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1. WO2016154556 - FLIGHT CONTROLLER WITH GENERATOR CONTROL

Publication Number WO/2016/154556
Publication Date 29.09.2016
International Application No. PCT/US2016/024261
International Filing Date 25.03.2016
IPC
B64C 19/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
19Aircraft control not otherwise provided for
B64D 41/00 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
41Power installations for auxiliary purposes
F02D 9/00 2006.01
FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
DCONTROLLING COMBUSTION ENGINES
9Controlling engines by throttling air or fuel-and-air induction conduits or exhaust conduits
B64C 11/00 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
11Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
CPC
B64C 2201/042
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
04characterised by type of power plant
042by electric motors; Electric power sources therefor, e.g. fuel cells, solar panels or batteries
B64C 2201/108
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
10characterised by the lift producing means
108using rotors, or propellers
B64C 2201/141
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
2201Unmanned aerial vehicles; Equipment therefor
14characterised by flight control
141autonomous, i.e. by navigating independently from ground or air stations, e.g. by using inertial navigation systems [INS]
B64C 39/024
BPERFORMING OPERATIONS; TRANSPORTING
64AIRCRAFT; AVIATION; COSMONAUTICS
CAEROPLANES; HELICOPTERS
39Aircraft not otherwise provided for
02characterised by special use
024of the remote controlled vehicle type, i.e. RPV
B64D 2027/026
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
27Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
02Aircraft characterised by the type or position of power plant
026comprising different types of power plants, e.g. combination of an electric motor and a gas-turbines
B64D 31/06
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
31Power plant control; Arrangement thereof
02Initiating means
06actuated automatically
Applicants
  • SKYFRONT CORP. [US]/[US]
Inventors
  • MESTLER, Troy
  • STEPANOV, Anton
Agents
  • PARK, Jong, Andrew
Priority Data
15/080,40024.03.2016US
62/137,91525.03.2015US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) FLIGHT CONTROLLER WITH GENERATOR CONTROL
(FR) CONTRÔLEUR DE VOL AVEC CONTRÔLE D'UN GÉNÉRATEUR
Abstract
(EN)
A flight controller system includes an electronic speed control throttle input from which an anticipated electrical power demand is determined. The flight controller system includes a controller that determines a throttle input for a generator in order to satisfy the anticipated electrical power demand. The flight controller system includes an electronic speed control throttle output providing a delayed electronic speed control throttle signal.
(FR)
Un système de contrôleur de vol comprend : une entrée de commande des gaz de contrôle de vitesse électronique à partir de laquelle une demande de puissance électrique anticipée est déterminée ; un contrôleur qui détermine une entrée de commande des gaz pour un générateur afin de répondre à la demande de puissance électrique anticipée ; et une sortie de commande des gaz de contrôle de vitesse électronique délivrant un signal retardé de commande des gaz de contrôle de vitesse électronique.
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