FIELD: engines and pumps.
SUBSTANCE: pancake hypersonic straight-flow air breathing engine (HSFABE) for bringing the transport vehicle into movement includes many equally-spaced posts separated with paths, and pilot portion of the post, which is enclosed inside each of the above posts. Geometry of pilot portion of the post is effective to receive the pilot portion of air of supersonic air flow from HSFABE air intake and to reduce the pilot portion of air to subsonic speed. The rest portion of the main air of supersonic air flow bypasses the pilot portion of the post via paths and remains at supersonic speed. Each post includes inward directed pilot fuel atomisers and outward directed main fuel atomisers. Pilot portion of the post is enclosed in the limits of each post.
EFFECT: reducing heat load of combustion chamber, shortening the length of combustion chamber at using the fuel injection directly to the flow.
33 cl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD AND AIR VEHICLE FOR MOVING IN PLANETARY ATMOSPHERE WITH SPEEDS ABOVE THE FIRST SPACE AND HIGHLY INTEGRATED HYPERSONIC VEHICLE APPARATUS (VERSIONS) FOR IMPLEMENTATION OF THE METHOD | 2012 |
|
RU2618831C2 |
| HYPERSONIC RAMJET ENGINE | 2017 |
|
RU2691702C2 |
| HYPERSONIC RAMJET ENGINE AND METHOD OF ORGANIZATION OF COMBUSTION | 2003 |
|
RU2262000C2 |
| EXPERIMENTAL HYPERSONIC RAMJET ENGINE | 2003 |
|
RU2238420C1 |
| AIRCRAFT RAMJET ENGINE | 2004 |
|
RU2269022C2 |
| STRAIGHT-FLOW AIR-JET ENGINE | 2020 |
|
RU2736670C1 |
| METHOD OF SETTING-UP COMBUSTION IN HYPERSONIC RAMJET ENGINE AND HYPERSONIC RAMJET ENGINE FOR REALIZATION OF THIS METHODS (VERSIONS) | 1994 |
|
RU2082017C1 |
| HYPERSONIC RAMJET ENGINE AND CONCEPT OF COMBUSTION | 2013 |
|
RU2529935C1 |
| HYPERSONIC RAMJET ENGINE AND CONCEPT OF COMBUSTION | 2012 |
|
RU2516735C1 |
| ENGINE OF HYPERSONIC AIRCRAFT | 2015 |
|
RU2591361C1 |
