1. A device for driving at least one wheel of a landing gear of an aircraft, comprising:
at least one turbine machine incorporated in the landing gear of the aircraft, the turbine machine comprising:
a pneumatic turbine, comprising an air management system configured to control an air flow and speed of rotation of the pneumatic turbine, wherein the pneumatic turbine is directly controlled from the cockpit by a control means to control a taxiing speed of the aircraft during forward low-speed taxiing phases.
2. The device according to claim 1, wherein the control means comprises an electrical mini-joystick configured to send a control signal to an electrical power center configured to relay the control signal to an air intake management system configured to control an air pressure at an inlet of the pneumatic turbine.
3. The device according to claim 1, wherein the turbine machine comprises an axial turbine stage driving an output shaft through a reducerinverter comprising one or more planetary gear trains.
4. The device according to claim 1, wherein the turbine machine comprises a freewheel device.
5. The device according to claim 1, comprising a pneumatic supply system for supplying the pneumatic turbine, wherein air for the pneumatic system is supplied from a pneumatic circuit of the aircraft.
6. The device according to claim 5, wherein the pneumatic circuit comprises a network linking an auxiliary power unit to an air conditioning of the aircraft.
7. The device according to claim 1 comprising a pneumatic supply system for supplying the pneumatic turbine, wherein air for the pneumatic system is supplied from a pneumatic circuit of a compressor.
8. The device according to claim 5, wherein the pneumatic supply system comprises an air intake control and shut-off valve.
9. The device according to claim 8, wherein the air management system is proximate a compressor or proximate the air intake control and shut-off valve.
10. The device according to claim 5, wherein the landing gear comprises an operating mechanism, and the pneumatic supply system is coupled to the landing gear operating mechanism by an articulated andor telescopic means.
11. System for taxiing an aircraft comprising at least two devices according to claim 10, wherein the control means operates to control the speed of each of a plurality of drive wheels using a differential control of the rotation speeds of the turbines of said devices to enhance the aircraft’s steering capabilities.
The claims below are in addition to those above.
All refrences to claim(s) which appear below refer to the numbering after this setence.
1. A low-power and high-speed transmission and reception apparatus, comprising:
a sending-end circuit sending an input signal;
a receiving-end circuit receiving the signal from the sending-end circuit;
a transmission line connected to the sending-end circuit and the receiving-end circuit in series, for transferring the signal from the sending-end circuit to the receiving-end circuit; and
a termination resistor included in at least one of the sending-end circuit and the receiving-end circuit,
wherein a value of the termination resistor is greater than a characteristic impedance value of the transmission line.
2. The low-power and high-speed transmission and reception apparatus of claim 1, wherein the value of the termination resistor is 1.5 times greater than the characteristic impedance value of the transmission line.
3. The low-power and high-speed transmission and reception apparatus of claim 1, wherein the receiving-end circuit comprises a Decision Feedback Equalization (DFE) circuit for compensating for at least one of an electromagnetic wave reflection phenomenon generated due to mismatch between a value of the termination resistor and characteristic impedance of the transmission line and an Inter-Symbol Interference (ISI) increase phenomenon attributable to a value of the termination resistor.
4. The low-power and high-speed transmission and reception apparatus of claim 3, wherein:
the sending-end circuit sends a data pattern for removing a skew between data and a clock, included in a signal to be received by the receiving-end circuit, to the receiving-end circuit before actually sending a signal, and
the receiving-end circuit performs a deskew operation on the signal to be received using the received data pattern.
5. The low-power and high-speed transmission and reception apparatus of claim 4, wherein:
the data pattern is a pattern in which \u20181\u2019 and \u20180\u2019 are alternately repeated, and
the receiving-end circuit generates a clock signal having an edge matched with a dead center of a period of the received data pattern and performs the deskew operation.
6. The low-power and high-speed transmission and reception apparatus of claim 3, wherein:
the sending-end circuit sends a pulse signal for measuring a reflection time and reflected size of the electromagnetic wave and a size of the ISI to the receiving-end circuit before actually sending a signal, and
the receiving-end circuit measures the reflection time and reflected size of the electromagnetic wave and the size of the ISI using the received pulse signal through the DFE circuit and compensates for the electromagnetic wave reflection phenomenon and the ISI based on the measured reflection time and reflected size of the electromagnetic wave and the measured size of the ISI.
7. The low-power and high-speed transmission and reception apparatus of claim 6, wherein the pulse signal is a periodic single-1 pulse signal in which \u20181\u2019 is in a 1-bit time interval of data and \u20180\u2019 continues to remain in a remaining time interval.
8. The low-power and high-speed transmission and reception apparatus of claim 6, wherein the receiving-end circuit measures and compensates for the reflection time and reflected size of the electromagnetic wave and the size of the ISI based on a point of time at which the \u20181\u2019 was received during one period of the single-1 pulse signal through the DFE circuit.
9. The low-power and high-speed transmission and reception apparatus of claim 7, wherein the receiving-end circuit measures all the reflection time and reflected size of the electromagnetic wave and the size of the ISI using one identical front-end circuit included in the DFE circuit based on the point of time at which the \u20181\u2019 was received, determines all positions and coefficient values of DFE taps using the measured values, and compensates for the electromagnetic wave reflection phenomenon and the ISI using the determined positions and coefficients of the DFE taps.
10. The low-power and high-speed transmission and reception apparatus of claim 9, wherein in order to compensate for the electromagnetic wave reflection phenomenon appearing at a receiving end using the DFE circuit, all DFE taps corresponding to all time intervals in which the reflection phenomenon continues are not used, but only DFE taps corresponding to several time intervals that are twice a propagation time of the transmission line, that is, a time interval where the reflection phenomenon appears, are used.
11. The low-power and high-speed transmission and reception apparatus of claim 1, wherein the transmission of the signal including the data and the clock through the transmission line is performed using a differential signaling method or a single-ended signaling method.
12. The low-power and high-speed transmission and reception apparatus of claim 1, wherein the low-power and high-speed transmission and reception apparatus sends one clock signal or sends one datum or a plurality of data in parallel.
13. The low-power and high-speed transmission and reception apparatus of claim 8, wherein the receiving-end circuit measures all the reflection time and reflected size of the electromagnetic wave and the size of the ISI using one identical front-end circuit included in the DFE circuit based on the point of time at which the \u20181\u2019 was received, determines all positions and coefficient values of DFE taps using the measured values, and compensates for the electromagnetic wave reflection phenomenon and the ISI using the determined positions and coefficients of the DFE taps.
14. The low-power and high-speed transmission and reception apparatus of claim 13, wherein in order to compensate for the electromagnetic wave reflection phenomenon appearing at a receiving end using the DFE circuit, all DFE taps corresponding to all time intervals in which the reflection phenomenon continues are not used, but only DFE taps corresponding to several time intervals that are twice a propagation time of the transmission line, that is, a time interval where the reflection phenomenon appears, are used.