[특허]Auxiliary power unit starting system for an aircraft

Airbus Operations S.L.

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Auxiliary power unit starting system for an aircraft

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02N-011/04 H02P-009/04 F02C-007/26 F01D-019/00 F02C-007/268 B64D-041/00 F02N-011/08 B64D-031/00 B64F-001/34 G05D-001/00
출원번호	US-0156619 (2016-05-17)
등록번호	US-9964044 (2018-05-08)
우선권정보	EP-15382255 (2015-05-18)
발명자 / 주소	Juarez Becerril, Alberto Marcos Garcia, Mario
출원인 / 주소	Airbus Operations S.L.
대리인 / 주소	Greer, Burns & Crain Ltd.
인용정보	피인용 횟수 : 0 인용 특허 : 14

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An auxiliary power unit (APU) starting system for an aircraft comprises an APU comprising a starter motor and a generator, a DC power network, an AC power network, an electric connection line, and a control unit for controlling the APU starting and generating phase. The APU starting system additionally comprises switches for alternatively connecting through the electric connection line the DC power network with the APU starter motor, and the AC power network with the APU generator, wherein the control unit is further configured to operate the switches to...

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1. An auxiliary power unit starting system for an aircraft comprising: an auxiliary power unit comprising a DC starter motor to start the auxiliary power unit and a generator to provide AC power to the aircraft,a DC power network to provide power to the DC starter motor,an AC power network adapted to receive power from the generator,an electric connection line connectable between the generator and the AC power network to supply the generated power to the AC power network,a control unit configured to control the auxiliary power unit during an auxiliary power unit starting phase, and an auxiliary power unit generating phase, the auxiliary power unit starting system further comprising:switches to alternatively connect, through the electric connection line, the DC power network with the DC starter motor during the APU starting phase, and the generator with the AC power network, during the auxiliary power unit generating phase,wherein the control unit is configured to operate the switches to connect the DC power network with the DC starter motor by means of the electric connection line during the auxiliary power unit starting phase, and the AC power network with the generator by means of same electric connection line, during the auxiliary power unit generating phase. 2. The auxiliary power unit starting system according to claim 1, wherein the switch comprises a first switch for selectively connecting the electric connection line with the DC starter motor or with the generator, and wherein the control unit is additionally configured to operate the first switch to connect the DC starter motor during the auxiliary power unit starting phase, and the generator during the auxiliary power unit generating phase. 3. The auxiliary power unit starting system according to claim 2, further comprising a first additional line connecting the DC starter motor with the electric connection line, wherein the first switch comprises a first contactor provided in the electric connection line and a second contactor provided in the first additional line, and wherein the control unit is configured to operate the first and second contactors to selectively connect the electric connection line with the generator or with the DC starter motor. 4. The auxiliary power unit starting system according to claim 1, wherein the switch further comprises a second switch for selectively connecting the electric connection line with the AC power network or with the DC power network, and wherein the control unit is additionally configured to operate the second switch to connect the DC power network during the auxiliary power unit starting phase, and the AC power network during the auxiliary power unit generating phase. 5. The auxiliary power unit starting system according to claim 4, further comprising a second additional line connecting the DC power network to the electric connection line, wherein the second switch comprises a third contactor provided in the electric connection line and a fourth contactor provided in the second additional line, and wherein the control unit is configured to operate the third and fourth contactors to selectively connect the electric connection line with the AC power network or the DC power network. 6. The auxiliary power unit starting system according to claim 1, wherein the DC power network comprises a battery configured to start the auxiliary power unit DC starter motor. 7. The auxiliary power unit starting system according to claim 1, wherein the DC power network comprises a transformer rectifier unit connected to the AC power network to provide DC power. 8. The auxiliary power unit starting system according to claim 1, wherein the auxiliary power unit generator and the electric connection line are connected via one or several phases during the auxiliary power unit generating phase. 9. The auxiliary power unit starting system according to claim 1, wherein the electric connection line comprises one or several wires per phase of the generator. 10. The auxiliary power unit starting system according to claim 9, wherein the DC power network is connected to the DC starter motor by at least one wire of the electric connection line during the auxiliary power unit starting phase. 11. The auxiliary power unit starting system according to claim 9, wherein the control unit is configured to detect a wire failure or damage to prevent overcurrent during APU starting phase. 12. The auxiliary power unit starting system according to claim 1, wherein the switch comprises contactors configured as interlocking devices to prevent simultaneous connection. 13. The auxiliary power unit starting system according to claim 1, wherein the switch comprises a first switch for selectively connecting the electric connection line with the DC starter motor or with the generator,wherein the control unit is additionally configured to operate the first switch to connect the DC starter motor during the auxiliary power unit starting phase, and the generator during the auxiliary power unit generating phase,further comprising a first additional line connecting the DC starter motor with the electric connection line, wherein the first switch comprises a first contactor provided in the electric connection line and a second contactor provided in the first additional line, and wherein the control unit is configured to operate the first and second contactors to selectively connect the electric connection line with the generator or with the DC starter motor,wherein the switch further comprises a second switch for selectively connecting the electric connection line with the AC power network or with the DC power network, and wherein the control unit is additionally configured to operate the second switch to connect the DC power network during the auxiliary power unit starting phase, and the AC power network during the auxiliary power unit generating phase,further comprising a second additional line connecting the DC power network to the electric connection line, wherein the second switch comprises a third contactor provided in the electric connection line and a fourth contactor provided in the second additional line, and wherein the control unit is configured to operate the third and fourth contactors to selectively connect the electric connection line with the AC power network or the DC power network,wherein the switch comprises contactors configured as interlocking devices to prevent simultaneous connection, andwherein the switch comprises several contactors in series on the electric connection line, the first additional line, and the second additional line. 14. An aircraft comprising an auxiliary power unit starting system, comprising: an auxiliary power unit comprising a DC starter motor to start the auxiliary power unit and a generator to provide AC power to the aircraft,a DC power network to provide power to the DC starter motor,an AC power network adapted to receive power from the generator,an electric connection line connectable between the generator and the AC power network to provide the generated power to the AC power network,a control unit configured to control the auxiliary power unit during an auxiliary power unit starting phase and an auxiliary power unit generating phase, the auxiliary power unit starting system further comprising:switches to alternatively connect, through the electric connection line, the DC power network with the DC starter motor during the APU starting phase, and the generator with the AC power network, during the auxiliary power unit generating phase,wherein the control unit is configured to operate the switches to connect the DC power network with the DC starter motor by means of the electric connection line during the auxiliary power unit starting phase, and the AC power network with the generator by means of the same electric connection line during the auxiliary power unit generating phase.

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Auxiliary power unit starting system for an aircraft

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Auxiliary power unit starting system for an aircraft

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이 특허에 인용된 특허 (14)

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IPC 상세정보(version : 201201)

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