Some content of this application is unavailable at the moment.
If this situation persist, please contact us atFeedback&Contact
1. (WO2018178776) CAMERA CONTROL MECHANISM FOR AN AERIAL VEHICLE
Latest bibliographic data on file with the International Bureau    Submit observation

Pub. No.: WO/2018/178776 International Application No.: PCT/IB2018/051059
Publication Date: 04.10.2018 International Filing Date: 21.02.2018
IPC:
B64D 47/08 (2006.01) ,B64D 47/00 (2006.01) ,B64C 39/02 (2006.01)
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
47
Equipment not otherwise provided for
08
Arrangements of cameras
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
47
Equipment not otherwise provided for
B PERFORMING OPERATIONS; TRANSPORTING
64
AIRCRAFT; AVIATION; COSMONAUTICS
C
AEROPLANES; HELICOPTERS
39
Aircraft not otherwise provided for
02
characterised by special use
Applicants:
IDEAFORGE TECHNOLOGY PVT. LTD. [IN/IN]; EL-146 TTC Industrial Area Electronic Zone, MIDC Mahape, Navi Mumbai Maharashtra 400710, IN
Inventors:
SINGH, Rahul; IN
MORE, Santosh; IN
Agent:
KHURANA & KHURANA, ADVOCATES & IP ATTORNEYS; E-13, UPSIDC, Site-IV, Behind-Grand Venice Kasna Road, Greater Noida, National Capital Region Uttar Pradesh 201310, IN
Priority Data:
20172101180431.03.2017IN
Title (EN) CAMERA CONTROL MECHANISM FOR AN AERIAL VEHICLE
(FR) MÉCANISME DE COMMANDE DE CAMÉRA POUR VÉHICULE AÉRIEN
Abstract:
(EN) The present disclosure relates to a control system for a retractable belly mounted payload in an Aerial vehicle for retraction, pan and tilt movements of the payload, comprising a first mechanism to rotate the payload about a vertically oriented first axis for pan movement of the payload, and a second mechanism to rotate the payload about a horizontally oriented second axis, wherein rotation of the payload about the second axis provides movement of the payload between a retracted position within belly of the Aerial Vehicle and a deployed position out of the belly of the Aerial Vehicle, as well as tilt movement of the payload in its deployed position. First mechanism is driven by a servo through a set of gears or pulley-belt mechanism, and second mechanism is driven by a directly connected servo connected to the payload. Both the servos rotate along with payload during pan movement.
(FR) La présente invention concerne un système de commande pour une charge utile rétractable montée sur le ventre dans un véhicule aérien pour les mouvements de rétraction, panoramiques et d'inclinaison de la charge utile, comprenant un premier mécanisme pour faire tourner la charge utile autour d'un premier axe orienté verticalement pour un mouvement panoramique de la charge utile, et un second mécanisme pour faire tourner la charge utile autour d'un second axe orienté horizontalement, la rotation de la charge utile autour du second axe fournissant un mouvement de la charge utile entre une position rétractée dans le ventre du véhicule aérien et une position déployée hors du ventre du véhicule aérien, ainsi que le mouvement d'inclinaison de la charge utile dans sa position déployée. Le premier mécanisme est entraîné par un servomécanisme par l'intermédiaire d'un ensemble d'engrenages ou d'un mécanisme de courroie de poulie, et le second mécanisme est entraîné par un servomécanisme connecté directement à la charge utile. Les deux servomécanismes tournent conjointement avec la charge utile pendant le mouvement panoramique.
front page image
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: English (EN)
Filing Language: English (EN)