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1. WO2020066391 - FLYING BODY PROVIDED WITH BODY TO BE DEPLOYED

Publication Number WO/2020/066391
Publication Date 02.04.2020
International Application No. PCT/JP2019/032921
International Filing Date 22.08.2019
IPC
B64D 17/34 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
17Parachutes
22Load suspension
34adapted to control direction or rate of descent
B64C 13/20 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
13Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02Initiating means
16actuated automatically, e.g. responsive to gust detectors
20using radiated signals
B64C 27/08 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 31/036 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
31Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028Hang-glider-type aircraft; Microlight-type aircraft
036having parachute-type wing
B64C 39/02 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 17/80 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
17Parachutes
80in association with aircraft, e.g. for braking thereof
CPC
B64C 13/20
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
13Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
02Initiating means
16actuated automatically, e.g. responsive to gust detectors
20using radiated signals
B64C 27/08
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
27Rotorcraft; Rotors peculiar thereto
04Helicopters
08with two or more rotors
B64C 31/036
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
31Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028Hang-glider-type aircraft; Microlight-type aircraft
036having parachute-type wing
B64C 39/02
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
B64D 17/34
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
17Parachutes
22Load suspension
34adapted to control direction or rate of descent
B64D 17/80
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
17Parachutes
80in association with aircraft, e.g. for braking thereof
Applicants
  • 日本化薬株式会社 NIPPONKAYAKU KABUSHIKIKAISHA [JP]/[JP]
Inventors
  • 中村 博 NAKAMURA, Hiroshi
  • 八木橋 泰彦 YAGIHASHI, Yasuhiko
  • 玉城 晃洋 TAMASHIRO, Akihiro
Agents
  • 奈良 泰宏 NARA, Yasuhiro
Priority Data
2018-18596728.09.2018JP
2018-18597728.09.2018JP
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) FLYING BODY PROVIDED WITH BODY TO BE DEPLOYED
(FR) CORPS VOLANT POURVU D'UN CORPS À DÉPLOYER
(JA) 被展開体を備えた飛行体
Abstract
(EN)
[Problem] To provide a flying body provided with a deployment device of a lift generation member, the flying body configured so as to make automatic avoidance of a collision with an obstacle easier than heretofore. [Solution] A flying body 30 is provided with: an obstacle detection unit 5, a control unit 6, a battery 7, a storage unit 8 that stores information transmitted from the control unit 6, and a transmission/reception unit 9 that receives an operation signal from a controller 40, and transmits information of the flying body 30 to the controller 40. The obstacle detection unit 5 is configured to detect the altitude of the flying body 30, and to output an altitude detection signal, which is the detected altitude information, to the control unit 6. In addition, if the obstacle detection unit 5 detects an obstacle present within a prescribed distance, the obstacle detection unit 5 outputs an obstacle detection signal to the control unit 6, and also detects the distance between a flying body main body 31 and the obstacle, and outputs a distance detection signal, which is the detected distance information, to the control unit 6. The control unit 6 determines whether to activate right and left brake cord tension devices depending on the signals received from the obstacle detection unit 5.
(FR)
La présente invention aborde le problème de la réalisation d'un corps volant pourvu d'un dispositif de déploiement d'un élément de génération de portance, le corps volant étant configuré de façon à rendre l'évitement automatique d'une collision avec un obstacle plus facile que précédemment. La solution selon l'invention porte sur un corps volant (30) qui est pourvu : d'une unité de détection d'obstacle (5), d'une unité de commande (6), d'une batterie (7), d'une unité de stockage (8) qui stocke des informations transmises à partir de l'unité de commande (6) et une unité d'émission/réception (9) qui reçoit un signal de fonctionnement en provenance d'un contrôleur (40) et émet des informations du corps volant (30) au contrôleur (40). L'unité de détection d'obstacle (5) est configurée pour détecter l'altitude du corps volant (30) et pour délivrer en sortie un signal de détection d'altitude, qui est l'information d'altitude détectée, à l'unité de commande (6). De plus, si l'unité de détection d'obstacle (5) détecte un obstacle présent au sein d'une distance prescrite, l'unité de détection d'obstacle (5) délivre en sortie un signal de détection d'obstacle à l'unité de commande (6) et détecte également la distance entre un corps principal de corps volant (31) et l'obstacle, et délivre en sortie un signal de détection de distance, qui est l'information de distance détectée, à l'unité de commande (6). L'unité de commande (6) détermine s'il faut activer des dispositifs de tension de cordon de frein de droite et de gauche en fonction des signaux reçus de la part l'unité de détection d'obstacle (5).
(JA)
【課題】障害物との衝突を自動回避することが従来よりも容易になる揚力発生部材の展開装置を備えた飛行体を提供する。 【解決手段】飛行体30は、障害物検知部5、制御部6、バッテリ7、制御部6から送信された情報を記憶する記憶部8、コントローラ40からの操作信号を受信し、飛行体30の情報をコントローラ40に送信する送受信部9などを備えている。障害物検知部5は、飛行体30の高度を検出し、検出した高度情報である高度検出信号を制御部6に出力するようになっている。また、障害物検知部5は、所定距離内に存在する障害物を検知した場合、障害物検知信号を制御部6に出力するとともに、飛行体本体31と障害物との距離を検出し、検出した距離情報である距離検出信号を制御部6に出力する。制御部6は、障害物検知部5から受信した信号に応じて左右のブレークコード引張装置10を作動させるか否かの判断を行う。
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