DE60111923D1 - Abbrechbare betätigungsvorrichtung mit redundanter stromversorgung - Google Patents

Abbrechbare betätigungsvorrichtung mit redundanter stromversorgung

Info

Publication number
DE60111923D1
DE60111923D1 DE60111923T DE60111923T DE60111923D1 DE 60111923 D1 DE60111923 D1 DE 60111923D1 DE 60111923 T DE60111923 T DE 60111923T DE 60111923 T DE60111923 T DE 60111923T DE 60111923 D1 DE60111923 D1 DE 60111923D1
Authority
DE
Germany
Prior art keywords
cancelable
actuator
power supply
redundant power
redundant
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 - Lifetime
Application number
DE60111923T
Other languages
English (en)
Other versions
DE60111923T2 (de
Inventor
Edward Rudoy
Larry Leroy Mccormick
E Vega
W Courtney
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.)
Nea Electronics Inc
Original Assignee
Nea Electronics Inc
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 Nea Electronics Inc filed Critical Nea Electronics Inc
Publication of DE60111923D1 publication Critical patent/DE60111923D1/de
Application granted granted Critical
Publication of DE60111923T2 publication Critical patent/DE60111923T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/641—Interstage or payload connectors
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
    • B64G1/645—Separators
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02J—CIRCUIT ARRANGEMENTS OR SYSTEMS FOR SUPPLYING OR DISTRIBUTING ELECTRIC POWER; SYSTEMS FOR STORING ELECTRIC ENERGY
    • H02J1/00—Circuit arrangements for dc mains or dc distribution networks
    • H02J1/10—Parallel operation of dc sources

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
  • Electromagnets (AREA)
  • Air Bags (AREA)
  • Insulation, Fastening Of Motor, Generator Windings (AREA)
  • Fuses (AREA)
DE60111923T 2000-02-02 2001-02-01 Abbrechbare betätigungsvorrichtung mit redundanter stromversorgung Expired - Lifetime DE60111923T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/498,761 US6433990B1 (en) 2000-02-02 2000-02-02 Frangible actuator with redundant power supply
US498761 2000-02-02
PCT/US2001/003556 WO2001056884A2 (en) 2000-02-02 2001-02-01 Frangible actuator with redundant power supply

Publications (2)

Publication Number Publication Date
DE60111923D1 true DE60111923D1 (de) 2005-08-18
DE60111923T2 DE60111923T2 (de) 2006-05-24

Family

ID=23982387

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60111923T Expired - Lifetime DE60111923T2 (de) 2000-02-02 2001-02-01 Abbrechbare betätigungsvorrichtung mit redundanter stromversorgung

Country Status (5)

Country Link
US (1) US6433990B1 (de)
EP (1) EP1255675B1 (de)
AU (1) AU2001238023A1 (de)
DE (1) DE60111923T2 (de)
WO (1) WO2001056884A2 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6747541B1 (en) 2002-12-06 2004-06-08 G&H Technology, Inc. Spool assembly with integrated link-wire and electrical terminals for non-explosive actuators used in electro-mechanical structural separation devices
US8904889B2 (en) * 2004-08-02 2014-12-09 Nea Electronics, Inc. High load release device
US8568053B2 (en) * 2008-04-14 2013-10-29 Space Systems/Loral, Llc Radial release device
FR2930306A3 (fr) * 2008-04-16 2009-10-23 Conseil & Technique Dispositif de fixation servant a assembler des objets, puis a les liberer rapidement
US8021069B2 (en) * 2008-06-23 2011-09-20 Space Systems/Loral, Inc. Redundant radial release apparatus
US7893560B2 (en) * 2008-09-12 2011-02-22 Nellcor Puritan Bennett Llc Low power isolation design for a multiple sourced power bus
EP2213572B1 (de) 2009-01-29 2013-02-27 RUAG Aerospace Austria GmbH Vorrichtung zum Herunterdrücken einer beweglichen Struktur auf ein Raumschiff
AT509989B1 (de) * 2010-08-16 2012-01-15 Ruag Space Gmbh Vorrichtung zum festhalten und kommandierten freigeben eines freizugebenden elements eines raumfahrzeuges
US9085377B2 (en) * 2011-05-17 2015-07-21 Space Systems/Loral, Llc Redundant fuse wire release device
CN103368539B (zh) * 2012-03-26 2016-08-31 通用电气公司 开关元件和开关系统
US9761401B1 (en) 2016-08-27 2017-09-12 Glenair, Inc. Hold-down release apparatus and methods incorporating a fuse wire
US10518907B2 (en) 2016-09-13 2019-12-31 Ensign-Bickford Aerospace & Defense Company Spacecraft device initiation system
US10062537B1 (en) 2016-09-29 2018-08-28 Glenair, Inc. Redundant fuse wires in a hold-down release apparatus
US10029809B1 (en) 2016-09-29 2018-07-24 Glenair, Inc. Retention sleeve with rolling bearings in a hold-down release apparatus
US10124915B2 (en) 2017-01-23 2018-11-13 Ensign-Bickford Aerospace & Defense Company Hold down release mechanism with integral sensing
CN107689476B (zh) * 2017-09-22 2019-08-16 上海航天测控通信研究所 一种宇航用电热丝熔断释放装置
WO2019125257A1 (en) * 2017-12-21 2019-06-27 Ruag Space Ab A separation device
CN108327929A (zh) * 2018-02-09 2018-07-27 北京航空航天大学 一种超弹性sma带捆绑式非火工解锁机构
FR3086354B1 (fr) * 2018-09-26 2020-12-25 Conseil & Technique Dispositif de fixation servant a assembler entre eux des objets, puis a les liberer rapidement
AT521967B1 (de) * 2019-02-19 2020-07-15 Space Lock Gmbh Vorrichtung zum Umsetzen eines elektrischen Signals in eine mechanische Bewegung

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT334855B (de) 1975-01-23 1977-02-10 Voest Ag Vorrichtung zur verbindung der meissel mit dem schramkopf einer streckenvortriebsmaschine od.dgl.
GB2067034B (en) 1980-01-05 1983-09-28 British Aerospace Power distribution arrangement
US5221171A (en) 1992-10-15 1993-06-22 G & H Technology, Inc. Non-explosive separation nut
US5312147A (en) 1993-08-09 1994-05-17 G & H Technology, Inc. Electromechanical high load separation apparatus with a smooth release
US5438173A (en) 1994-01-27 1995-08-01 G & H Technology, Inc. Cell bypass switch
US5598041A (en) 1995-11-16 1997-01-28 Lockheed Martin Corporation Efficient fault tolerant switching circuit for redundant d. c. power supplies
DE19649739C2 (de) 1996-11-30 1998-11-12 Daimler Benz Aerospace Ag Freigabevorrichtung für Niederhalter z. B. an Solargeneratoren
DE19709298C2 (de) * 1997-03-06 1999-03-11 Isad Electronic Sys Gmbh & Co Startersysteme für einen Verbrennungsmotor sowie Verfahren zum Starten eines Verbrennungsmotors
US6249063B1 (en) * 1998-03-17 2001-06-19 Nea Electronics, Inc. Battery cell bypass with frangible actuator

Also Published As

Publication number Publication date
WO2001056884A3 (en) 2002-01-31
WO2001056884A2 (en) 2001-08-09
EP1255675A2 (de) 2002-11-13
EP1255675B1 (de) 2005-07-13
DE60111923T2 (de) 2006-05-24
AU2001238023A1 (en) 2001-08-14
US6433990B1 (en) 2002-08-13

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Legal Events

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8364 No opposition during term of opposition