RU2016107562A - The method of air cooling of fuel equipment located outside the aircraft, and a system for its implementation - Google Patents

The method of air cooling of fuel equipment located outside the aircraft, and a system for its implementation Download PDF

Info

Publication number
RU2016107562A
RU2016107562A RU2016107562A RU2016107562A RU2016107562A RU 2016107562 A RU2016107562 A RU 2016107562A RU 2016107562 A RU2016107562 A RU 2016107562A RU 2016107562 A RU2016107562 A RU 2016107562A RU 2016107562 A RU2016107562 A RU 2016107562A
Authority
RU
Russia
Prior art keywords
air
aircraft
heat
flow
located outside
Prior art date
Application number
RU2016107562A
Other languages
Russian (ru)
Other versions
RU2632057C2 (en
Inventor
Андрей Александрович Басов
Анатолий Александрович Дядькин
Максим Александрович Лексин
Юрий Максимович Прохоров
Original Assignee
Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева"
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 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" filed Critical Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева"
Priority to RU2016107562A priority Critical patent/RU2632057C2/en
Publication of RU2016107562A publication Critical patent/RU2016107562A/en
Application granted granted Critical
Publication of RU2632057C2 publication Critical patent/RU2632057C2/en

Links

Classifications

    • 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, or structural parts of the aircraft
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L23/00Details of semiconductor or other solid state devices
    • H01L23/34Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements
    • H01L23/46Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids
    • H01L23/467Arrangements for cooling, heating, ventilating or temperature compensation ; Temperature sensing arrangements involving the transfer of heat by flowing fluids by flowing gases, e.g. air
    • 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

Landscapes

  • Cooling Or The Like Of Electrical Apparatus (AREA)

Claims (2)

1. Способ воздушного охлаждения тепловыделяющей аппаратуры, расположенной снаружи летательных аппаратов, включающий тепловой контакт между тепловыделяющими поверхностями аппаратуры и воздушными термоплатами, движение атмосферного воздуха через проточные полости воздушных термоплат, отличающийся тем, что формируют зону для прохождения и распределения потока атмосферного воздуха через проточные полости воздушных термоплат, разбивают ее на независимые участки с шагом, зависящим от количества выделяющегося тепла на единицу площади, через проточные полости воздушных термоплат пропускают скоростной воздушный поток атмосферного воздуха, возникающий при движении летательного аппарата, причем воздушный поток направляют последовательно от первого участка по направлению движения летательного аппарата к последующим участкам.1. The method of air cooling of heat-generating equipment located outside the aircraft, including thermal contact between the heat-generating surfaces of the equipment and air thermal boards, the movement of atmospheric air through the flow cavities of air thermal circuits, characterized in that they form a zone for the passage and distribution of atmospheric air flow through the flow cavities of air thermal plates, divide it into independent sections with a step depending on the amount of heat released per unit area, h Through flowing cavities of air thermal boards, a high-speed air stream of atmospheric air, which occurs during the movement of the aircraft, is passed, and the air flow is directed sequentially from the first section in the direction of movement of the aircraft to subsequent sections. 2. Система для реализации способа воздушного охлаждения тепловыделяющей аппаратуры, расположенной снаружи летательных аппаратов, включающая несущую конструкцию, воздушный канал, состоящий из воздуховодов и воздухозаборника с установленной в нем заслонкой для перекрытия доступа воздуха, систему управления, электрически связанную с узлом управления заслонкой, датчики температуры, установленные на поверхности тепловыделяющей аппаратуры, отличающаяся тем, что несущая конструкция представляет собой объемную крепежную раму, образованную ярусами, каждый из которых состоит, по крайней мере, из четырех силовых профилей, установленных по принципу колодезной кладки с консолями, на которых установлены теплообменники, выполненные в виде воздушных термоплат, каждая из которых установлена под углом 45° по ходу движения воздушного потока и имеет две термостатируемые поверхности, на которых размещена тепловыделяющая аппаратура, в систему введен воздушный тракт, состоящий из коллектора, образованного внутренней частью колодезной кладки силовых профилей, и проточных полостей воздушных термоплат, при этом в коллекторе установлены герметизирующие перегородки, разделяющие его на независимые участки, каждый из которых снабжен воздуховодом, установленным в угловых зонах крепежной рамы, и диффузором.2. A system for implementing the method of air cooling of fuel equipment located outside the aircraft, including the supporting structure, an air channel consisting of air ducts and an air intake with a shutter installed therein to shut off air access, a control system electrically connected to the shutter control unit, temperature sensors mounted on the surface of the heat-generating equipment, characterized in that the supporting structure is a three-dimensional mounting frame formed tiers, each of which consists of at least four power profiles installed on the principle of well laying with consoles, on which heat exchangers are installed, made in the form of air thermal plates, each of which is installed at an angle of 45 ° in the direction of the air flow and it has two thermostatic surfaces on which the heat-generating equipment is placed, an air path is introduced into the system, consisting of a collector formed by the inside of the well masonry of power profiles, and flow cavities termoplat ear, thus established in the reservoir sealing septum, dividing it into independent portions, each of which is provided with a duct installed in the corner areas of the mounting frame, and the diffuser.
RU2016107562A 2016-03-01 2016-03-01 Air cooling method of heat generating equipment, located outside aircrafts, and system for its implementation RU2632057C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016107562A RU2632057C2 (en) 2016-03-01 2016-03-01 Air cooling method of heat generating equipment, located outside aircrafts, and system for its implementation

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016107562A RU2632057C2 (en) 2016-03-01 2016-03-01 Air cooling method of heat generating equipment, located outside aircrafts, and system for its implementation

Publications (2)

Publication Number Publication Date
RU2016107562A true RU2016107562A (en) 2017-09-06
RU2632057C2 RU2632057C2 (en) 2017-10-02

Family

ID=59798610

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016107562A RU2632057C2 (en) 2016-03-01 2016-03-01 Air cooling method of heat generating equipment, located outside aircrafts, and system for its implementation

Country Status (1)

Country Link
RU (1) RU2632057C2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2710025C2 (en) * 2017-09-20 2019-12-24 Дмитрий Валерьевич Хачатуров Cooling method of power semiconductor devices

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2731043C2 (en) * 2019-01-09 2020-08-28 Российская Федерация, от имени которой выступает федеральное государственное казенное учреждение "Управление авиации Федеральной службы безопасности Российской Федерации" Aviation suspended container with payload
RU2747320C1 (en) * 2020-09-04 2021-05-04 федеральное государственное автономное образовательное учреждение высшего образования "Северо-Кавказский федеральный университет" Method for cooling unmanned aerial vehicle and device for implementing method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4869071A (en) * 1988-03-24 1989-09-26 Sundstrand Corporation Cooling system for an aircraft pod
DE102006046114B4 (en) * 2006-09-28 2012-02-02 Airbus Operations Gmbh Cooling arrangement for cooling a heat body for an aircraft
RU99449U8 (en) * 2010-06-15 2011-01-20 Открытое Акционерное Общество Таганрогский авиационный научно-технический комплекс им. Г.М. Бериева (ОАО ТАНТК им. Г.М. Бериева) CONTROL DEVICE FOR BLINDS OF BLINDS FOR REGULATING THE AIR CONSUMPTION THROUGH THE AIRCRAFT HEAT EXCHANGER
RU104151U1 (en) * 2010-11-02 2011-05-10 Открытое акционерное общество "Туполев" DEVICE BLOWING THE EQUIPMENT

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2710025C2 (en) * 2017-09-20 2019-12-24 Дмитрий Валерьевич Хачатуров Cooling method of power semiconductor devices

Also Published As

Publication number Publication date
RU2632057C2 (en) 2017-10-02

Similar Documents

Publication Publication Date Title
JP6906033B2 (en) Passive roof exhaust system
Fulpagare et al. Effect of plenum chamber obstructions on data center performance
IN2014DE02482A (en)
RU2016107562A (en) The method of air cooling of fuel equipment located outside the aircraft, and a system for its implementation
US20160165760A1 (en) Rack and method of cooling electronic device
RU2008129540A (en) EVAPORATIVE COOLING DEVICE
US9426903B1 (en) Cooling air stack for computer equipment
JP6375101B2 (en) How to ventilate the warehouse
JP2013162052A5 (en)
CN112840292A (en) System and method for cooling computing devices within a facility
RU2515530C2 (en) Device of conditioning for cooling of air in cabinet for electronic devices
CN103673573A (en) Straight-through drying oven with air curtain system
CN102404975B (en) Data center
JP5428968B2 (en) Cooling system
WO2013076853A1 (en) Cooling device and electronic apparatus
KR101597506B1 (en) Constant temperature and humidity air conditioning system
JP2015040667A5 (en)
CN104411148A (en) Thermal radiation protection cabinet
JP2015218947A (en) Air conditioning system
KR101604847B1 (en) dehumidifier device for a control panel
JP2017105876A (en) Target core sensor device
TWM602772U (en) Baking box configuration module
JP6779479B2 (en) Temperature control unit, temperature control system using temperature control unit, and temperature control building structure using temperature control unit
CN203980207U (en) A kind of radiator and there is the LED light fixture of this radiator
CN104519713A (en) Heat dissipation device