SU38396A1 - Reactive internal combustion turbine - Google Patents
Reactive internal combustion turbineInfo
- Publication number
- SU38396A1 SU38396A1 SU119644A SU119644A SU38396A1 SU 38396 A1 SU38396 A1 SU 38396A1 SU 119644 A SU119644 A SU 119644A SU 119644 A SU119644 A SU 119644A SU 38396 A1 SU38396 A1 SU 38396A1
- Authority
- SU
- USSR - Soviet Union
- Prior art keywords
- internal combustion
- combustion turbine
- reactive internal
- turbine
- chambers
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title description 8
- 238000007906 compression Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 1
Description
Изобретение касаетс турбины внутреннего горени с отдельными камерами горени дл каждого сопла. В предлагаемой турбине применен р д труб, соедин ющих отдельные камеры горени с камерой сжати и имеющих различную длину с целью получени последовательных вспышек в различных камерах .The invention relates to an internal combustion turbine with separate combustion chambers for each nozzle. In the proposed turbine, a series of tubes are used that connect separate combustion chambers with a compression chamber and having different lengths in order to obtain consecutive flashes in different chambers.
На схематическом чертеже фиг. 1 изображает продольный разрез турбины и фиг. 2-вид ротора турбины спереди.In the schematic drawing of FIG. 1 shows a longitudinal section of a turbine; and FIG. 2 is a front view of the turbine rotor.
В предлагаемой турбине ротор, представл ющий собою сегнерово колесо, имеет камеры горен41 /-V, сообщающиес через клапаны А и турбины В (фиг. 1) с камерой сжати . Указанным трубам Si, BZ, BS, Bi, В-а придана различна длина с той целью, чтобы сжата в камере горюча смесь, проход по трубам с одинаковою скоростью, посту пала последовательно в камеры /, ///, V. II, IV. Вследствие этого вспышки в ксмерах горени происход т не одновременно , а последовательно, т. е. двигатель работает, как многоцилиндровый.In the proposed turbine, the rotor, which is the Segner wheel, has Goren41 / -V chambers communicating via valves A and turbines B (Fig. 1) with the compression chamber. The specified pipes Si, BZ, BS, Bi, B are given a different length in order to compress the combustible mixture in the chamber, pass through the pipes at the same speed, post successively to the chambers /, ///, V. II, IV . As a result, flashes in combustion chambers do not occur simultaneously, but sequentially, i.e., the engine works like a multi-cylinder one.
Предмет изобретени .The subject matter of the invention.
Реактивна турбина внутреннего горени с отдельными камерами горение дл каждого сопла, отличающа с применением труб 5i, SB, Ss, 4, 5, соедин ющих отдельные камеры горени /-V и имеющих различную длину, с целью получени последовательных вспышек в различных камерах.An internal combustion turbine with separate combustion chambers for each nozzle, characterized by using tubes 5i, SB, Ss, 4, 5 connecting separate combustion chambers (-V) and having different lengths, with the aim of obtaining consecutive flashes in different chambers.
к авторскому свидетельству Л. Н. Петрова и Н. Л. Михайлова № 38396to the author's testimony of L. N. Petrov and N. L. Mikhailov No. 38396
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Related Parent Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| SU120975 Division | |||
| SU12975 Division |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| SU38396A1 true SU38396A1 (en) | 1934-08-31 |
| SU38395A1 SU38395A1 (en) | 1934-08-31 |
Family
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