Processing

Please wait...

Settings

Settings

Goto Application

1. WO2019044125 - FLYING BODY

Publication Number WO/2019/044125
Publication Date 07.03.2019
International Application No. PCT/JP2018/023363
International Filing Date 19.06.2018
IPC
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 13/30 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
24Transmitting means
26without power amplification or where power amplification is irrelevant
28mechanical
30using cable, chain, or rod mechanisms
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
B64D 25/00 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
25Emergency apparatus or devices, not otherwise provided for
B64D 45/04 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
45Aircraft indicators or protectors not otherwise provided for
04Landing aids; Safety measures to prevent collision with earth's surface
CPC
B64C 13/30
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
24Transmitting means
26without power amplification or where power amplification is irrelevant
28mechanical
30using cable, chain, or rod mechanisms
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
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
B64D 25/00
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
25Emergency apparatus or devices, not otherwise provided for
B64D 45/04
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
45Aircraft indicators or protectors not otherwise provided for
04Landing aids; Safety measures to prevent collision with earth's surface
Applicants
  • 日本化薬株式会社 NIPPON KAYAKU KABUSHIKI KAISHA [JP]/[JP]
Inventors
  • 中村 博 NAKAMURA, Hiroshi
  • 八木橋 泰彦 YAGIHASHI, Yasuhiko
  • 笹本 幸一 SASAMOTO, Koichi
Agents
  • 特許業務法人深見特許事務所 FUKAMI PATENT OFFICE, P.C.
Priority Data
2017-16564330.08.2017JP
Publication Language Japanese (JA)
Filing Language Japanese (JA)
Designated States
Title
(EN) FLYING BODY
(FR) CORPS VOLANT
(JA) 飛行体
Abstract
(EN)
This flying body comprises: a fuselage; a canopy capable of adjusting the speed of a fall when falling; a brake cord having one end connected to the canopy; a winding device (20) which is provided on the fuselage and allows the other end of the brake cord to be wound thereon; a sensor unit (5) for detecting the distance between the sensor unit (5) and an external object; and a control unit (6) for controlling the operation of the winding device (20) on the basis of the detection result of the sensor unit (5). The winding device (20) includes a gas generator (21) as a drive source. If the distance detected by the sensor unit (5) is equal to or less than a predetermined value, the control unit (6) actuates the gas generator (21) and thereby operates the winding device (20) so as to wind the other end of the brake cord.
(FR)
L'invention concerne un corps volant qui comporte : un fuselage ; un auvent capable de régler la vitesse d'une chute lors de la chute ; un cordon de frein ayant une extrémité reliée à l'auvent ; un dispositif d'enroulement (20) qui est disposé sur le fuselage et qui permet d'enrouler l'autre extrémité du cordon de frein ; une unité de détection (5) pour détecter la distance entre l'unité de détection (5) et un objet externe ; une unité de commande (6) pour commander le fonctionnement du dispositif d'enroulement (20) sur la base du résultat de détection de l'unité de détection (5). Le dispositif d'enroulement (20) comprend un générateur de gaz (21) en tant que source d'entraînement. Si la distance détectée par l'unité de détection (5) est inférieure ou égale à une valeur prédéterminée, l'unité de commande (6) actionne le générateur de gaz (21) et actionne ainsi le dispositif d'enroulement (20) afin d'enrouler l'autre extrémité du cordon de frein.
(JA)
飛行体は、機体と、落下時において落下速度を調整可能なキャノピーと、キャノピーに一端部が接続されたブレークコードと、機体に設けられるとともにブレークコードの他端部が巻き取り可能な巻取装置(20)と、外部の対象物との間の距離を検出するセンサ部(5)と、センサ部(5)の検出結果に基づいて巻取装置(20)の動作を制御する制御部(6)とを備える。巻取装置(20)は、駆動源としてのガス発生器(21)を含み、制御部(6)は、センサ部(5)によって検出された距離が所定値以下である場合に、ガス発生器(21)を作動させることでブレークコードの他端部が巻き取られるように巻取装置(20)を動作させる。
Latest bibliographic data on file with the International Bureau