Device for ejecting a diphasic mixture

Patent metadata

Field	Value
Publication number	US-9352340-B2
Application number	US-44443207-A
Country	US
Kind code	B2
Filing date	Aug 27, 2007
Priority date	Oct 4, 2006
Publication date	May 31, 2016
Grant date	May 31, 2016

Abstract

A device for ejecting an at least diphasic mixture includes an injection inlet for a liquid and a gas, a distribution chamber for producing a first liquid-gas mixture, an ejection nozzle of the first liquid-gas mixture in a main direction defined by an axis-vector. The ejection nozzle has a geometry comprising, on its length at least, a minimal section or neck at a location of the axis-vector. Among others things, due to the nozzle geometry, the expansion obtained inside the ejection nozzle allows the first liquid-gas mixture from the distribution chamber to be converted into a second mixture, according to the flow configuration, consisting for instance of a diphasic mist jet having an ejection range and liquid particle size that can be controlled according to the liquid and gas mass flow and to the absolute pressure at the injection inlet.

First claim

The invention claimed is:

1. A device for ejecting an at least diphasic mixture, comprising:
at least one injection inlet for introducing a liquid and a gas;
a distribution chamber for producing a first liquid/gas mixture communicating with said injection inlet;
an ejection nozzle communicating with said distribution chamber for ejecting the first liquid/gas mixture, said ejection nozzle having a nozzle outlet, and said ejection nozzle extending in a main direction defined by a vector axis and having a geometry formed, over a length thereof, with the nozzle inlet having a first converging access zone with a steep gradient having a steep gradient axial length along said vector axis followed by a second converging zone with a shallow gradient and a second converging zone axial length along the vector axis, said second converging zone leading to a minimum cross-section defining a neck at a given location along the vector axis, said minimum cross-section causing a pressure reduction within said ejection nozzle, allowing the first liquid/gas mixture originating from said distribution chamber to be converted, in a direction of flow, into a second liquid/gas mixture at said nozzle outlet; said outlet being a diverging zone having a diverging zone axial length along the vector axis, the steep gradient axial length being less than the diverging zone axial length, which is less than the second converging zone axial length, said vector being a main axis of said ejection nozzle, said nozzle inlet and said nozzle outlet being symmetric about said main axis of said ejection nozzle;
wherein an ejection range of the second liquid/gas mixture and a particle size of the liquid in droplet form is controllable as a function of a mass flow rate of the liquid and the gas and of an absolute pressure at said injection inlet.

2. The device according to claim 1 , wherein an ejection jet of the second mixture is a diphasic mist jet primarily following the vector axis and wherein a particle size in the mist jet, a range and a volume spread outside the vector axis are controllable.

3. The device according to claim 2 , wherein a pressure at said injection inlet into said distribution chamber is relatively low and a mist jet velocity is relatively high.

4. The device according to claim 3 , wherein the pressure at said injection inlet is less than 20 bar and the mist jet velocity lies above 50 m/s.

5. The device according to claim 1 , wherein a gas injection inlet and a liquid injection inlet of said at least one injection inlet are at a common level ahead of said nozzle inlet.

6. The device according to claim 1 , wherein said ejection nozzle is one of a plurality of ejection nozzles provided with separate vector axes and disposed on walls of said distribution chamber.

7. The device according to claim 6 , wherein said ejection nozzles are disposed to achieve a mist coverage area or volume that extends at least over a defined range.

8. The device according to claim 6 , wherein said distribution chamber is disposed between a stator and a rotor with an axis of rotation, and wherein said at least one ejection nozzle is disposed on said rotor.

9. The device according to claim 8 , wherein at least one ejection nozzle is disposed on said stator.

10. The device according to claim 8 , wherein certain vector axes of said ejection nozzles are arranged asymmetrically on said rotor relative to a plane comprising an axis of rotation.

11. The device according to claim 10 , wherein the certain vector axes of said ejection nozzles are oriented with an offset by an angle of between 0° and 90° beneath a plane perpendicular to the axis of rotation.

12. The device according to claim 8 , wherein the vector axes of said ejection nozzles do not intersect with the axis of rotation and an arrangement thereof is suitable for producing a rotation of said rotor at a controlled speed of rotation.

13. The device according to claim 6 , wherein said ejection nozzles have mutually different geometries with an influence on a particle size and/or a range of the second liquid/gas mixture.

14. The device according to claim 1 , wherein the liquid is water and the gas is compressed air.

15. A device for ejection an at least diaphasic mixture, comprising:
at least one injection inlet for introducing a liquid and a gas;
a distribution chamber for producing a first liquid/gas mixture communicating with said injection inlet;
an ejection nozzle communicating with said distribution chamber for ejecting the first liquid/gas mixture, said ejection nozzle having a nozzle inlet, a nozzle outlet, and said ejection nozzle extending in a main direction defined by a vector axis and having a geometry formed, over a length thereof, with the nozzle inlet having a first converging access zone with a steep gradient having a steep gradient axial length along said vector axis followed by a second converging zone with a shallow gradient and a second converging zone axial length along the vector axis, said second converging zone leading to a minimum cross-section defining a neck at a given location along the vector axis, and said minimum cross-section causing a pressure reduction of the gas within said ejection nozzle, allowing the first liquid/gas mixture originating from said distribution chamber to be converted, in a direction of flow, into a second liquid/gas mixture at said nozzle outlet, said outlet being a diverging zone having a diverging zone axial length along the vector axis, the steep gradient axial length being less than the diverging zone axial length, which is less than the second converging zone axial length, and wherein the gas accelerates and vectorizes a large proportion of the droplets along the vector axis;
wherein an ejection range of the second liquid gas mixture and a particle size of the liquid in droplet form is controllable as a function of a mass flow rate of the liquid and the gas and of an absolute pressure at said injection inlet.

16. The device according to claim 15 , wherein said nozzle inlet and said nozzle outlet are symmetric about said vector axis of said ejection nozzle.

17. A method, comprising: providing the device according to claim 1 , and ejecting a liquid/gas mixture through for extinguishing a fire, for fire prevention by moistening with low liquid consumption, or for material cooling using water as a primary liquid and optionally admixing an extinguishing agent, a moistening agent, or a cooling agent.

18. A method of surface-treating a material, which comprises:
providing the device according to claim 1 ; and
injecting water as the liquid and optionally admixing a cleaning agent, and cleaning the material; or
injecting liquid mainly containing a coloring agent and applying paint onto the material; or
producing a second mixture containing a chemical solution which is liquid or partially solid with a small particle size, and abrasively treating the material.

19. A method, comprising: providing the device according to claim 1 and employing the device for propellant feed/atomization for a rocket engine or for optimized fuel injection for a combustion engine.

20. A fuel ejection method, comprising: providing the device according to claim 1 , injecting fuel into the injection inlet and ejecting the fuel from the at least one ejection nozzle and combusting the fuel and forming a large flame.

21. A propulsion method, which comprises providing the device according to claim 1 and employing the ejection nozzle as a propulsion means for a vehicle.

Assignees

• Bourrilhon Thibaut
• Dusser Bernard
• Fernandes Patrick
• Thibault Jean-Paul
• Siemens Sas
• Univ Grenoble Alpes
• Centre Nat Rech Scient

Inventors

• Bourrilhon Thibaut
• Dusser Bernard
• Fernandes Patrick
• Thibault Jean-Paul

Classifications

• B05B3/0417

  comprising a liquid driven rotor, e.g. a turbine · CPC title

• B05B7/0012 Primary

  Apparatus for achieving spraying before discharge from the apparatus · CPC title

• B05B7/0483

  with gas and liquid jets intersecting in the mixing chamber · CPC title

• A62C31/05

  with two or more outlets · CPC title

• B05B7/0475

  with means for deflecting the peripheral gas flow towards the central liquid flow (B05B7/0458 takes precedence) · CPC title