Injection manifold with Tesla valves for rotating detonation engines
US-12098848-B2 · Sep 24, 2024 · US
US10151271B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10151271-B2 |
| Application number | US-201514754342-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 29, 2015 |
| Priority date | Jul 28, 2014 |
| Publication date | Dec 11, 2018 |
| Grant date | Dec 11, 2018 |
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A flow-management system may comprise a center body impermeable to air. A conical surface of the center body may face forward. A blocking surface of the center body may be coaxial with the conical surface and may comprise an annular recess. An annular ring may be aft of the center body and fluidly coupled with the blocking surface. A tube may encase the center body and annular ring. The annular ring may comprise an air-foil shape to direct a pulse to the blocking surface. The blocking surface may comprise a central peak and a circular ridge separated by the annular recess.
Opening claim text (preview).
What is claimed is: 1. A flow-management system, comprising: a center body impermeable to gas; a conical surface of the center body facing forward; a blocking surface of the center body coaxial with the conical surface and comprising an annular recess disposed between a central peak and a circular ridge, wherein the circular ridge extends rearward of the central peak; and an annular ring aft of the center body and fluidly coupled with the blocking surface, wherein the annular ring is symmetrical about a centerline axis, wherein a distance between the centerline axis and a forward edge of the annular ring is smaller than a distance between the centerline axis and an aft edge of the annular ring. 2. The flow-management system of claim 1 , further comprising a tube encasing the center body and annular ring. 3. The flow-management system of claim 1 , wherein the annular ring comprises an air-foil shape to direct a pulse to the blocking surface. 4. The flow-management system of claim 1 , wherein the center body is axially symmetric. 5. The flow-management system of claim 1 , further comprising a strut mounted to the conical surface of the center body. 6. A pulse detonation engine comprising: a tube; a center body fixed to the tube; a conical surface of the center body facing forward; a blocking surface of the center body coaxial with the conical surface and comprising an annular recess disposed between a central peak and a circular ridge, wherein the circular ridge extends rearward of the central peak, wherein the blocking surface is impermeable to gas; a duct defined by the conical surface and tube; and an annular ring aft of the center body comprising an air-foil shape configured to divert a pulse towards the blocking surface, wherein the annular ring is symmetrical about a centerline axis, wherein a distance between the centerline axis and a forward edge of the annular ring is smaller than a distance between the centerline axis and an aft edge of the annular ring. 7. The pulse detonation engine of claim 6 , wherein the air-foil shape of the annular ring is further configured to divert the pulse away from the duct. 8. The pulse detonation engine of claim 6 , wherein the conical surface is impermeable to air. 9. The pulse detonation engine of claim 6 , wherein the center body is axially symmetric. 10. The pulse detonation engine of claim 6 , further comprising: a first strut connecting the tube and center body; and a second strut connecting the tube and annular ring. 11. The pulse detonation engine of claim 6 , further comprising a detonation zone in the tube and aft of the annular ring, wherein the pulse originates from the detonation zone.
having aerodynamic valves · CPC title
the working fluid forming a resonating or oscillating gas column, i.e. the combustion chambers having no positively actuated valves, e.g. using Helmholtz effect · CPC title
the jet being intermittent, i.e. pulse-jet · CPC title
using valveless combustion chambers · CPC title
for controlling, signalling, or supervising the conveyance of a product · CPC title
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