RU2001135440A - Method for increasing jet propulsion - Google Patents

Method for increasing jet propulsion

Info

Publication number
RU2001135440A
RU2001135440A RU2001135440/28A RU2001135440A RU2001135440A RU 2001135440 A RU2001135440 A RU 2001135440A RU 2001135440/28 A RU2001135440/28 A RU 2001135440/28A RU 2001135440 A RU2001135440 A RU 2001135440A RU 2001135440 A RU2001135440 A RU 2001135440A
Authority
RU
Russia
Prior art keywords
jet propulsion
increasing
increasing jet
nozzle
channel
Prior art date
Application number
RU2001135440/28A
Other languages
Russian (ru)
Other versions
RU2221727C2 (en
Inventor
Дмитрий Алексеевич Хлесткин
Original Assignee
Дмитрий Алексеевич Хлесткин
Filing date
Publication date
Application filed by Дмитрий Алексеевич Хлесткин filed Critical Дмитрий Алексеевич Хлесткин
Priority to RU2001135440/11A priority Critical patent/RU2221727C2/en
Priority claimed from RU2001135440/11A external-priority patent/RU2221727C2/en
Publication of RU2001135440A publication Critical patent/RU2001135440A/en
Application granted granted Critical
Publication of RU2221727C2 publication Critical patent/RU2221727C2/en

Links

Claims (1)

Способ увеличения реактивной тяги истекающей струи путем нагрева выбрасываемой через канал или сопло рабочей жидкости, отличающийся тем, что нагрев рабочей жидкости производят без изменения ее агрегатного и фазного состояния до температуры, превышающей температуру насыщения жидкости при давлении среды, в которую происходит истечение струи, а канал или сопло выполняют с расширяющимся выходным участком.A method of increasing the reactive thrust of an outflowing jet by heating the working fluid discharged through a channel or nozzle, characterized in that the working fluid is heated without changing its aggregate and phase state to a temperature exceeding the saturation temperature of the liquid at the pressure of the medium into which the jet flows, and the channel or the nozzle is performed with an expanding outlet section.
RU2001135440/11A 2001-12-28 2001-12-28 Method of increasing reactive thrust of escaping jet RU2221727C2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2001135440/11A RU2221727C2 (en) 2001-12-28 2001-12-28 Method of increasing reactive thrust of escaping jet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2001135440/11A RU2221727C2 (en) 2001-12-28 2001-12-28 Method of increasing reactive thrust of escaping jet

Publications (2)

Publication Number Publication Date
RU2001135440A true RU2001135440A (en) 2003-08-20
RU2221727C2 RU2221727C2 (en) 2004-01-20

Family

ID=32090568

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2001135440/11A RU2221727C2 (en) 2001-12-28 2001-12-28 Method of increasing reactive thrust of escaping jet

Country Status (1)

Country Link
RU (1) RU2221727C2 (en)

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