RU2006137541A - Pulsating Air-Jet Engine - Google Patents

Pulsating Air-Jet Engine Download PDF

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Publication number
RU2006137541A
RU2006137541A RU2006137541/06A RU2006137541A RU2006137541A RU 2006137541 A RU2006137541 A RU 2006137541A RU 2006137541/06 A RU2006137541/06 A RU 2006137541/06A RU 2006137541 A RU2006137541 A RU 2006137541A RU 2006137541 A RU2006137541 A RU 2006137541A
Authority
RU
Russia
Prior art keywords
jet engine
pulsating air
detonation
combustion chamber
inlet pipe
Prior art date
Application number
RU2006137541/06A
Other languages
Russian (ru)
Inventor
Константин Валентинович Мигалин (RU)
Константин Валентинович Мигалин
Алексей Ильич Сиденко (RU)
Алексей Ильич Сиденко
Кирилл Константинович Мигалин (RU)
Кирилл Константинович Мигалин
Original Assignee
Константин Валентинович Мигалин (RU)
Константин Валентинович Мигалин
Алексей Ильич Сиденко (RU)
Алексей Ильич Сиденко
Кирилл Константинович Мигалин (RU)
Кирилл Константинович Мигалин
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 Константин Валентинович Мигалин (RU), Константин Валентинович Мигалин, Алексей Ильич Сиденко (RU), Алексей Ильич Сиденко, Кирилл Константинович Мигалин (RU), Кирилл Константинович Мигалин filed Critical Константин Валентинович Мигалин (RU)
Priority to RU2006137541/06A priority Critical patent/RU2006137541A/en
Publication of RU2006137541A publication Critical patent/RU2006137541A/en

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  • Combustion Methods Of Internal-Combustion Engines (AREA)

Claims (1)

Пульсирующий воздушно-реактивный двигатель, содержащий, в частности, камеру сгорания, впускной патрубок, резонаторную трубу, топливные форсунки и механизм инициирования детонации, отличающийся тем, что механизм инициирования детонации смонтирован на торцевой стенке камеры сгорания, с противоположной стороны от впускного патрубка, и выполнен в виде детонационной форкамеры, на входе которой установлены воздушный клапан и топливная форсунка.A pulsating jet engine containing, in particular, a combustion chamber, an inlet pipe, a resonator pipe, fuel nozzles and a detonation initiation mechanism, characterized in that the detonation initiation mechanism is mounted on the end wall of the combustion chamber, on the opposite side from the inlet pipe, and is made in the form of a detonation prechamber, at the entrance of which an air valve and a fuel injector are installed.
RU2006137541/06A 2006-10-23 2006-10-23 Pulsating Air-Jet Engine RU2006137541A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
RU2006137541/06A RU2006137541A (en) 2006-10-23 2006-10-23 Pulsating Air-Jet Engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU2006137541/06A RU2006137541A (en) 2006-10-23 2006-10-23 Pulsating Air-Jet Engine

Publications (1)

Publication Number Publication Date
RU2006137541A true RU2006137541A (en) 2008-04-27

Family

ID=39452814

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2006137541/06A RU2006137541A (en) 2006-10-23 2006-10-23 Pulsating Air-Jet Engine

Country Status (1)

Country Link
RU (1) RU2006137541A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2668777C1 (en) * 2017-04-06 2018-10-02 Габлия Юрий Александрович Method for restricting actions of aggressive crowd and a device for implementing the method

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2668777C1 (en) * 2017-04-06 2018-10-02 Габлия Юрий Александрович Method for restricting actions of aggressive crowd and a device for implementing the method

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Legal Events

Date Code Title Description
FA94 Acknowledgement of application withdrawn (non-payment of fees)

Effective date: 20081020