BR9602020A - Permutador de calor processo de introdução de fluido de condicionamento no mesmo e caldeira para reaquecimento do fluido - Google Patents

Permutador de calor processo de introdução de fluido de condicionamento no mesmo e caldeira para reaquecimento do fluido

Info

Publication number
BR9602020A
BR9602020A BR9602020A BR9602020A BR9602020A BR 9602020 A BR9602020 A BR 9602020A BR 9602020 A BR9602020 A BR 9602020A BR 9602020 A BR9602020 A BR 9602020A BR 9602020 A BR9602020 A BR 9602020A
Authority
BR
Brazil
Prior art keywords
fluid
reheat
boiler
heat exchanger
exchanger process
Prior art date
Application number
BR9602020A
Other languages
English (en)
Inventor
Patrick Alan Houghton
Swaminathan Sunder
Frank Jude Riska
Melvyn Roy Collyer
William Robert Licht
Original Assignee
Air Prod & Chem
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 Air Prod & Chem filed Critical Air Prod & Chem
Publication of BR9602020A publication Critical patent/BR9602020A/pt

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
    • 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
    • B64G1/244—Spacecraft control systems
    • 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
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • B64G1/285—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using momentum 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/369—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using gyroscopes as attitude sensors
    • 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
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
    • 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)
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
BR9602020A 1995-04-28 1996-04-23 Permutador de calor processo de introdução de fluido de condicionamento no mesmo e caldeira para reaquecimento do fluido BR9602020A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/430,636 US5667171A (en) 1995-04-28 1995-04-28 Satellite spin axis stabilization using a single degree of freedom transverse momentum storage device

Publications (1)

Publication Number Publication Date
BR9602020A true BR9602020A (pt) 1998-10-06

Family

ID=23708400

Family Applications (1)

Application Number Title Priority Date Filing Date
BR9602020A BR9602020A (pt) 1995-04-28 1996-04-23 Permutador de calor processo de introdução de fluido de condicionamento no mesmo e caldeira para reaquecimento do fluido

Country Status (4)

Country Link
US (3) US5667171A (pt)
EP (1) EP0739818B1 (pt)
BR (1) BR9602020A (pt)
DE (1) DE69602798T2 (pt)

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US6062512A (en) * 1997-08-27 2000-05-16 Hughes Electronics Corporation Wobble and nutation control, and spin stabilization for a spacecraft using momentum conserving devices
US6162123A (en) 1997-11-25 2000-12-19 Woolston; Thomas G. Interactive electronic sword game
US6128556A (en) * 1998-03-16 2000-10-03 Honeywell International Inc. CMG control based on angular momentum to control satellite attitude
US6152403A (en) * 1998-11-11 2000-11-28 Hughes Electronics Corporation Gyroscopic calibration methods for spacecraft
US6202007B1 (en) * 1999-02-19 2001-03-13 John A. Spicer Exact stability integration in network designs
US6463365B1 (en) * 2000-02-01 2002-10-08 Raytheon Company System and method for controlling the attitude of a space craft
US7074175B2 (en) 2001-07-25 2006-07-11 Erik Schroeder Handy Thermotherapy via targeted delivery of nanoscale magnetic particles
US6860451B1 (en) * 2003-11-21 2005-03-01 The Boeing Company Spacecraft spin axis reorientation method
US7665695B2 (en) * 2003-12-03 2010-02-23 The Boeing Company Unified attitude control for spacecraft transfer orbit operations
US20050133670A1 (en) * 2003-12-03 2005-06-23 Wang H. G. Unified sensor-based attitude determination and control for spacecraft operations
US7603424B2 (en) * 2005-11-03 2009-10-13 Research In Motion Limited Method and system for generating template replies to electronic mail messages
WO2007059430A2 (en) * 2005-11-10 2007-05-24 Bristol-Myers Squibb Pharma Company Moesin, caveolin 1 and yes associated protein 1 as predictive markers of response to dasatinib in breast cancers
JP5030811B2 (ja) * 2008-02-15 2012-09-19 三菱重工業株式会社 宇宙機システム
US8620496B2 (en) * 2008-07-23 2013-12-31 The Boeing Company Systems and method of controlling a spacecraft using attitude sensors
FR2937954B1 (fr) * 2008-10-31 2011-07-29 Thales Sa Procede et systeme de desaturation des roues d'inertie d'un engin spatial
US8014911B2 (en) * 2009-11-03 2011-09-06 Honeywell International Inc. Methods and systems for imposing a momentum boundary while reorienting an agile vehicle with control moment gyroscopes
RU2481250C1 (ru) * 2011-12-28 2013-05-10 Федеральное государственное унитарное предприятие "Московское опытно-конструкторское бюро "Марс" (ФГУП МОКБ "Марс") Система стабилизации углового движения космического аппарата
FR3013685B1 (fr) 2013-11-25 2017-05-19 Astrium Sas Procede et dispositif de commande d'une phase d'acquisition du soleil par un engin spatial
US10050491B2 (en) 2014-12-02 2018-08-14 Management Services Group, Inc. Devices and methods for increasing energy and/or power density in composite flywheel energy storage systems
US9573623B2 (en) * 2015-01-08 2017-02-21 GM Global Technology Operations LLC Collision avoidance control integrated with electric power steering controller and rear steer
EA028853B1 (ru) * 2015-07-07 2018-01-31 федеральное государственное автономное образовательное учреждение высшего образования "Самарский государственный аэрокосмический университет имени академика С.П. Королева (национальный исследовательский университет)" (СГАУ) Способ пространственной переориентации и изменения параметров углового движения космического аппарата
US10144531B2 (en) 2016-02-04 2018-12-04 The Boeing Company Reorientation of a spinning spacecraft using gimbaled electric thrusters
US9963248B2 (en) * 2016-02-04 2018-05-08 The Boeing Company Spin stabilization of a spacecraft for an orbit maneuver
US11279501B2 (en) * 2018-10-25 2022-03-22 General Atomics Satellite attitude control system using eigen vector, non-linear dynamic inversion, and feedforward control
CN116280275B (zh) * 2023-01-19 2024-03-19 中国科学院微小卫星创新研究院 一种角动量自守恒机构以及卫星

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* Cited by examiner, † Cited by third party
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US3591108A (en) * 1967-01-27 1971-07-06 Rca Corp Control system for spinning bodies
US3637170A (en) * 1969-12-31 1972-01-25 Thomas O Paine Spacecraft attitude control method and apparatus
US4012018A (en) * 1973-10-04 1977-03-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration All sky pointing attitude control system
US3999729A (en) * 1975-03-20 1976-12-28 Rca Corporation Backup wheel for a three axis reaction wheel spacecraft
US4071211A (en) * 1976-09-23 1978-01-31 Rca Corporation Momentum biased active three-axis satellite attitude control system
US4193570A (en) * 1978-04-19 1980-03-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Active nutation controller
US4275861A (en) 1978-08-04 1981-06-30 Rca Corporation Orientation of momentum stabilized vehicles
US4230294A (en) * 1979-07-23 1980-10-28 Rca Corporation Closed loop roll control for momentum biased satellites
US4618112A (en) * 1983-04-15 1986-10-21 Rca Corporation Spacecraft angular momentum stabilization system and method
US4961551A (en) * 1988-11-18 1990-10-09 Hughes Aircraft Company Stabilization of a spinning spacecraft of arbitary shape
US5012992A (en) * 1988-12-09 1991-05-07 Hughes Aircraft Company Spin stabilization via momentum wheels or similar devices
US5067673A (en) * 1990-02-07 1991-11-26 Hughes Aircraft Company Essentially passive method for inverting the orientation of a dual spin spacecraft
US5255878A (en) * 1990-08-03 1993-10-26 Space Systems/Loral, Inc. Spin reorientation maneuver for spinning spacecraft
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
US5308024A (en) * 1992-07-20 1994-05-03 General Electric Co. Disturbance torque compensated three axis yaw control system
US5476239A (en) * 1994-04-19 1995-12-19 The United States Of America As Represented By The Secretary Of The Navy Gyro platform assembly with a spinning vehicle

Also Published As

Publication number Publication date
DE69602798D1 (de) 1999-07-15
EP0739818A1 (en) 1996-10-30
EP0739818B1 (en) 1999-06-09
US5758846A (en) 1998-06-02
DE69602798T2 (de) 2000-01-27
US6382565B1 (en) 2002-05-07
US5667171A (en) 1997-09-16

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Legal Events

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FB36 Technical and formal requirements: requirement - article 36 of industrial property law
FF Decision: intention to grant
FG9A Patent or certificate of addition granted
B24C Patent annual fee: request for for restoration

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