System and method for transferring airplanes
First Claim
Patent Images
1. An airplane transfer system for transferring an airplane comprising an airplane control component, said system comprising:
- (a) a transfer module comprising at least one motor and adapted to transfer an airplane, when the transfer module is driven by said at least one motor; and
(b) a controller coupled to the transfer module and configured to;
i) receive at least one transfer signal that is responsive to one or more commands provided via said airplane control component; and
ii) control the transfer module in response to the at least one transfer signal, wherein said one or more commands are a priori capable of controlling the airplane or components thereof;
wherein said airplane control component includes a steering component;
wherein said controller is configured to control steering of said transfer module in response to said at least one transfer signal which is responsive to steering commands generated by said steering component of said airplane.
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Abstract
An airplane transfer system for transferring an airplane comprising an airplane control component. The system comprises: a transfer module comprising at least one motor and adapted to transfer an airplane; and a controller coupled to the transfer module and configured to: i) receive a at least one transfer signal that is responsive to one or more commands provided via the airplane control component; and ii) control the transfer module in response to the transfer signal, wherein the commands are a priori capable of controlling the airplane or components thereof.
101 Citations
19 Claims
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1. An airplane transfer system for transferring an airplane comprising an airplane control component, said system comprising:
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(a) a transfer module comprising at least one motor and adapted to transfer an airplane, when the transfer module is driven by said at least one motor; and (b) a controller coupled to the transfer module and configured to;
i) receive at least one transfer signal that is responsive to one or more commands provided via said airplane control component; and
ii) control the transfer module in response to the at least one transfer signal, wherein said one or more commands are a priori capable of controlling the airplane or components thereof;wherein said airplane control component includes a steering component; wherein said controller is configured to control steering of said transfer module in response to said at least one transfer signal which is responsive to steering commands generated by said steering component of said airplane. - View Dependent Claims (2, 3, 4, 5, 6, 17)
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7. An airplane transfer system for transferring an airplane comprising an airplane control component and an electric control system configured to generate one or more transfer signals responsive to one or more commands provided from said airplane control component, said airplane transfer system comprising:
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(a) a transfer module comprising at least one motor and adapted to transfer an airplane, when the transfer module is driven by said at least one motor; and (b) a controller coupled to the transfer module and configured to;
i) be connected to said electric control system, so as to provide an electric communication path;
ii) receive said one or more transfer signals via said electric communication path; and
iii) control the transfer module in response to the one or more transfer signals, wherein said one or more commands are a priori capable of controlling the airplane or components thereof via said electric control system;wherein said airplane control component includes a steering component; wherein said controller is configured to control steering of said transfer module in response to said one or more transfer signals which is responsive to steering commands generated by said steering component of said airplane. - View Dependent Claims (8, 9, 10, 11, 12, 13, 14, 15, 18)
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16. An airplane transfer system for transferring an airplane, said airplane comprising a plurality of wheels;
- at least one mechanical system configured for operating at least one of said plurality of wheels, at least one airplane control component configured to issue one or more commands, and an electronic control system comprising;
a control interface configured to convert the one or more commands to transfer signals;
a component interface associated the at least one mechanical system and configured to receive the electrical signals and control its associated mechanical system based thereon; and
a plurality of electric cables in electrical communication with the control interface and the component interfaces and being configured for carrying the transfer signal therebetween;said airplane transfer system comprising; (a) a transfer module comprising at least one motor and adapted to transfer the airplane, when the transfer module is driven by said at least one motor; and (b) a controller coupled to the transfer module and configured to;
i) be connected to said electric control system, so as to provide an electric communication path;
ii) receive said transfer signals via said electric communication path; and
iii) control the transfer module in response to the transfer signals, wherein said commands are a priori capable of controlling the airplane or components thereof via said electric control system;wherein said at least one airplane control component includes a steering component; wherein said controller is configured to control steering of said transfer module in response to said transfer signals which is responsive to steering commands generated by said steering component of said airplane. - View Dependent Claims (19)
- at least one mechanical system configured for operating at least one of said plurality of wheels, at least one airplane control component configured to issue one or more commands, and an electronic control system comprising;
Specification