GB1393637A - Electric power supply arrangement for aircraft - Google Patents

Electric power supply arrangement for aircraft

Info

Publication number
GB1393637A
GB1393637A GB5111373A GB5111373A GB1393637A GB 1393637 A GB1393637 A GB 1393637A GB 5111373 A GB5111373 A GB 5111373A GB 5111373 A GB5111373 A GB 5111373A GB 1393637 A GB1393637 A GB 1393637A
Authority
GB
United Kingdom
Prior art keywords
voltage
output
converting
inverter
transformer
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.)
Expired
Application number
GB5111373A
Other languages
English (en)
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.)
Siemens Corp
Original Assignee
Siemens Corp
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
Priority claimed from DE19722253739 external-priority patent/DE2253739C3/de
Application filed by Siemens Corp filed Critical Siemens Corp
Publication of GB1393637A publication Critical patent/GB1393637A/en
Expired legal-status Critical Current

Links

Classifications

    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/42—Conversion of DC power input into AC power output without possibility of reversal
    • H02M7/44—Conversion of DC power input into AC power output without possibility of reversal by static converters
    • H02M7/48—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode
    • H02M7/4807—Conversion of DC power input into AC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode having a high frequency intermediate AC stage
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02M—APPARATUS FOR CONVERSION BETWEEN AC AND AC, BETWEEN AC AND DC, OR BETWEEN DC AND DC, AND FOR USE WITH MAINS OR SIMILAR POWER SUPPLY SYSTEMS; CONVERSION OF DC OR AC INPUT POWER INTO SURGE OUTPUT POWER; CONTROL OR REGULATION THEREOF
    • H02M7/00—Conversion of AC power input into DC power output; Conversion of DC power input into AC power output
    • H02M7/02—Conversion of AC power input into DC power output without possibility of reversal
    • H02M7/04—Conversion of AC power input into DC power output without possibility of reversal by static converters
    • H02M7/12—Conversion of AC power input into DC power output without possibility of reversal by static converters using discharge tubes with control electrode or semiconductor devices with control electrode

Landscapes

  • Engineering & Computer Science (AREA)
  • Power Engineering (AREA)
  • Inverter Devices (AREA)
  • Dc-Dc Converters (AREA)
GB5111373A 1972-11-02 1973-11-02 Electric power supply arrangement for aircraft Expired GB1393637A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722253739 DE2253739C3 (de) 1972-11-02 Schaltungsanordnung zur Versorgung des Bordnetzes eines Fahrzeuges, insbesondere eines Luftfahrzeuges

Publications (1)

Publication Number Publication Date
GB1393637A true GB1393637A (en) 1975-05-07

Family

ID=5860707

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5111373A Expired GB1393637A (en) 1972-11-02 1973-11-02 Electric power supply arrangement for aircraft

Country Status (2)

Country Link
FR (1) FR2205763B1 (https=)
GB (1) GB1393637A (https=)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0010900A1 (en) * 1978-10-23 1980-05-14 Era Patents Limited A static inverter with a relatively low-frequency output voltage, and a method for generating this voltage
GB2137833A (en) * 1983-04-08 1984-10-10 Toshiba Kk Uninterruptible power supply
US4945467A (en) * 1988-02-26 1990-07-31 Black & Decker Inc. Multiple-mode voltage converter
CN115051421A (zh) * 2021-03-08 2022-09-13 通用汽车环球科技运作有限责任公司 用于移动电源的装置

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0010900A1 (en) * 1978-10-23 1980-05-14 Era Patents Limited A static inverter with a relatively low-frequency output voltage, and a method for generating this voltage
US4348719A (en) 1978-10-23 1982-09-07 Era Patents Limited Static inverter with energy return
GB2137833A (en) * 1983-04-08 1984-10-10 Toshiba Kk Uninterruptible power supply
US4562357A (en) * 1983-04-08 1985-12-31 Tokyo Shibaura Denki Kabushiki Kaisha Uninterruptible power supply and a starting method
US4945467A (en) * 1988-02-26 1990-07-31 Black & Decker Inc. Multiple-mode voltage converter
CN115051421A (zh) * 2021-03-08 2022-09-13 通用汽车环球科技运作有限责任公司 用于移动电源的装置

Also Published As

Publication number Publication date
DE2253739A1 (de) 1974-05-16
DE2253739B2 (de) 1976-02-19
FR2205763B1 (https=) 1976-11-19
FR2205763A1 (https=) 1974-05-31

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Legal Events

Date Code Title Description
PS Patent sealed
PCNP Patent ceased through non-payment of renewal fee