DE602005012307D1 - Wand mit integriertem impuls - Google Patents

Wand mit integriertem impuls

Info

Publication number
DE602005012307D1
DE602005012307D1 DE602005012307T DE602005012307T DE602005012307D1 DE 602005012307 D1 DE602005012307 D1 DE 602005012307D1 DE 602005012307 T DE602005012307 T DE 602005012307T DE 602005012307 T DE602005012307 T DE 602005012307T DE 602005012307 D1 DE602005012307 D1 DE 602005012307D1
Authority
DE
Germany
Prior art keywords
wall
integrated impulse
impulse
integrated
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
DE602005012307T
Other languages
German (de)
English (en)
Inventor
Jack H Jacobs
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 DE602005012307D1 publication Critical patent/DE602005012307D1/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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
    • 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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • H—ELECTRICITY
    • H02—GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02K—DYNAMO-ELECTRIC MACHINES
    • H02K7/00—Arrangements for handling mechanical energy structurally associated with dynamo-electric machines, e.g. structural association with mechanical driving motors or auxiliary dynamo-electric machines
    • H02K7/02—Additional mass for increasing inertia, e.g. flywheels
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/425—Power storage
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/425—Power storage
    • B64G1/426—Flywheels
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/428—Power distribution and management
    • Y—GENERAL 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E60/00—Enabling technologies; Technologies with a potential or indirect contribution to GHG emissions mitigation
    • Y02E60/16—Mechanical 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)
DE602005012307T 2004-11-03 2005-11-02 Wand mit integriertem impuls Expired - Lifetime DE602005012307D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (1)

Publication Number Publication Date
DE602005012307D1 true DE602005012307D1 (de) 2009-02-26

Family

ID=36260697

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602005012307T Expired - Lifetime DE602005012307D1 (de) 2004-11-03 2005-11-02 Wand mit integriertem impuls

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

Family Cites Families (8)

* 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
EP0496184A1 (en) 1991-01-25 1992-07-29 CONTRAVES ITALIANA S.p.A. Attitude control actuator, particularly for spacecrafts
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
US6534887B1 (en) * 2000-10-06 2003-03-18 Honeywell International Inc. Microwheel

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
JP4768745B2 (ja) 2011-09-07
US20060091261A1 (en) 2006-05-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition