Apparatus for a fuel system

• US 4,898,329 A
• Filed: 11/04/1987
• Issued: 02/06/1990
• Est. Priority Date: 11/04/1987
• Status: Expired due to Term

• Current Assignee: United Technologies Corporation (Rtx Corporation)
• Original Assignee: United Technologies Corporation (Rtx Corporation)
• Inventors: Wright, Richard R., Wilcox, Gilbert B., Davis, Franklin J.
• Primary Examiner(s): Kashnikow, Andres
• Assistant Examiner(s): Forman, Michael J.
• Application Number:
  US07/117,117
• Time in Patent Office: 825 Days
• Field of Search: 239/13, 239/397.5, 239/600, 239/590.3, 239/553.3, 285/187, 285/905
• US Class Current: 239/13
• CPC Class Codes: F23R 3/283 Attaching or cooling of fuel injecting means including supports for fuel injectors, stems, or lances

Abstract

A fuel nozzle assembly 32 which extends into a flow path 18 for working medium gases is disclosed. Various construction details which decrease the amount of heat transfer to the fuel are developed. The assembly includes an external heat shield 50 and an internal heat shield 98 which provide longitudinally overlapping insulating gaps 52, 102 between the fuel and the hot working medium gases. In particular, the insulating gap 52 extends to the inlet 94 of the fuel nozzle support.

Claims

1. A fuel nozzle assembly for a machine for the type which is adapted to extend into a flow path for working medium gases, wherein the improvement comprises:

a fuel nozzle,

a support for the fuel nozzle, the support having an external surface, an inlet, and an internal surface bounding a passage for fuel which has a longitudinal dimension and which extends from the inlet through the support,

an external heat shield spaced from the support to leave an external insulating gap therebetween which extends longitudinally with respect to and outwardly of at least a portion of the passage,

an internal heat shield which is disposed within said passage and which is spaced from the internal surface of the support leaving an internal insulating gap therebetween which longitudinally overlaps the external insulating gap and extends to at least an upstreammost edge of the inlet of the fuel nozzle support.

2. The fuel nozzle assembly of claim 1 wherein the internal heat shield has a first end and a second end, wherein the fuel nozzle assembly includes an inlet connector for flowing fuel which has an upstream end and a downstream end, the inlet connector being integrally attached to the fuel nozzle, and having a passage for fuel, the passage in the inlet connector having a longitudinal direction, the passage being in flow communication with the passage in the fuel nozzle support, the inlet connector having a midsection having a region for positioning the second end of the internal heat shield, the region of the midsection being spaced longitudinally from the fuel nozzle support and wherein the internal heat shield extends past the downstream end of the connector in the connector passage to the midsection and is engaged by the midsection.

3. The fuel nozzle of claim 2 wherein the exterior of the midsection of the connector is surrounded by cooling air.

4. The fuel nozzle assembly of claim 3 wherein the inlet connector has a base section which extends from the midsection and which is engaged by the fuel nozzle support and wherein the midsection has a cross-section area which is smaller than the cross-section area of the base section.

5. The fuel nozzle assembly of claim 4 wherein the inlet connector has an inlet section which extends from the midsection and which includes a conical seat extending about the interior of the inlet section wherein the fuel nozzle assembly includes a one-piece transfer tube and screen and wherein the transfer tube is disposed in the passage in the inlet connector and engage the inlet connector at the conical seat in the inlet section.

6. The fuel nozzle assembly of claim 1 wherein the midsection slidably engages the internal heat shield.

7. The fuel assembly of claim 6 wherein the exterior of the midsection of the connector is surrounded by cooling air.

8. The fuel nozzle assembly of claim 7 wherein the inlet connector has a base section which extends from the midsection and which is engaged by the fuel nozzle support and wherein the midsection has a cross-sectional area which is smaller than the cross-sectional area of the base section.

9. The fuel assembly of claim 8 wherein the inlet connector has an inlet section which extends from the midsection and which includes a conical seat extending about the interior of the inlet section wherein the fuel nozzle assembly includes a one-piece transfer tube and screen and wherein the transfer tube is disposed in the passage in the inlet connector and engages the inlet connector at the conical seat in the inlet section.

10. A fuel nozzle assembly for a rotary machine which is adapted to extend into a flow path for hot working medium gases, the fuel nozzle assembly including:

a fuel nozzle;

a support for the fuel nozzle having

a first end which positions the fuel nozzle,

a second end which is adapted by an inlet to pass fuel, the second end having an inlet region, an orifice region and an internal insulating gap region extending between the inlet region and the orifice region,

a passage for fuel extending from the inlet through the support to place the fuel nozzle in flow communication with a source of fuel, the passage extending longitudinally through the second end, the passage having a first cross-sectional area in the inlet region which adaps the support to receive an inlet connector, and the passage having a second cross-sectional area in the internal insulating gap region which is smaller than the first cross-sectional area;

an inlet connector having a passage for fuel in flow communication with the passage in the support, the inlet connector further having,

a base section which has a cross-sectional area A₁, which is disposed in the inlet region of the support and which is fixed to the support,

an inlet section which is spaced from the support having an outwardly facing internal seal seat extending about the exterior of the passage and an outwardly facing seal extending about the exterior of the inlet connector and,

a midsection which extends between the inlet section and the base section and which has a cross-sectional area A₂, which is smaller than the cross-sectional area A₁ ;

a tube assembly including

a tube having a passage therethrough disposed in the passage of the inlet connector, the tube having a first end and a second end, a seal seat which engages the internal seal seat of the inlet connector, the tube having a flange at the first end which extends from the connector, the flange having a seal extending about the exterior of the tube which adapts the tube to engage the interior of a fuel supply element and,

a screen which is attached to the second end of the tube assembly and which is disposed in the connector passage permitting flow communication between the passage in the tube and the passages in the connector and the support;

an external shield which extends about the exterior of the support and is spaced from the support leaving an external insulating gap therebetween which overlaps longitudinally the internal insulating gap region;

an internal shield disposed in the connector passage and the support passage, the internal shield having an orifice disposed within the orifice region of the support, the internal shield being spaced from the inlet connector and the support leaving an internal insulating gap therebetween upstream of the orifice region;

wherein the internal insulating gap overlaps longitudinally the external insulating gap and extends longitudinally to the inlet of the support, wherein the internal shield is fixed to the support in the orifice region and slidably engages the midsection of the connector.

11. A method for shielding fuel flowing through a passage in a fuel nozzle assembly of a gas turbine engine, the passage having a longitudinal dimension, the engine having a fuel nozzle support which is attached to a casing of the engine and which has an inlet for said passage said inlet being at an upstreammost edge of said fuel nozzle support, which includes the steps of:

shielding the fuel stream with a longitudinally extending insulating gap outwardly of the passage; and

,

shielding the passage with an internal insulating gap internally of the passage which longitudinally overlaps the external gap and extends longitudinally to at least said upstreammost edge of the inlet to the passage.