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1. (WO2019044125) FLYING BODY
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Pub. No.: WO/2019/044125 International Application No.: PCT/JP2018/023363
Publication Date: 07.03.2019 International Filing Date: 19.06.2018
IPC:
B64C 31/036 (2006.01) ,B64C 13/30 (2006.01) ,B64D 17/80 (2006.01) ,B64D 25/00 (2006.01) ,B64D 45/04 (2006.01)
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
31
Aircraft intended to be sustained without power plant; Powered hang-glider-type aircraft; Microlight-type aircraft
028
Hang-glider-type aircraft; Microlight-type aircraft
036
having parachute-type wing
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
13
Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
24
Transmitting means
26
without power amplification or where power amplification is irrelevant
28
mechanical
30
using cable, chain, or rod mechanisms
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
17
Parachutes
80
in association with aircraft, e.g. for braking thereof
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
25
Emergency apparatus or devices, not otherwise provided for
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
D
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS
45
Aircraft indicators or protectors not otherwise provided for
04
Landing 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]; 東京都千代田区丸の内二丁目1番1号 1-1, Marunouchi 2-chome, Chiyoda-ku, Tokyo 1000005, JP
Inventors:
中村 博 NAKAMURA, Hiroshi; JP
八木橋 泰彦 YAGIHASHI, Yasuhiko; JP
笹本 幸一 SASAMOTO, Koichi; JP
Agent:
特許業務法人深見特許事務所 FUKAMI PATENT OFFICE, P.C.; 大阪府大阪市北区中之島三丁目2番4号 中之島フェスティバルタワー・ウエスト Nakanoshima Festival Tower West, 2-4, Nakanoshima 3-chome, Kita-ku, Osaka-shi, Osaka 5300005, JP
Priority Data:
2017-16564330.08.2017JP
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。
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Designated States: AE, AG, AL, AM, AO, AT, AU, AZ, BA, BB, BG, BH, BN, BR, BW, BY, BZ, CA, CH, CL, CN, CO, CR, CU, CZ, DE, DJ, DK, DM, DO, DZ, EC, EE, EG, ES, FI, GB, GD, GE, GH, GM, GT, HN, HR, HU, ID, IL, IN, IR, IS, JO, JP, KE, KG, KH, KN, KP, KR, KW, KZ, LA, LC, LK, LR, LS, LU, LY, MA, MD, ME, MG, MK, MN, MW, MX, MY, MZ, NA, NG, NI, NO, NZ, OM, PA, PE, PG, PH, PL, PT, QA, RO, RS, RU, RW, SA, SC, SD, SE, SG, SK, SL, SM, ST, SV, SY, TH, TJ, TM, TN, TR, TT, TZ, UA, UG, US, UZ, VC, VN, ZA, ZM, ZW
African Regional Intellectual Property Organization (ARIPO) (BW, GH, GM, KE, LR, LS, MW, MZ, NA, RW, SD, SL, ST, SZ, TZ, UG, ZM, ZW)
Eurasian Patent Office (AM, AZ, BY, KG, KZ, RU, TJ, TM)
European Patent Office (EPO) (AL, AT, BE, BG, CH, CY, CZ, DE, DK, EE, ES, FI, FR, GB, GR, HR, HU, IE, IS, IT, LT, LU, LV, MC, MK, MT, NL, NO, PL, PT, RO, RS, SE, SI, SK, SM, TR)
African Intellectual Property Organization (BF, BJ, CF, CG, CI, CM, GA, GN, GQ, GW, KM, ML, MR, NE, SN, TD, TG)
Publication Language: Japanese (JA)
Filing Language: Japanese (JA)