RU2734123C2 - Структурно-интегрированная система терморегулирования для воздушно-космических летательных аппаратов - Google Patents

Структурно-интегрированная система терморегулирования для воздушно-космических летательных аппаратов Download PDF

Info

Publication number
RU2734123C2
RU2734123C2 RU2016150174A RU2016150174A RU2734123C2 RU 2734123 C2 RU2734123 C2 RU 2734123C2 RU 2016150174 A RU2016150174 A RU 2016150174A RU 2016150174 A RU2016150174 A RU 2016150174A RU 2734123 C2 RU2734123 C2 RU 2734123C2
Authority
RU
Russia
Prior art keywords
heat
conducting
aircraft
thermal
thermally active
Prior art date
Application number
RU2016150174A
Other languages
English (en)
Russian (ru)
Other versions
RU2016150174A3 (https=
RU2016150174A (ru
Inventor
Дэвид И. БЛЭНДИНГ
Арун МЮЛЕЙ
Джеффри К. КОФФМАН
Даг Ван АФФЕЛЕН
Original Assignee
Зе Боинг Компани
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 Зе Боинг Компани filed Critical Зе Боинг Компани
Publication of RU2016150174A publication Critical patent/RU2016150174A/ru
Publication of RU2016150174A3 publication Critical patent/RU2016150174A3/ru
Application granted granted Critical
Publication of RU2734123C2 publication Critical patent/RU2734123C2/ru

Links

Images

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
    • B64G1/46Arrangements or adaptations of devices for control of environment or living conditions
    • B64G1/50Arrangements or adaptations of devices for control of environment or living conditions for temperature control
    • HELECTRICITY
    • H05ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR
    • H05KPRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS; MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS
    • H05K7/00Constructional details common to different types of electric apparatus
    • H05K7/20Modifications to facilitate cooling, ventilating, or heating
    • H05K7/2039Modifications to facilitate cooling, ventilating, or heating characterised by the heat transfer by conduction from the heat generating element to a dissipating body
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C1/00Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06Frames; Stringers; Longerons ; Fuselage sections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/182Stringers, longerons
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/185Spars
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/18Spars; Ribs; Stringers
    • B64C3/187Ribs
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/26Construction, shape, or attachment of separate skins, e.g. panels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C9/00Adjustable control surfaces or members, e.g. rudders
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space
    • B64D13/06Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned
    • B64D13/08Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space the air being conditioned the air being heated or cooled
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/30Wing lift efficiency
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/40Weight reduction
    • 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
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/50On board measures aiming to increase energy efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Health & Medical Sciences (AREA)
  • General Health & Medical Sciences (AREA)
  • Remote Sensing (AREA)
  • Toxicology (AREA)
  • Environmental & Geological Engineering (AREA)
  • Environmental Sciences (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Biodiversity & Conservation Biology (AREA)
  • Physics & Mathematics (AREA)
  • Pulmonology (AREA)
  • Automation & Control Theory (AREA)
  • Thermal Sciences (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Physics & Mathematics (AREA)
  • Microelectronics & Electronic Packaging (AREA)
  • Cooling Or The Like Of Electrical Apparatus (AREA)
  • Cooling Or The Like Of Semiconductors Or Solid State Devices (AREA)
RU2016150174A 2016-02-29 2016-12-20 Структурно-интегрированная система терморегулирования для воздушно-космических летательных аппаратов RU2734123C2 (ru)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/056,731 US10029808B2 (en) 2016-02-29 2016-02-29 Structurally integrated thermal management system for aerospace vehicles
US15/056,731 2016-02-29

Publications (3)

Publication Number Publication Date
RU2016150174A RU2016150174A (ru) 2018-06-20
RU2016150174A3 RU2016150174A3 (https=) 2020-04-28
RU2734123C2 true RU2734123C2 (ru) 2020-10-13

Family

ID=58212946

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016150174A RU2734123C2 (ru) 2016-02-29 2016-12-20 Структурно-интегрированная система терморегулирования для воздушно-космических летательных аппаратов

Country Status (6)

Country Link
US (1) US10029808B2 (https=)
EP (1) EP3210885B1 (https=)
JP (1) JP6909012B2 (https=)
CN (1) CN107135629A (https=)
CA (1) CA2950699C (https=)
RU (1) RU2734123C2 (https=)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US12409756B2 (en) 2017-04-05 2025-09-09 H55 Sa Aircraft monitoring system and method for electric or hybrid aircrafts
US10479223B2 (en) 2018-01-25 2019-11-19 H55 Sa Construction and operation of electric or hybrid aircraft
US11065979B1 (en) 2017-04-05 2021-07-20 H55 Sa Aircraft monitoring system and method for electric or hybrid aircrafts
US11148819B2 (en) 2019-01-23 2021-10-19 H55 Sa Battery module for electrically-driven aircraft
US11063323B2 (en) 2019-01-23 2021-07-13 H55 Sa Battery module for electrically-driven aircraft
US10723437B2 (en) 2017-05-30 2020-07-28 The Boeing Company System for structurally integrated thermal management for thin wing aircraft control surface actuators
US10710741B2 (en) 2018-07-02 2020-07-14 Joby Aero, Inc. System and method for airspeed determination
WO2020061085A1 (en) 2018-09-17 2020-03-26 Joby Aero, Inc. Aircraft control system
US10983534B2 (en) 2018-12-07 2021-04-20 Joby Aero, Inc. Aircraft control system and method
US11230384B2 (en) 2019-04-23 2022-01-25 Joby Aero, Inc. Vehicle cabin thermal management system and method
KR102806907B1 (ko) 2019-04-23 2025-05-13 조비 에어로, 인크. 배터리 열 관리 시스템 및 방법
US11827383B2 (en) * 2020-04-09 2023-11-28 Sierra Space Corporation Encapsulated insulation with uniformly heated surfaces for use on spacecraft internal surfaces
CN112351660B (zh) * 2020-11-20 2023-04-14 中国电子科技集团公司第二十九研究所 一种低气动阻力蒙皮换热装置及其设计方法
CN112706913B (zh) * 2020-12-07 2022-03-11 沈阳飞机设计研究所扬州协同创新研究院有限公司 一种主动热控分布式电液伺服舵机
CN112606994B (zh) * 2020-12-29 2023-07-21 中国航空工业集团公司西安飞机设计研究所 一种太阳能无人机机翼一体化热控设计方法
WO2022174229A1 (en) * 2021-02-09 2022-08-18 Joby Aero, Inc. Aircraft propulsion unit
CN113665850B (zh) * 2021-08-02 2023-06-13 湖北航天技术研究院总体设计所 一种舵轴的相变式防热结构及飞行器
EP4149225A1 (en) * 2021-09-13 2023-03-15 Unseenlabs Integration of systems comprising standard electronic components in spacecrafts
CN114997597B (zh) * 2022-05-12 2023-07-18 南京航空航天大学 一种飞行器热管理系统的评价方法
CN115092424B (zh) * 2022-06-16 2024-10-25 东南大学 一种航天用液态金属磁性纳米流体散热器
CN115506893B (zh) * 2022-10-11 2025-06-03 中国航发沈阳发动机研究所 一种航空发动机燃油热管理系统
CN115768086A (zh) * 2022-12-09 2023-03-07 中国科学院长春光学精密机械与物理研究所 一种空间紫外成像光谱仪探测器的散热装置
CN117411549B (zh) * 2023-12-12 2024-03-12 上海卫星互联网研究院有限公司 一种通信设备及卫星
CN119939801B (zh) * 2024-12-27 2025-10-14 浙江大学 一种基于散热优化的智能自感知碳纤维与金属复合结构设计方法

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937304A1 (fr) * 2008-10-16 2010-04-23 Airbus France Actionneur de gouverne d'aeronef a refroidissement statique.
US20130048262A1 (en) * 2011-08-29 2013-02-28 Aerovironment Inc Thermal management system for an aircraft avionics bay
CN103847968A (zh) * 2014-03-05 2014-06-11 北京航空航天大学 一种利用机载废热的新型机翼防冰系统

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4819720A (en) 1984-11-09 1989-04-11 Mcdonnell Douglas Corporation Skin heat exchanger
US5506032A (en) 1994-04-08 1996-04-09 Martin Marietta Corporation Structural panel having integral heat pipe network
US5692558A (en) * 1996-07-22 1997-12-02 Northrop Grumman Corporation Microchannel cooling using aviation fuels for airborne electronics
JP4919184B2 (ja) * 2001-04-02 2012-04-18 株式会社竹中工務店 水分蒸発冷却屋根・壁体構造
JP4433271B2 (ja) * 2003-08-06 2010-03-17 東洋紡績株式会社 多孔質材料用保水性付与剤、その使用方法及び多孔質材料
US7325772B1 (en) * 2003-09-04 2008-02-05 L-3 Communications Corporation Aircraft heat sink and electronics enclosure
JP2005098674A (ja) * 2003-09-05 2005-04-14 Cinqvit:Kk 冷却装置
US8109324B2 (en) * 2005-04-14 2012-02-07 Illinois Institute Of Technology Microchannel heat exchanger with micro-encapsulated phase change material for high flux cooling
US8950468B2 (en) 2007-05-11 2015-02-10 The Boeing Company Cooling system for aerospace vehicle components
US7765811B2 (en) * 2007-06-29 2010-08-03 Laird Technologies, Inc. Flexible assemblies with integrated thermoelectric modules suitable for use in extracting power from or dissipating heat from fluid conduits
US8059409B2 (en) * 2009-06-19 2011-11-15 General Electric Company Avionics chassis
GB201012552D0 (en) * 2010-07-23 2010-11-17 Bae Systems Plc Aircraft thermal insulation
AU2012206414A1 (en) * 2011-01-11 2013-08-01 Bae Systems Plc Turboprop-powered aircraft
US8640469B2 (en) * 2011-08-08 2014-02-04 The Boeing Company Aircraft supplemental liquid cooler and method
FR2992629B1 (fr) 2012-06-27 2014-09-12 Airbus Operations Sas Dispositif de liaison mecanique d'une gouverne a un element structural fixe d'aeronef et element de voilure d'aeronef equipe de ce dispositif
US9578781B2 (en) * 2014-05-09 2017-02-21 Advanced Cooling Technologies, Inc. Heat management for electronic enclosures

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937304A1 (fr) * 2008-10-16 2010-04-23 Airbus France Actionneur de gouverne d'aeronef a refroidissement statique.
US20130048262A1 (en) * 2011-08-29 2013-02-28 Aerovironment Inc Thermal management system for an aircraft avionics bay
CN103847968A (zh) * 2014-03-05 2014-06-11 北京航空航天大学 一种利用机载废热的新型机翼防冰系统

Also Published As

Publication number Publication date
RU2016150174A3 (https=) 2020-04-28
US10029808B2 (en) 2018-07-24
EP3210885B1 (en) 2019-09-11
CA2950699A1 (en) 2017-08-29
US20170247126A1 (en) 2017-08-31
JP2017154728A (ja) 2017-09-07
RU2016150174A (ru) 2018-06-20
CA2950699C (en) 2021-04-20
JP6909012B2 (ja) 2021-07-28
CN107135629A (zh) 2017-09-05
EP3210885A1 (en) 2017-08-30

Similar Documents

Publication Publication Date Title
RU2734123C2 (ru) Структурно-интегрированная система терморегулирования для воздушно-космических летательных аппаратов
EP2680289B1 (en) Contactor mounting panel with improved thermal characteristics
US8294020B2 (en) Energy harvesting devices
EP2802047B1 (en) Heat sink for contactor in power distribution assembly
JP2017154728A5 (https=)
EP3419035B1 (en) Integrated contactor mounting post
US10350960B1 (en) Coupled battery and motor controller thermal management system
JP6482759B2 (ja) 発熱体として使用される金属マトリックス複合材
US20040211862A1 (en) Unmanned aerial vehicle with integrated wing battery
CN107466281B (zh) 无人飞行器的机架及无人飞行器
Reinhardt et al. Wide-bandgap power electronics for the More Electric Aircraft
US11225331B2 (en) Method and system for supplying power to an unmanned aerial vehicle
US9691926B2 (en) Using solar cells as bypass diode heat sinks
JP7119793B2 (ja) 飛行体
GB2447333A (en) Thermoelectric energy harvesting arrangement
EP3792175B1 (en) A thermal management system, a composite wing, and a composite wing spar
KR20250080170A (ko) 나셀 전기추진시스템을 구비한 비행체
Lawson et al. Thermal management of electromechanical actuation on an all-electric aircraft
CN109606612B (zh) 特种无人机结构功能一体化舱段和特种无人机
US20190382130A1 (en) Airborne structure element with embedded metal beam
BR102017000592A2 (pt) Aerospace vehicle, method for cooling of aerospace vehicle, and, thermal management system for an aerospace vehicle
BR102017000592B1 (pt) Veículo aeroespacial, e, método para resfriamento de veículo aeroespacial
JP7626912B2 (ja) 放熱部品および車両
CN117769199A (zh) 数据处理装置和车辆
CN209167996U (zh) 车载计算单元、散热器以及车载计算单元组件