SU676849A1 - Gravity heat tube - Google Patents

Gravity heat tube

Info

Publication number
SU676849A1
SU676849A1 SU782586714A SU2586714A SU676849A1 SU 676849 A1 SU676849 A1 SU 676849A1 SU 782586714 A SU782586714 A SU 782586714A SU 2586714 A SU2586714 A SU 2586714A SU 676849 A1 SU676849 A1 SU 676849A1
Authority
SU
USSR - Soviet Union
Prior art keywords
heat tube
gravity heat
ejector
evaporator
gravity
Prior art date
Application number
SU782586714A
Other languages
Russian (ru)
Inventor
Файзулла Каримович Рашидов
Юсуф Каримович Рашидов
Original Assignee
Ф. К. Рашидов и Ю. К. Рашидов
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 Ф. К. Рашидов и Ю. К. Рашидов filed Critical Ф. К. Рашидов и Ю. К. Рашидов
Priority to SU782586714A priority Critical patent/SU676849A1/en
Application granted granted Critical
Publication of SU676849A1 publication Critical patent/SU676849A1/en

Links

Landscapes

  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)

Description

Дает тепло. Одновременно из-за разности давлений между конденсатором 2 и приемной камерой эжектора 7 конденсат по жидкостному каналу 5 направл етс  в приемную камеру эжектора 7 и, увлека сь паром, поступающим в эжектор 7 из испарител  1 по паровому каналу 3, попадает в конденсатосборник 9, а оттуда по каналу 6, благодар  гидростатическому давлению, самотеком в испаритель 1.It gives heat. At the same time, due to the pressure difference between the condenser 2 and the receiving chamber of the ejector 7, the condensate through the liquid channel 5 is directed to the receiving chamber of the ejector 7 and, entrained in steam entering the ejector 7 from the evaporator 1 through the steam channel 3, enters the condensate collector 9, and from there through channel 6, due to hydrostatic pressure, by gravity to the evaporator 1.

За счет непрерывного процесса испарение - конденсаци  между испарителем 1 и конденсатором 2 поддерживаетс  разность давлений, обусловленна  разностью температуры кипени  и конденсации теплоносител , что обеспечивает необходимый дл  работы эжектора 7 перепад давлений.Due to the continuous evaporation-condensation process between the evaporator 1 and condenser 2, the pressure difference is maintained due to the difference in the boiling temperature and condensation of the coolant, which provides the pressure drop necessary for the operation of the ejector 7.

Использование энергии высо| оскоростного потока пара в эжекторе позвол ет увеличить максимальное значение передаваемого теплового потока.Energy use is high | The rapid flow of steam in the ejector allows the maximum value of the transferred heat flux to be increased.

Гравитационна  теплова  труба обеспечивает также увеличение перепада высот между испарителем и конденсатором.The gravitational heat pipe also provides an increase in the height difference between the evaporator and the condenser.

Claims (1)

1. Авторское свидетельство СССР № 664014, кл. F 28D 15/00, 1974.1. USSR author's certificate No. 664014, cl. F 28 D 15/00, 1974.
SU782586714A 1978-03-02 1978-03-02 Gravity heat tube SU676849A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU782586714A SU676849A1 (en) 1978-03-02 1978-03-02 Gravity heat tube

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU782586714A SU676849A1 (en) 1978-03-02 1978-03-02 Gravity heat tube

Publications (1)

Publication Number Publication Date
SU676849A1 true SU676849A1 (en) 1979-07-30

Family

ID=20751958

Family Applications (1)

Application Number Title Priority Date Filing Date
SU782586714A SU676849A1 (en) 1978-03-02 1978-03-02 Gravity heat tube

Country Status (1)

Country Link
SU (1) SU676849A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336837A (en) * 1981-02-11 1982-06-29 The United States Of America As Represented By The United States Department Of Energy Entirely passive heat pipe apparatus capable of operating against gravity
US4467861A (en) * 1982-10-04 1984-08-28 Otdel Fiziko-Tekhnicheskikh Problem Energetiki Uralskogo Nauchnogo Tsentra Akademii Nauk Sssr Heat-transporting device
CN103015954A (en) * 2012-12-03 2013-04-03 中国石油天然气股份有限公司 Producing well shaft combined gravity assisted heat pipe

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4336837A (en) * 1981-02-11 1982-06-29 The United States Of America As Represented By The United States Department Of Energy Entirely passive heat pipe apparatus capable of operating against gravity
US4467861A (en) * 1982-10-04 1984-08-28 Otdel Fiziko-Tekhnicheskikh Problem Energetiki Uralskogo Nauchnogo Tsentra Akademii Nauk Sssr Heat-transporting device
CN103015954A (en) * 2012-12-03 2013-04-03 中国石油天然气股份有限公司 Producing well shaft combined gravity assisted heat pipe
CN103015954B (en) * 2012-12-03 2015-07-08 中国石油天然气股份有限公司 Producing well shaft combined gravity assisted heat pipe

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