Apparatus and method for determining luminosity of hydrocarbon fuels

• US 4,865,444 A
• Filed: 10/15/1987
• Issued: 09/12/1989
• Est. Priority Date: 04/05/1984
• Status: Expired due to Fees

• Current Assignee: Mobil Oil Corporation (Exxon Mobil Corporation)
• Original Assignee: Mobil Oil Corporation (Exxon Mobil Corporation)
• Inventors: Yan, Tsoung Y., Green, Gary J.
• Primary Examiner(s): McGraw, Vincent P.
• Application Number:
  US07/108,596
• Time in Patent Office: 698 Days
• Field of Search: 356/36, 356/315, 356/316
• US Class Current: 356/36
• CPC Class Codes: B01J 2/08 Gelation of a colloidal solution
• CPC Class Codes: B01J 35/51 Spheres
• 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 7/066 with an inner liquid outlet surrounded by at least one annular gas outlet
• CPC Class Codes: B05B 7/0892 the outlet orifices for jets constituted by a liquid or a mixture containing a liquid being disposed on a circle
• CPC Class Codes: C10L 1/00 Liquid carbonaceous fuels
• CPC Class Codes: F23D 11/10 the spraying being induced by a gaseous medium, e.g. water vapour

Abstract

Disclosed is apparatus comprising a means for injecting a controlled stream of hydrocarbon liquid into a concurrently flowing stream of gas in a Venturi forming droplets. Droplets are subsequently combusted in a gas stream. The level of radient emissions is measured photoelectrically. Results obtained are useful in predicting service life of combustor walls in jet engines and the like.

Claims

1. A method for determining the quality of a liquid hydrocarbon fuel by measuring its luminosity comprising:

(a) introducing a downflowing stream of linearly spaced droplets of said hydrocarbon fuel into a combustion zone;

(b) combusting said stream of droplets in said combustion zone; and

(c) measuring the intensity of the radiation emitted by said stream of droplets during said combustion.

2. The method of claim 1 wherein the spacing between said linearly spaced droplets is uniform.

3. The method of claim 1 wherein said linearly spaced droplets are of a uniform size.

4. The method of claim 1 wherein said combustion zone comprises a flowing stream of heated gas and air or oxygen.

5. The method of claim 1 wherein said combustion zone also contains a diluent gas.

6. The method of claim 1 wherein the temperature in said combustion zone is at a temperature of between about 1100°

and about 2000°

K.

7. The method of claim 1 wherein said combustion zone contains a hot combustion environment provided by the post-combustion gases from combusting a lean premixed mixture of methane, oxygen and nitrogen.

8. A method for determining the luminosity of a liquid hydrocarbon fuel comprising:

(a) introducing a downflowing stream of linearly spaced droplets of said liquid fuel into a downflowing moving stream of heated oxidizing gases;

(b) at least partially combusting said stream of droplets; and

(c) measuring the intensity of the radiation from said combusting stream of droplets at a plurality of locations in said stream.

9. The method of claim 8 wherein the measured intensity of (c) is utilized to predict liner life of a jet engine.

10. The method of claim 8 wherein the spacing between said linearly spaced droplets is uniform and about 50 to 500 droplet diameters.

11. The method of claim 8 wherein said linearly spaced droplets are of a uniform size.

12. The method of claim 8 wherein said stream of heated oxidizing gases comprises a burning mixture of fuel gas and oxygen or air.

13. The method of claim 8 wherein said combustion zone is at a temperature of between about 1100°

and about 2000°

K.

14. The method of claim 8 wherein the diameter of the individual droplets is about 50 to 500 microns.

15. A device for measuring the luminosity of a burning hydrocarbon liquid fuel comprising:

(a) a venturi positioned at or near the upper end of a transparent tubular member;

(b) a capillary tube having an open end positioned near the throat of said venturi;

(c) means for injecting a stream of liquid hydrocarbon from said capillary tube into said venturi and thence into said tubular member;

(d) means for injecting a stream of gas into the space defined between said venturi tube and said capillary tube, thereby forming a series of droplets of hydrocarbon liquid;

(e) means at or near the top of said tubular member for burning in the presence of excess oxygen a combustible gas and for igniting said droplets of hydrocarbon liquid; and

(f) means for measuring the luminosity of said burning droplets of hydrocarbon fuel as they flow through said tubular member.

16. The device of claim 15 wherein said means of measuring luminosity is photographic means.

17. The device of claim 15 wherein said means for measuring luminosity is a photodiode electronically connected with an oscilloscope.