WO2003085850A1 - Power supply for a satellite receiver - Google Patents

Power supply for a satellite receiver Download PDF

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Publication number
WO2003085850A1
WO2003085850A1 PCT/US2003/010283 US0310283W WO03085850A1 WO 2003085850 A1 WO2003085850 A1 WO 2003085850A1 US 0310283 W US0310283 W US 0310283W WO 03085850 A1 WO03085850 A1 WO 03085850A1
Authority
WO
WIPO (PCT)
Prior art keywords
input
supply voltage
voltage
power
output
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/US2003/010283
Other languages
English (en)
French (fr)
Inventor
John James Fitzpatrick
Suresh Vishwanatm Leley
Andrew Eric Bowyer
Iii John Joseph Curtis
Robert Alan Pitsch
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Thomson Licensing SAS
Original Assignee
Thomson Licensing SAS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Thomson Licensing SAS filed Critical Thomson Licensing SAS
Priority to MXPA04009706A priority Critical patent/MXPA04009706A/es
Priority to EP03746133.2A priority patent/EP1490979B1/en
Priority to US10/509,970 priority patent/US6996389B2/en
Priority to AU2003226246A priority patent/AU2003226246A1/en
Priority to JP2003582921A priority patent/JP4369759B2/ja
Priority to KR10-2004-7015618A priority patent/KR20040105835A/ko
Priority to CN038073250A priority patent/CN1643800B/zh
Publication of WO2003085850A1 publication Critical patent/WO2003085850A1/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/06Receivers
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04HBROADCAST COMMUNICATION
    • H04H40/00Arrangements specially adapted for receiving broadcast information
    • H04H40/18Arrangements characterised by circuits or components specially adapted for receiving
    • H04H40/27Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95
    • H04H40/90Arrangements characterised by circuits or components specially adapted for receiving specially adapted for broadcast systems covered by groups H04H20/53 - H04H20/95 specially adapted for satellite broadcast receiving
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/06Receivers
    • H04B1/16Circuits
    • H04B1/18Input circuits, e.g. for coupling to an antenna or a transmission line
    • HELECTRICITY
    • H04ELECTRIC COMMUNICATION TECHNIQUE
    • H04BTRANSMISSION
    • H04B1/00Details of transmission systems, not covered by a single one of groups H04B3/00 - H04B13/00; Details of transmission systems not characterised by the medium used for transmission
    • H04B1/38Transceivers, i.e. devices in which transmitter and receiver form a structural unit and in which at least one part is used for functions of transmitting and receiving
    • H04B1/40Circuits

Definitions

  • a second input supply voltage is selected to be developed at the input, when the second antenna signal is selected.
  • a fault detector is coupled to the switch for changing the switching state in the switch, when the second antenna signal is selected and a fault condition occurs, to select an input supply voltage to be developed at the input that is different from the second input supply voltage.
  • FIGURE 1 illustrates a typical satellite receiver system
  • FIGURE 3 illustrates a power supply regulator, embodying an inventive feature, which can be incorporated in the satellite receiver system of FIGURE 1 ;
  • FIGURE 4 illustrates a flow chart for describing a mode of operation the power supply regulator of FIGURE 3 providing protection by a hardware technique;
  • An LNB similar to LNB 86 of FIGURE 1, includes an internal power supply regulator, not shown, for generating an internal supply voltage of 5V, not shown, from voltage Vo at either the 13V level or the 18V level.
  • the internal power supply regulator not shown, requires a minimum input supply voltage of 6V for producing the 5V level that is capable of providing the maximum required LNB operation current.
  • a maximum LNB operation current can be produced when voltage Vo at at least 6 volts level is applied to LNB 86.
  • power supply regulator 10 of FIGURE 3 is designed to supply a maximum current level of an output current IQ when output supply voltage Vo is equal to or greater than 6 volt.
  • the relationship between output supply voltage Vo and an output current IQ are shown in FIGURE 2, as explained before.
  • MOSFET 51 is turned off by signal 23b to supply, via diode 21, input voltage Ni at approximately 16 volts at the emitter of power transistor Ql .
  • This action advantageously, decreases the amount of power that power transistor Ql needs to dissipate.
  • the threshold level established by voltage 22a is preferably selected to be lower than the lower voltage level 13V of output voltage Vo, and higher than 6 volts.
  • step 114 When the fault condition disappears, as depicted in step 113 of FIGURE 5, normal operation step 114 can resume. On the other hand, if the fault persists, an interval timer step 115 will maintain the 13 volt mode. If fault is not detected in step 111, microprocessor 41 of FIGURE 3 selectively generates signal 23b at the LOW state or at the HIGH state in a step 116. Signal 23b of FIGURE 3 at the HIGH state will cause power supply regulator 10 to operate in the 18 volt mode in which output voltage Vo is 18V, in a manner described before, as depicted in step 117 of FIGURE 5.
  • a single input supply voltage 301' is provided, namely the 22 volt supply.
  • Power resistor 310' is used to absorb the additional heat generated in the lower 13 volt mode, when the lower level of 13 volts of output voltage V 0 is selected.
  • Power resistor 310' can be implemented, for example, by using two resistors coupled across the main current conducting terminals 5 la' and 51b' of MOSFET 51' and having an equivalent value of 9 Ohm.

Landscapes

  • Engineering & Computer Science (AREA)
  • Signal Processing (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Input Circuits Of Receivers And Coupling Of Receivers And Audio Equipment (AREA)
  • Continuous-Control Power Sources That Use Transistors (AREA)
PCT/US2003/010283 2002-04-03 2003-04-03 Power supply for a satellite receiver Ceased WO2003085850A1 (en)

Priority Applications (7)

Application Number Priority Date Filing Date Title
MXPA04009706A MXPA04009706A (es) 2002-04-03 2003-04-03 Suministro de energia para un receptor de satelite.
EP03746133.2A EP1490979B1 (en) 2002-04-03 2003-04-03 Power supply for a satellite receiver
US10/509,970 US6996389B2 (en) 2002-04-03 2003-04-03 Power supply for a satellite receiver
AU2003226246A AU2003226246A1 (en) 2002-04-03 2003-04-03 Power supply for a satellite receiver
JP2003582921A JP4369759B2 (ja) 2002-04-03 2003-04-03 衛星受信機のための電源
KR10-2004-7015618A KR20040105835A (ko) 2002-04-03 2003-04-03 위성 수신기용 전원
CN038073250A CN1643800B (zh) 2002-04-03 2003-04-03 用于卫星接收机的电源

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US37001602P 2002-04-03 2002-04-03
US60/370,016 2002-04-03

Publications (1)

Publication Number Publication Date
WO2003085850A1 true WO2003085850A1 (en) 2003-10-16

Family

ID=28792017

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2003/010283 Ceased WO2003085850A1 (en) 2002-04-03 2003-04-03 Power supply for a satellite receiver

Country Status (7)

Country Link
EP (1) EP1490979B1 (enExample)
JP (1) JP4369759B2 (enExample)
KR (1) KR20040105835A (enExample)
CN (1) CN1643800B (enExample)
AU (1) AU2003226246A1 (enExample)
MX (1) MXPA04009706A (enExample)
WO (1) WO2003085850A1 (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8509716B2 (en) 2005-09-19 2013-08-13 Thomson Licensing Adaptive impedance for LNB power supply output in dependence on communication mode/protocol

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR100655972B1 (ko) * 2004-10-22 2006-12-11 엘지전자 주식회사 지피에스 전원관리 기능을 갖는 이동통신 단말기 및 그 방법
CN104570853B (zh) * 2014-12-18 2017-04-05 中国科学院长春光学精密机械与物理研究所 高可靠组合智能空间电源系统
CN104767948B (zh) * 2015-04-10 2017-12-01 无锡市晶源微电子有限公司 一种卫星接收高频头lnb偏置电路

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5563500A (en) * 1994-05-16 1996-10-08 Thomson Consumer Electronics, Inc. Voltage regulator having complementary type transistor
US5826170A (en) * 1994-11-08 1998-10-20 Space Systems/Loral, Inc. Satellite communication power management system
US5828206A (en) * 1995-03-17 1998-10-27 Toko Kabushiki Kaisha Serial control type voltage regulator
US6061577A (en) * 1994-12-20 2000-05-09 Alcatel Electrical power supply circuit, in particular for portable appliances

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9008898D0 (en) * 1990-04-20 1990-06-20 Ferguson Ltd Receiver for satellite reception
CN1147139C (zh) * 1998-02-16 2004-04-21 皇家菲利浦电子有限公司 卫星接收机

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5563500A (en) * 1994-05-16 1996-10-08 Thomson Consumer Electronics, Inc. Voltage regulator having complementary type transistor
US5826170A (en) * 1994-11-08 1998-10-20 Space Systems/Loral, Inc. Satellite communication power management system
US6061577A (en) * 1994-12-20 2000-05-09 Alcatel Electrical power supply circuit, in particular for portable appliances
US5828206A (en) * 1995-03-17 1998-10-27 Toko Kabushiki Kaisha Serial control type voltage regulator

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See also references of EP1490979A4 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8509716B2 (en) 2005-09-19 2013-08-13 Thomson Licensing Adaptive impedance for LNB power supply output in dependence on communication mode/protocol

Also Published As

Publication number Publication date
CN1643800B (zh) 2010-05-26
JP2005522142A (ja) 2005-07-21
EP1490979A4 (en) 2011-05-04
MXPA04009706A (es) 2005-01-11
AU2003226246A1 (en) 2003-10-20
EP1490979B1 (en) 2015-08-12
KR20040105835A (ko) 2004-12-16
JP4369759B2 (ja) 2009-11-25
EP1490979A1 (en) 2004-12-29
CN1643800A (zh) 2005-07-20

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