RU2013109079A - KNOCK TRANSMISSION DEVICE - Google Patents
KNOCK TRANSMISSION DEVICE Download PDFInfo
- Publication number
- RU2013109079A RU2013109079A RU2013109079/06A RU2013109079A RU2013109079A RU 2013109079 A RU2013109079 A RU 2013109079A RU 2013109079/06 A RU2013109079/06 A RU 2013109079/06A RU 2013109079 A RU2013109079 A RU 2013109079A RU 2013109079 A RU2013109079 A RU 2013109079A
- Authority
- RU
- Russia
- Prior art keywords
- couplings
- cones
- longitudinal section
- hydraulic diameter
- truncated
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R7/00—Intermittent or explosive combustion chambers
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/02—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being intermittent, i.e. pulse-jet
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fluidized-Bed Combustion And Resonant Combustion (AREA)
- Gear-Shifting Mechanisms (AREA)
Abstract
1. Устройство для передачи детонации выполнено в виде расширяющегося конуса, отличающееся тем, что расширяющийся конус состоит из нескольких усеченных конусов с разными углами раствора, при этом между конусами с разными углами раствора дополнительно устанавливаются муфты с длиной вдоль оси трубы lне более 2 D, где D- гидравлический диаметр выходного сечения усеченного конуса.2. Устройство по п.1, отличающееся тем, что усеченные конусы в продольном сечении имеют прямолинейную конфигурацию и их суммарная длина (с учетом муфт) составляет не более 9-10 D, где D - гидравлический диаметр на выходе из инициирующего узла.3. Устройство по п.1, отличающееся тем, что муфты в продольном сечении имеют различную конфигурацию.1. The device for transmitting detonation is made in the form of an expanding cone, characterized in that the expanding cone consists of several truncated cones with different solution angles, while couplings with a length along the pipe axis l of not more than 2 D are additionally installed between the cones with different solution angles, where D is the hydraulic diameter of the output section of the truncated cone. 2. The device according to claim 1, characterized in that the truncated cones in a longitudinal section have a straight configuration and their total length (including couplings) is not more than 9-10 D, where D is the hydraulic diameter at the outlet of the initiating node. The device according to claim 1, characterized in that the couplings in longitudinal section have a different configuration.
Claims (3)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
PCT/RU2010/000402 WO2012011830A1 (en) | 2010-07-19 | 2010-07-19 | Device for transmitting a detonation |
Publications (1)
Publication Number | Publication Date |
---|---|
RU2013109079A true RU2013109079A (en) | 2014-09-10 |
Family
ID=45497057
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2013109079/06A RU2013109079A (en) | 2010-07-19 | 2010-07-19 | KNOCK TRANSMISSION DEVICE |
Country Status (2)
Country | Link |
---|---|
RU (1) | RU2013109079A (en) |
WO (1) | WO2012011830A1 (en) |
Families Citing this family (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN109114591A (en) * | 2018-07-25 | 2019-01-01 | 南京理工大学 | It is a kind of to change the combustion chamber for realizing detonation control by wall angle |
CN109114593A (en) * | 2018-07-25 | 2019-01-01 | 南京理工大学 | A kind of multi-step cascade combustion chamber for controlling detonation |
CN109114590A (en) * | 2018-07-25 | 2019-01-01 | 南京理工大学 | A kind of combustion chamber of movable step control detonation |
CN114297812B (en) * | 2021-12-31 | 2024-08-20 | 北京理工大学 | Design method of triangle lattice center input type face synchronous explosion-propagation network |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1335004A (en) * | 1962-06-09 | 1963-08-16 | Snecma | Non-homogeneous flow gas generator |
RU2059852C1 (en) * | 1993-06-10 | 1996-05-10 | Саратовская научно-производственная фирма "Растр" | Pulse hypersonic ram-jet engine |
RU2080466C1 (en) * | 1993-06-10 | 1997-05-27 | Саратовская научно-производственная фирма "Растр" | Combined chamber of detonation combustion pulsejet engine |
RU2282044C1 (en) * | 2004-11-22 | 2006-08-20 | Бордовский Антон Владимирович | Detonation combustion pulsejet engine |
-
2010
- 2010-07-19 RU RU2013109079/06A patent/RU2013109079A/en not_active Application Discontinuation
- 2010-07-19 WO PCT/RU2010/000402 patent/WO2012011830A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2012011830A1 (en) | 2012-01-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FA92 | Acknowledgement of application withdrawn (lack of supplementary materials submitted) |
Effective date: 20150701 |