Sump tank for a gas turbine engine

Patent metadata

Field	Value
Publication number	US-10208637-B2
Application number	US-201615276538-A
Country	US
Kind code	B2
Filing date	Sep 26, 2016
Priority date	Sep 26, 2016
Publication date	Feb 19, 2019
Grant date	Feb 19, 2019

Abstract

A sump tank for use with a gas turbine engine in offshore conditions is disclosed. In embodiments, the sump tank includes two circuitous lubricant flow paths. Each flow path includes an end compartment, a side compartment, and a tube that feed to a central compartment. The baffles used to form the central compartment are angled so as to cause the lubricant entering from the tubes to swirl, which may increase the residence time of the lubricant and may help ensure that any entrained air is released from the lubricant prior to entering the suction line.

First claim

What is claimed is:

1. A sump tank for a gas turbine engine, the sump tank comprising:
a tank body for containing a lubricant, the tank body including
a tank base,
a tank top above the tank base,
a first endwall extending from the tank base to the tank top,
a second endwall extending from the tank base to the tank top opposite the first endwall,
a first sidewall extending from the tank base to the tank top, and
a second sidewall extending from the tank base to the tank top opposite the first sidewall;

a first end baffle extending from the first sidewall to the second sidewall and from the tank base to the tank top, the first end baffle being located closer to the first endwall than the second endwall and forming a first end compartment with the first endwall, and portions of the first sidewall and the second sidewall;
a second end baffle extending from the first sidewall to the second sidewall and from the tank base to the tank top, the second end baffle being located closer to the second endwall than the first end baffle and forming a second end compartment with the second endwall, and portions of the first sidewall and the second sidewall;
a first central baffle extending from the first end baffle towards the first sidewall at a central baffle angle, the first central baffle joined to the first end baffle adjacent a midpoint of the first end baffle and closer to the first sidewall than to the second sidewall;
a second central baffle extending from the second end baffle towards the first sidewall at the central baffle angle, the second central baffle joined to the second end baffle adjacent a midpoint of the second end baffle and closer to the first sidewall than to the second sidewall, the second central baffle forming a first side compartment with the first central baffle, and portions of the first end baffle, the second end baffle and the first sidewall, the first side compartment located between the first end compartment and the second end compartment;
a third central baffle extending from the second end baffle towards the second sidewall at the central baffle angle, the third central baffle joined to the second end baffle adjacent the midpoint of the second end baffle and closer to the second sidewall than to the first sidewall;
a fourth central baffle extending from the first end baffle towards the second sidewall at the central baffle angle, the fourth central baffle joined to the first end baffle adjacent the midpoint of the first end baffle and closer to the second sidewall than to the first sidewall, the fourth central baffle forming a second side compartment with the third central baffle, and portions of the first end baffle, the second end baffle and the second sidewall, the second side compartment located between the first end compartment and the second end compartment, and the fourth central baffle forming a central compartment with the first central baffle, the second central baffle, the third central baffle, the first end baffle and the second end baffle, the central compartment located between the first end baffle and the second end baffle as well as between the first side compartment and the second side compartment;
a first tube including a first tube inlet located in the first side compartment adjacent to the second end baffle and a first tube outlet located in the central compartment adjacent the first end baffle, the first tube including a first bend;
a second tube including a second tube inlet located in the second side compartment adjacent to the first end baffle and a second tube outlet located in the central compartment adjacent the second end baffle, the second tube including a second bend;
a first end lubricant passage in the first end baffle adjacent the tank base, the first end lubricant passage fluidly connecting the first end compartment and the first side compartment;
a second end lubricant passage in the second end baffle adjacent the tank base, the second end lubricant passage fluidly connecting the second end compartment and the second side compartment;
return lines connected to the tank top at return locations above the first end compartment adjacent the first end baffle and above the second end compartment adjacent the second end baffle; and
a suction line including a suction line inlet located in the central compartment adjacent to a centroid of the central compartment.

2. The sump tank of claim 1 , further comprising:
a tank vent located above the suction line inlet;
a first end air passage located in the first end baffle adjacent the tank top and fluidly connecting the first end compartment and the first side compartment;
a second end air passage located in the second end baffle adjacent the tank top and fluidly connecting the second end compartment and the second side compartment;
a first central air passage in the first central baffle adjacent the tank top;
a second central air passage in the second central baffle adjacent the tank top;
a third central air passage in the third central baffle adjacent the tank top; and
a fourth central air passage in the fourth central baffle adjacent the tank top.

3. The sump tank of claim 2 , wherein the first central baffle and the second central baffle intersect and are integral, and the third central baffle and the fourth central baffle intersect and are integral.

4. The sump tank of claim 3 , further comprising:
a first side division baffle extending from the first sidewall to the intersection of the first and second central baffles subdividing the first side compartment, the first side division baffle is offset from the tank top forming a first side divider air passage therebetween and is offset from the tank base forming a first side divider lubricant passage therebetween;
a second side division baffle extending from the second sidewall to the intersection of the third and fourth central baffles subdividing the second side compartment, the second side division baffle being offset from the tank top forming a second side air passage therebetween and being offset from the tank base forming a second side lubricant passage therebetween;
an end division baffle extending from the second endwall to the second end baffle, the end division baffle subdividing the second end compartment; and
an end divider lubricant passage in the end division baffle adjacent to the tank base.

5. The sump tank of claim 1 , wherein a first cross-sectional area of the first tube and a second cross-sectional area of the second tube are sized to maintain the velocity of the lubricant high enough to cause the lubricant in the central compartment to swirl and low enough to prevent turbulent flow of the lubricant.

6. The sump tank of claim 1 , further comprising a level transmitter in the central compartment adjacent the suction line inlet.

7. The sump tank of claim 1 , wherein the central baffle angle is from 45 to 65 degrees.

8. A sump tank for a gas turbine engine, the sump tank comprising:
a tank body for containing a lubricant, the tank body including
a tank base,
a tank top above the tank base,
a first endwall extending from the tank base to the tank top,
a second endwall extending from the tank base to the tank top opposite the first endwall,
a first sidewall extending from the tank base to the tank top, and
a second sidewall extending from the tank base to the tank top opposite the first sidewall;

a first end compartment including a first rectangular prism shape, the first end compartment boundary including the first endwall, the first sidewall, the second sidewall, and a first end baffle extending from the first sidewall to the second sidewall parallel to the first endwall, the first end baffle being located closer to the first endwall than to the second en

Assignees

• Solar Turbines Inc

Inventors

• Mulock Mark Justin

Classifications

• F01M11/065

  Position · CPC title

• F01M11/064 Primary

  Movement · CPC title

• F16N31/004

  combined with container · CPC title

• F01D25/18 Primary

  Lubricating arrangements (of machines or engines in general F01M) · CPC title

• F01M11/08

  Separating lubricant from air or fuel-air mixture before entry into cylinder (separating in general B01D) · CPC title