SU826137A1 - Apparatus for pulsative burning of fuel - Google Patents

Apparatus for pulsative burning of fuel Download PDF

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Publication number
SU826137A1
SU826137A1 SU792809110A SU2809110A SU826137A1 SU 826137 A1 SU826137 A1 SU 826137A1 SU 792809110 A SU792809110 A SU 792809110A SU 2809110 A SU2809110 A SU 2809110A SU 826137 A1 SU826137 A1 SU 826137A1
Authority
SU
USSR - Soviet Union
Prior art keywords
length
combustion
tubes
pulsating
exhaust chamber
Prior art date
Application number
SU792809110A
Other languages
Russian (ru)
Inventor
Виталий Степанович Северянин
Семен Михайлович Добкин
Эдуард Михайлович Телегин
Анатолий Вадимович Вакуленко
Original Assignee
Severyanin Vitalij S
Dobkin Semen M
Telegin Eduard M
Vakulenko Anatolij V
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 Severyanin Vitalij S, Dobkin Semen M, Telegin Eduard M, Vakulenko Anatolij V filed Critical Severyanin Vitalij S
Priority to SU792809110A priority Critical patent/SU826137A1/en
Application granted granted Critical
Publication of SU826137A1 publication Critical patent/SU826137A1/en

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  • Fluidized-Bed Combustion And Resonant Combustion (AREA)

Description

(54) УСТРОЙСТВО ДЛЯ ПУЛЬСИРУЮЩЕГО СЖИГАНИЯ(54) DEVICE FOR PULSING BURNING

ТОПЛИВАFUEL

Claims (2)

Изобретение относитс  к энергетике и может быть использовано дл  устройст работа которых сопровождаетс  низкочас тотным шумом. Известно устройство дл  пульсирующего сжигани  топлива, содержащее камеру воспламенени , сообщенную с выхлопной камерой двум  резонансными тру бами 1. J. Недостатком известного устройства  вл ютс  низкие эксплуатационные карак гёристики, обусловленные высоким уровнем шума при работе. Цель изобретени  - повышение эффективности сжигани . Поставленна  цель достигаетс  тем, что длина одной из труб в три раза пре- вьииает длину другой. На чертеже схематично изображено устройство цл  пульсирующего сжигани  топлива. Устройство содержит камеру 1 воспла менени ., сообщенную с выхлопной камеро 2, двум  резонансными трубами 3 и 4. При работе устройства дл  пульсирующего сжигани  топливо сгорает в камере 1 воспламенени  и по резонансным трубам 3 и 4 направл етс  в ;ы)слопную камеру The invention relates to power engineering and can be used for devices whose operation is accompanied by low frequency noise. A device for pulsating fuel combustion is known, which contains an ignition chamber in communication with the exhaust chamber by two resonant tubes 1. J. A disadvantage of the known device is the low operating costs due to the high noise level during operation. The purpose of the invention is to increase the combustion efficiency. The goal is achieved by the fact that the length of one of the pipes exceeds the length of the other one by three times. The drawing shows schematically a device for the pulsating fuel combustion system. The device contains an ignition chamber 1. communicated with an exhaust chamber 2, two resonant tubes 3 and 4. When the pulsating combustion apparatus is operated, the fuel burns in the ignition chamber 1 and through the resonant tubes 3 and 4 is directed into; 2. Благодар  тому, что длина одной из труб в три раза превышает длину другой, продукты сгорани  приход т в выхлопную камеру в режимах пульсации с противоположными фазами, в результате сложени  которых уменьшаетс  излу.ченив шума. Формула изобретени  Устройство дл  пульсирующего сжигани  топлива, содержащее камеру воспламенени , сообщенную с выхлопной камерой двум  резонангными трубами, отличающеес  тем, что, с целью повышени  эффективности сжигани , длина оцной из труб в три раза превышает длину другой. Источники информации, прин тые во внимание при экспертизе 1. Авторское свидетельство СССР № 416518, КЛ. Р 23 С 3/02, 1971.2. Due to the fact that the length of one of the pipes is three times the length of the other, the products of combustion come into the exhaust chamber in pulsation modes with opposite phases, as a result of which the radiation decreases. Claims An apparatus for pulsating fuel combustion, comprising an ignition chamber connected to the exhaust chamber by two resonance tubes, characterized in that, in order to increase the efficiency of combustion, the slug length of the tubes is three times the length of the other. Sources of information taken into account in the examination 1. USSR author's certificate number 416518, CL. R 23 3/02, 1971.
SU792809110A 1979-08-15 1979-08-15 Apparatus for pulsative burning of fuel SU826137A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SU792809110A SU826137A1 (en) 1979-08-15 1979-08-15 Apparatus for pulsative burning of fuel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SU792809110A SU826137A1 (en) 1979-08-15 1979-08-15 Apparatus for pulsative burning of fuel

Publications (1)

Publication Number Publication Date
SU826137A1 true SU826137A1 (en) 1981-04-30

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Family Applications (1)

Application Number Title Priority Date Filing Date
SU792809110A SU826137A1 (en) 1979-08-15 1979-08-15 Apparatus for pulsative burning of fuel

Country Status (1)

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SU (1) SU826137A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4884963A (en) * 1988-08-05 1989-12-05 Gas Research Institute Pulse combustor
US4926798A (en) * 1988-08-05 1990-05-22 Gas Research Institute Process for pulse combustion
US5454711A (en) * 1990-11-19 1995-10-03 De Stichting Impuls Burner for pulsating combustion
US5800153A (en) * 1995-07-07 1998-09-01 Mark DeRoche Repetitive detonation generator
US5937635A (en) * 1996-11-27 1999-08-17 Lockheed Martin Corporation Pulse detonation igniter for pulse detonation chambers

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4884963A (en) * 1988-08-05 1989-12-05 Gas Research Institute Pulse combustor
US4926798A (en) * 1988-08-05 1990-05-22 Gas Research Institute Process for pulse combustion
US5454711A (en) * 1990-11-19 1995-10-03 De Stichting Impuls Burner for pulsating combustion
US5800153A (en) * 1995-07-07 1998-09-01 Mark DeRoche Repetitive detonation generator
US5937635A (en) * 1996-11-27 1999-08-17 Lockheed Martin Corporation Pulse detonation igniter for pulse detonation chambers

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