JP4768745B2 - 集積された運動量壁 - Google Patents

集積された運動量壁 Download PDF

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Publication number
JP4768745B2
JP4768745B2 JP2007540045A JP2007540045A JP4768745B2 JP 4768745 B2 JP4768745 B2 JP 4768745B2 JP 2007540045 A JP2007540045 A JP 2007540045A JP 2007540045 A JP2007540045 A JP 2007540045A JP 4768745 B2 JP4768745 B2 JP 4768745B2
Authority
JP
Japan
Prior art keywords
slat
wafer
stator
slats
edge
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 - Fee Related
Application number
JP2007540045A
Other languages
English (en)
Japanese (ja)
Other versions
JP2008519352A (ja
JP2008519352A5 (enExample
Inventor
ジェイコブス,ジャック・エイチ
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.)
Honeywell International Inc
Original Assignee
Honeywell International 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 Honeywell International Inc filed Critical Honeywell International Inc
Publication of JP2008519352A publication Critical patent/JP2008519352A/ja
Publication of JP2008519352A5 publication Critical patent/JP2008519352A5/ja
Application granted granted Critical
Publication of JP4768745B2 publication Critical patent/JP4768745B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02KDYNAMO-ELECTRIC MACHINES
    • H02K7/00Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/02Additional mass for increasing inertia, e.g. flywheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/425Power storage
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/425Power storage
    • B64G1/426Flywheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/42Arrangements or adaptations of power supply systems
    • B64G1/428Power distribution and management
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16Mechanical energy storage, e.g. flywheels or pressurised fluids

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Power Engineering (AREA)
  • Container, Conveyance, Adherence, Positioning, Of Wafer (AREA)
  • Control Of Position Or Direction (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)
JP2007540045A 2004-11-03 2005-11-02 集積された運動量壁 Expired - Fee Related JP4768745B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US10/980,929 2004-11-03
US10/980,929 US7273196B2 (en) 2004-11-03 2004-11-03 System for vehicle attitude and/or momentum control
PCT/US2005/039858 WO2006098778A2 (en) 2004-11-03 2005-11-02 Integrated momentum wall

Publications (3)

Publication Number Publication Date
JP2008519352A JP2008519352A (ja) 2008-06-05
JP2008519352A5 JP2008519352A5 (enExample) 2008-09-11
JP4768745B2 true JP4768745B2 (ja) 2011-09-07

Family

ID=36260697

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007540045A Expired - Fee Related JP4768745B2 (ja) 2004-11-03 2005-11-02 集積された運動量壁

Country Status (5)

Country Link
US (1) US7273196B2 (enExample)
EP (1) EP1807305B1 (enExample)
JP (1) JP4768745B2 (enExample)
DE (1) DE602005012307D1 (enExample)
WO (1) WO2006098778A2 (enExample)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7367529B2 (en) * 2004-10-22 2008-05-06 Honeywell International, Inc. Momentum tube for distributed actuation
US9641287B2 (en) 2015-01-13 2017-05-02 Honeywell International Inc. Methods and apparatus for high-integrity data transfer with preemptive blocking
US20180198388A1 (en) * 2017-01-06 2018-07-12 Honeywell International Inc. High efficiency actuator for use in a momentum control device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0496184A1 (en) * 1991-01-25 1992-07-29 CONTRAVES ITALIANA S.p.A. Attitude control actuator, particularly for spacecrafts
JP2004510927A (ja) * 2000-10-06 2004-04-08 ハネウェル・インターナショナル・インコーポレーテッド マイクロホイール

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3143892A (en) * 1958-03-12 1964-08-11 Bosch Arma Corp Inertial platform
US3127774A (en) * 1961-11-08 1964-04-07 North American Aviation Inc Means and method for determining the direction of the axis of rotation of a controllably rotating platform
US5261631A (en) * 1991-06-24 1993-11-16 Hughes Aircraft Company Momentum wheel platform steering system and method
US5406858A (en) * 1993-10-22 1995-04-18 The United States Of America As Represented By The Secretary Of The Navy Gyro platform assembly
US5611505A (en) * 1994-11-18 1997-03-18 Hughes Electronics Spacecraft energy storage, attitude steering and momentum management system
US6113033A (en) * 1999-02-04 2000-09-05 Hughes Electronics Corporation Combined flywheel energy storage and attitude control apparatus for spacecraft

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0496184A1 (en) * 1991-01-25 1992-07-29 CONTRAVES ITALIANA S.p.A. Attitude control actuator, particularly for spacecrafts
JP2004510927A (ja) * 2000-10-06 2004-04-08 ハネウェル・インターナショナル・インコーポレーテッド マイクロホイール

Also Published As

Publication number Publication date
EP1807305B1 (en) 2009-01-07
WO2006098778A2 (en) 2006-09-21
JP2008519352A (ja) 2008-06-05
EP1807305A2 (en) 2007-07-18
US7273196B2 (en) 2007-09-25
WO2006098778A3 (en) 2006-11-30
US20060091261A1 (en) 2006-05-04
DE602005012307D1 (de) 2009-02-26

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