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SU553455A1 - Device for measuring specific flow in supersonic gas flow - Google Patents

Device for measuring specific flow in supersonic gas flow

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Publication number
SU553455A1
SU553455A1 SU1937758A SU1937758A SU553455A1 SU 553455 A1 SU553455 A1 SU 553455A1 SU 1937758 A SU1937758 A SU 1937758A SU 1937758 A SU1937758 A SU 1937758A SU 553455 A1 SU553455 A1 SU 553455A1
Authority
SU
USSR - Soviet Union
Prior art keywords
flow
gas flow
supersonic gas
measuring specific
flow rate
Prior art date
Application number
SU1937758A
Other languages
Russian (ru)
Inventor
Иван Сергеевич Баринов
Борис Евгеньевич Жестков
Анатолий Васильевич Липин
Original Assignee
Предприятие П/Я Г-4903
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 Предприятие П/Я Г-4903 filed Critical Предприятие П/Я Г-4903
Priority to SU1937758A priority Critical patent/SU553455A1/en
Application granted granted Critical
Publication of SU553455A1 publication Critical patent/SU553455A1/en

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Description

1one

Изобретение относитс  к измерительной технике и предназначено дл  измерени  удельного расхода в сверхзвуковом потоке газа .The invention relates to a measurement technique and is intended to measure the specific flow rate in a supersonic gas flow.

Известно устройство дл  измерени  удельного расхода в сверхзвуковом потоке газа, содержащее конический заборник газа, камеру и датчик давлени , в котором расход газа, поступаюш .его через заборник, измер етс  по темпу роста добавлени  в камере 1.A device for measuring the specific flow rate in a supersonic gas flow is known, comprising a conical gas intake, a chamber and a pressure sensor in which the flow rate of gas flowing through the intake is measured by the growth rate of the addition in chamber 1.

Недостатком такого устройства  вл етс  то, что в процессе эксперимента измен етс  давление в камере, что приводит к изменению режима течени  газа через заборник и увеличивает погрешность измерений.The disadvantage of this device is that during the experiment the pressure in the chamber changes, which leads to a change in the mode of gas flow through the intake and increases the measurement error.

Кроме того, определение расхода по темпу роста давлени  в емкости не позвол ет получить высокую точность измерени  и измер ть потоки значительно разреженных газов и потоки с высокой эпитальпией.In addition, the determination of the flow rate based on the rate of pressure growth in the tank does not allow for obtaining high accuracy of measurement and measuring the flows of significantly diluted gases and flows with high epitapal.

Целью изобретени   вл етс  повышение точности измерени  и расширение области применени .The aim of the invention is to improve the measurement accuracy and the expansion of the field of application.

Эта цель достигаетс  тем, что в устройстве камера выполнена проточной - подсоединена к откачивающей системе и снабжена теплообменником .This goal is achieved by the fact that in the device the chamber is made flow through - connected to the pumping system and equipped with a heat exchanger.

На чертеже представлена схема устройства.The drawing shows a diagram of the device.

Устройство содержит «оническнй заборник 1 с острыми кромками входного отверсти .The device comprises a “one-side intake 1” with sharp edges of the inlet.

датчик давлени  2, трассу 3,  вл ющуюс  одновременно теплообменником, и откачивающую вакуумную систему 4. Все элементы устройства соединены вакуумно плотно.pressure sensor 2, track 3, which is simultaneously a heat exchanger, and a pump-down vacuum system 4. All elements of the device are vacuum-tightly connected.

Измер ют удельный расход при помощи предлагаемого устройства следующим образом . Конический заборник газа ввод т в поток . Расход газа через заборник 1 (при отсутствии отошедшего скачка уплотнени ) равеиThe specific consumption is measured using the proposed device as follows. A conical gas intake is introduced into the stream. Gas consumption through intake 1 (in the absence of a detached shock wave)

G pvS,G pvS,

где р - плотность,where p is the density

V - скорость потока газа,V is the gas flow rate,

5 - площадь входного отверсти  заборника. Расход G измер етс  по величине давлени  Р, регистрируемого датчиком 2, и расходной характеристике откачивающей системы 4. Величина удельного расхода pv определ етс  по измеренной величине расхода G5 - the area of the inlet of the intake. The flow rate G is measured by the pressure value P detected by sensor 2 and the flow characteristic of the pumping system 4. The specific flow rate pv is determined from the measured flow rate G

-1-one

Наличие теплообменника позвол ет проводить измерени  в потоках с высокой (низкой) температурой торможени .The presence of a heat exchanger allows measurements in streams with a high (low) stagnation temperature.

Claims (1)

1. Поттер Дж. Кинслоу М., Арни Дж. Бейли А. «Исследование гиперзвуковых течений под редакцией Риддел  Ф. Р. «Мир, М., 1964 г., стр. 422.1. Potter J. Kinslow M., Arnie J. Bailey A. “Investigation of hypersonic flows, edited by Riddell F. R.“ The World, M., 1964, p. 422. 1one
SU1937758A 1973-06-25 1973-06-25 Device for measuring specific flow in supersonic gas flow SU553455A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU1937758A SU553455A1 (en) 1973-06-25 1973-06-25 Device for measuring specific flow in supersonic gas flow

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU1937758A SU553455A1 (en) 1973-06-25 1973-06-25 Device for measuring specific flow in supersonic gas flow

Publications (1)

Publication Number Publication Date
SU553455A1 true SU553455A1 (en) 1977-04-05

Family

ID=20558177

Family Applications (1)

Application Number Title Priority Date Filing Date
SU1937758A SU553455A1 (en) 1973-06-25 1973-06-25 Device for measuring specific flow in supersonic gas flow

Country Status (1)

Country Link
SU (1) SU553455A1 (en)

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