Fuel injection nozzle and method of use

• US 6,554,202 B2
• Filed: 05/10/2002
• Issued: 04/29/2003
• Est. Priority Date: 05/13/1996
• Status: Expired due to Term

• Current Assignee: Universidad De Savilla
• Original Assignee: Universidad de Sevilla
• Inventors: Ganan-Calvo, Alfonso
• Primary Examiner(s): Ganey, Steven J.
• Application Number:
  US10/144,089
• Publication Number:
  US 20020185550A1
• Time in Patent Office: 354 Days
• Field of Search: 239/8, 239/290, 239/291, 239/338, 239/346, 239/371, 239/400, 239/410, 239/419, 239/419.3, 239/422, 239/423, 239/424, 239/428, 239/434.5, 128/200.21, 128/205.11, 128/204.16, 128/911, 261/76, 261/78.1, 261/78.2, 261/115, 261/116
• US Class Current: 239/8
• CPC Class Codes: A61M 15/0065 Inhalators with dosage or measuring devices A61M15/0028 takes precedence; dosage devices incorporated in aerosol cans B65D83/52
• CPC Class Codes: A61M 15/025 Bubble jet droplet ejection devices
• CPC Class Codes: A61M 2202/064 Powder
• CPC Class Codes: B01F 23/232 using flow-mixing means for introducing the gases, e.g. baffles
• CPC Class Codes: B01F 25/30 Injector mixers mixing by creating vortex flow B01F25/10
• CPC Class Codes: B01F 33/3011 using a sheathing stream of a fluid surrounding a central stream of a different fluid, e.g. for reducing the cross-section of the central stream or to produce droplets from the central stream
• CPC Class Codes: B01J 2219/00378 Piezoelectric or ink jet dispensers
• CPC Class Codes: B05B 1/02 designed to produce a jet, spray, or other discharge of particular shape or nature, e.g. in single drops, or having an outlet of particular shapeB05B1/26, B05B1/28, B05B1/34 take precedence
• CPC Class Codes: B05B 7/0475 with means for deflecting the peripheral gas flow towards the central liquid flow B05B7/0458 takes precedence
• CPC Class Codes: B05B 7/061 with several liquid outlets discharging one or several liquids
• CPC Class Codes: B05B 7/065 an inner gas outlet being surrounded by an annular adjacent liquid outlet
• CPC Class Codes: B05B 7/066 with an inner liquid outlet surrounded by at least one annular gas outlet
• CPC Class Codes: B05B 7/0884 the outlet orifices for jets constituted by a liquid or a mixture containing a liquid being aligned
• CPC Class Codes: B82Y 30/00 Nanotechnology for materials or surface science, e.g. nanocomposites
• CPC Class Codes: C40B 60/14 for creating libraries
• CPC Class Codes: F02M 43/04 Injectors peculiar thereto
• CPC Class Codes: F02M 67/10 Injectors peculiar thereto, e.g. valve less type
• CPC Class Codes: F02M 69/047 injectors with air chambers, e.g. communicating with atmosphere for aerating the nozzles F02M69/325 takes precedence
• CPC Class Codes: F02M 69/08 characterised by the fuel being carried by compressed air into main stream of combustion-air
• CPC Class Codes: F23D 11/106 medium and fuel meeting at the burner outlet
• CPC Class Codes: G01N 15/1409 : Handling samples, e.g. injecting samples
• CPC Class Codes: G01N 2015/1406 : Control of droplet point
• CPC Class Codes: G01N 21/01 : Arrangements or apparatus for facilitating the optical investigation
• CPC Class Codes: Y10S 977/773 : Nanoparticle, i.e. structure having three dimensions of 100 nm or less
• CPC Class Codes: Y10S 977/888 : Shaping or removal of materials, e.g. etching
• CPC Class Codes: Y10S 977/89 : Deposition of materials, e.g. coating, cvd, or ald
• CPC Class Codes: Y10S 977/896 : Chemical synthesis, e.g. chemical bonding or breaking

Abstract

The invention is directed to a stable capillary microjet and a monodisperse aerosol formed when the microjet dissociates. A variety of devices and methods are disclosed which allow for the formation of a stream of a first fluid (e.g. a liquid) characterized by forming a stable capillary microjet over a portion of the stream wherein the microjet portion of the stream is formed by a second fluid (e.g. a gas). The second fluid is preferably in a different state from the first fluid—liquid-gas or gas-liquid combinations. However, the first and second fluids may be two different fluids in miscible in each other. The stable capillary microjet comprises a diameter d_j at a given point A in the stream characterized by the formula: $d_j\cong {\left(\frac{8{\rho }_1}{{\Pi }^2\Delta P_g}\right)}^{\frac{1}{4}}Q^{\frac{1}{2}}$

wherein d_j is the diameter of the stable microjet, ≡ indicates approximately equally to where an acceptable margin of error is ±10%, ρ_l is the density of the liquid and ΔP_g is change in gas pressure of gas surrounding the stream at the point A.

Claims

1. A method of producing concentrically positioned streams, comprising the steps of:

(a) forcing a liquid formulation comprising a first liquid through a channel of a first feeding source in a manner which causes a stream of the first liquid to be expelled from a first exit opening at a first velocity;

(b) forcing a liquid comprising a second liquid through a second channel concentrically positioned around the first channel in a manner which causes a stream of the second liquid to be expelled from a second exit opening at a velocity which is substantially the same as the first velocity whereby the stream of second liquid is concentrically positioned around the stream of the first liquid;

(c) forcing a gas through a pressure chamber in a manner which causes the gas to exit the pressure chamber from an exit orifice positioned downstream of the concentrically positioned streams of the first and second liquids;

wherein the density of the liquid formulation is substantially the same as the density of the second liquid, and wherein the gas focuses the concentrically positioned streams to a stable unified jet which flows out of the chamber exit orifice.

2. The method of claim 1, wherein the first liquid comprises a pharmaceutically active drug.

3. The method of claim 1, wherein the stable unified jet has a length in a range of from about 1 micron to about 50 mm.

4. The method of claim 1, wherein the stable unified jet is maintained, at least in part, by tangential viscous stresses exerted by the gas on a surface of the jet in an axial direction of the jet.

5. The method of claim 1, wherein the stable unified jet formed in step (c) is comprises a diameter d_j at a given point A in the stream characterized by the formula:

$d_j\cong <br><br>{\left(\frac{8<br><br>{\mathrm{\rho <br><br>}}_1}{{\prod <br><br>}^2<br><br>\mathrm{\Delta <br><br>}<br><br>\text{\hspace{1em}<br><br>}<br><br>P_g}\right)}^{\frac{1}{4}}<br><br>Q^{\frac{1}{2}}$

wherein d_j is the diameter of the stable unified jet, indicates approximately equally to where an acceptable margin of error is ±

10% ρ

_l is the average density of the liquid of the unified jet and Δ

P_g is change in gas pressure of gas surrounding the jet at the point A and Q is the total flow rate of the stable unified jet.

6. The method of claim 5, wherein d_j is a diameter in a range of about 1 micron to about 1 mm.

7. The method of claim 5, wherein the stable unified jet formed in step (c) has a length in a range of from about 1 micron to about 50 mm.

8. The method of claim 5, wherein the stable unified jet formed in step (c) is maintained, at least in part, by tangential viscous stresses exerted by the gas on a surface of the jet in an axial direction of the jet.

9. The method of claim 5, wherein the stable unified jet formed in step (c) is further characterized by a slightly parabolic axial velocity profile.

10. The method of claim 1, wherein Δ

P=P₀−

P₁, the difference in pressure through the presssure chamber exit orifice, is equal to or less than twenty times the surface tension of the second liquid with the gas, divided by the radius of the stable unified jet.

11. The method of claim 1, wherein the first liquid comprises a pharmaceutically active drug and the second liquid comprises a coating material.