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RU2016101689A - Power plant or engine "Two-pulse jet engine" - Google Patents

Power plant or engine "Two-pulse jet engine" Download PDF

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Publication number
RU2016101689A
RU2016101689A RU2016101689A RU2016101689A RU2016101689A RU 2016101689 A RU2016101689 A RU 2016101689A RU 2016101689 A RU2016101689 A RU 2016101689A RU 2016101689 A RU2016101689 A RU 2016101689A RU 2016101689 A RU2016101689 A RU 2016101689A
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RU
Russia
Prior art keywords
engine
special
jet engine
power plant
power
Prior art date
Application number
RU2016101689A
Other languages
Russian (ru)
Inventor
Аслан Солтамбекович Тедтоев
Original Assignee
Аслан Солтамбекович Тедтоев
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Publication date
Application filed by Аслан Солтамбекович Тедтоев filed Critical Аслан Солтамбекович Тедтоев
Priority to RU2016101689A priority Critical patent/RU2016101689A/en
Publication of RU2016101689A publication Critical patent/RU2016101689A/en

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Claims (1)

Двухимпульсный реактивный двигатель - силовой агрегат, содержащий классическую схему реактивного двигателя, вырабатывающего энергию реактивной силой расширяющихся газов, отличающийся тем, что он за счет особенной формы, конструкции и оборудования специальной системы сопел для выхода реактивной струи, имеющих удлиненную изгибающуюся форму, состоящих из двух частей, организованных таким образом, что реактивная струя, вырываясь по первой части из камеры сгорания, упирается в устроенный на границах первой и второй части сопел специально под определенным углом размещенный упор и не теряя своей скорости, выходит наружу по второй части сопел, создавая удвоенный импульс движения, давая возможность дважды использовать одно и то же количество выделенной энергии, а также обеспечить особенную экономичность такой силовой установки без снижения мощности, обуславливая, в итоге, существенное увеличение коэффициента полезного действия, а также придание летательному аппарату, на котором он установлен, принципиально нового распределения тяговых усилий, помимо того, ранее недостижимого сочетания свойств скорости, маневренности (как в вертикальной, так и в горизонтальной плоскостях) и живучести.A two-pulse jet engine is a power unit containing the classical scheme of a jet engine generating energy by the reactive power of expanding gases, characterized in that it is due to the special shape, design, and equipment of a special nozzle system for exiting a jet stream having an elongated bending shape, consisting of two parts organized in such a way that the jet stream, breaking out along the first part of the combustion chamber, abuts against the nozzles arranged at the boundaries of the first and second parts At a certain angle, the placed stop and without losing its speed, goes out along the second part of the nozzles, creating a double impulse of movement, making it possible to use the same amount of released energy twice, as well as to ensure the special efficiency of such a power plant without reducing power, causing as a result, a significant increase in efficiency, as well as giving the aircraft on which it is installed, a fundamentally new distribution of traction, in addition, previously unattainable A combination of the properties of speed, maneuverability (both vertically and horizontally) and survivability.
RU2016101689A 2016-01-20 2016-01-20 Power plant or engine "Two-pulse jet engine" RU2016101689A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2016101689A RU2016101689A (en) 2016-01-20 2016-01-20 Power plant or engine "Two-pulse jet engine"

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2016101689A RU2016101689A (en) 2016-01-20 2016-01-20 Power plant or engine "Two-pulse jet engine"

Related Child Applications (1)

Application Number Title Priority Date Filing Date
RU2018140952A Division RU2018140952A (en) 2018-11-20 2018-11-20 Engine "Two-pulse jet engine"

Publications (1)

Publication Number Publication Date
RU2016101689A true RU2016101689A (en) 2017-07-26

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ID=59498384

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2016101689A RU2016101689A (en) 2016-01-20 2016-01-20 Power plant or engine "Two-pulse jet engine"

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RU (1) RU2016101689A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019136535A1 (en) * 2018-01-09 2019-07-18 Драгомир КОНСТАНТИНОВ Device for redirecting and lending momentum to streams of fluids under pressure
WO2020146928A1 (en) * 2019-01-15 2020-07-23 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid and capturing the impulse thereof
WO2021184085A1 (en) * 2020-03-16 2021-09-23 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid and capturing the impulse thereof
WO2021226681A1 (en) * 2020-05-11 2021-11-18 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019136535A1 (en) * 2018-01-09 2019-07-18 Драгомир КОНСТАНТИНОВ Device for redirecting and lending momentum to streams of fluids under pressure
WO2020146928A1 (en) * 2019-01-15 2020-07-23 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid and capturing the impulse thereof
WO2021184085A1 (en) * 2020-03-16 2021-09-23 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid and capturing the impulse thereof
WO2021226681A1 (en) * 2020-05-11 2021-11-18 Драгомир КОНСТАНТИНОВ Device for passively reversing flows of pressurized fluid

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Legal Events

Date Code Title Description
FA92 Acknowledgement of application withdrawn (lack of supplementary materials submitted)

Effective date: 20180718