuing the victim from a high-rise building by operating the parachute; and a disaster management center disposing a rescuing vehicle to a disaster occurrence area and remotely controlling the lifesaving drone when a disaster report is received, or a disaster occurrence area is recognized.

AERIAL VEHICLE AND METHOD OF CONTROLLING AERIAL VEHICLE

An aerial vehicle includes a lift generation member provided in an airframe in an expandable manner, a manipulation mechanism connected to the lift generation member and configured to manipulate the lift generation member, an expansion apparatus configured to expand the lift generation member, a control unit configured to control the manipulation mechanism, and a falling sensing unit configured to sense falling of the airframe. The expansion apparatus is configured to expand the lift generation member based on a falling sensing signal and the control unit is configured to start control of the manipulation mechanism based on the falling sensing signal.