Hydraulically driven de-oiler for gas turbine engines
A hydraulically driven de-oiler for gas turbine engines including a lubricant pumping section operatively coupled with a fuel impelling section, the lubricant pumping section and the fuel impelling section being divided by a lubricant to fuel divider; a helical sinus formed within the lubricant pumping section, the helical sinus configured to pump at least one of lubricant, and lubricant mist from a de-oiler tank inlet to a de-oiler tank outlet and configured to pump the air to a de-oiler air vent outlet in the absence of lubricant; and the fuel impelling section fluidly coupled with a fuel inlet and a fuel outlet, the fuel impelling section comprising impellers configured to receive a fluid flow of fuel and translate a flow energy from the fluid flow into a mechanical rotational energy and impart the mechanical rotational energy into the de-oiler.
1 . A hydraulically driven de-oiler for gas turbine engines comprising:
a lubricant pumping section operatively coupled with a fuel turbine impelling section, the lubricant pumping section and the fuel turbine impelling section being divided by a lubricant to fuel divider;
a helical sinus formed within the lubricant pumping section, the helical sinus configured to pump at least one of lubricant, and lubricant mist from a de-oiler tank inlet to a de-oiler tank outlet and configured to pump the air to a de-oiler air vent outlet in the absence of lubricant; and
the fuel turbine impelling section fluidly coupled with a fuel inlet and a fuel outlet, the fuel turbine impelling section comprising impellers configured to receive a fluid flow of fuel and translate a flow energy from the fluid flow into a mechanical rotational energy and impart the mechanical rotational energy into the de-oiler; wherein the fuel turbine impelling section is located radially outboard from the lubricant pumping section relative to the axis of the de-oiler, the fuel turbine impelling section is located between an exterior wall and the lubricant to fuel divider of the de-oiler.
2 . The hydraulically driven de-oiler for gas turbine engines according to claim 1 , wherein the helical sinus comprises lubricant impellers, the lubricant impellers being formed as contiguous helix shaped paddles that define a continuous flow passage with discrete pockets serially aligned along an axis of the de-oiler.
3 . The hydraulically driven de-oiler for gas turbine engines according to claim 2 , wherein the lubricant impellers are configured to rotate and impart mechanical rotary and axial motion to the lubricant mist and air to pump the lubricant mist and air through the de-oiler.
4 . The hydraulically driven de-oiler for gas turbine engines according to claim 2 , wherein the lubricant impellers are configured to impart centrifugal forces into the lubricant mist and air causing the lubricant to separate from the air.
5 . The hydraulically driven de-oiler for gas turbine engines according to claim 1 , wherein the lubricant to fuel divider is configured to transfer thermal energy from the lubricant pumping section to the fuel turbine impelling section such that the lubricant warms the fuel passing through the de-oiler.
6 . The hydraulically driven de-oiler for gas turbine engines according to claim 1 , further comprising:
a modified lubricant pumping section, the modified lubricant pumping section comprising a perforated divider, the perforated divider configured to separate the modified lubricant pumping section into a radially inner region and a radially outer region.
7 . A de-oiler system for a gas turbine engine comprising:
a lubrication system tank configured to contain lubricant, the lubricant fluidly coupled with at least one of the gas turbine engine, rotating hardware and bearings through a lubricant supply line;
a de-oiler operatively coupled with the lubrication system tank; the de-oiler comprising:
a lubricant pumping section operatively coupled with a fuel turbine impelling section, the lubricant pumping section and the fuel turbine impelling section being divided by a lubricant to fuel divider;
a helical sinus formed within the lubricant pumping section, the helical sinus configured to pump at least one of the lubricant, and a lubricant mist from a de-oiler tank inlet fluidly coupled with the lubrication system tank to a de-oiler tank outlet fluidly coupled with the lubrication system tank and configured to pump the air to a de-oiler air vent outlet in the absence of lubricant; and
the fuel turbine impelling section fluidly coupled with a fuel inlet and a fuel outlet, the fuel turbine impelling section comprising impellers configured to receive a fluid flow of fuel and translate a flow energy from the fluid flow into a mechanical rotational energy and impart the mechanical rotational energy into the de-oiler; wherein the fuel turbine impelling section is located radially outboard from the lubricant pumping section relative to the axis of the de-oiler, the fuel turbine impelling section is located between an exterior wall and the lubricant to fuel divider of the de-oiler.
8 . The de-oiler system for a gas turbine engine according to claim 7 , wherein the helical sinus comprises lubricant impellers, the lubricant impellers being formed as contiguous helix shaped paddles that define a continuous flow passage with pockets serially aligned along an axis of the de-oiler, wherein the lubricant impellers are configured to rotate and impart mechanical rotary and axial motion to the lubricant mist and air to pump the lubricant mist and air through the de-oiler, wherein the lubricant impellers are configured to impart centrifugal forces into the lubricant mist and air causing the lubricant to separate from the air.
9 . The de-oiler system for a gas turbine engine according to claim 7 , wherein the lubricant to fuel divider is configured to transfer thermal energy from the lubricant pumping section to the fuel turbine impelling section, such that the lubricant warms the fuel passing through the de-oiler.
10 . The de-oiler system for a gas turbine engine according to claim 7 , further comprising:
a perforated divider located in the lubricant pumping section, the perforated divider configured to separate the lubricant pumping section into a radially inner region and a radially outer region.
11 . The de-oiler system for a gas turbine engine according to claim 10 , further comprising:
perforations formed in the perforated divider, the perforations configured for fluid communication between the radially inner region and the radially outer region.
12 . A process for separating lubricant with a de-oiler system for a gas turbine engine comprising:
containing a lubricant within a lubrication system tank;
fluidly coupling the lubricant with at least one of the gas turbine engine, rotating hardware and bearings through a lubricant supply line;
operatively coupling a de-oiler with the lubrication system tank;
operatively coupling a lubricant pumping section of the de-oiler with a fuel turbine impelling section of the de-oiler;
separating the lubricant pumping section from the fuel turbine impelling section with a lubricant to fuel divider;
forming a helical sinus within the lubricant pumping section;
configuring the helical sinus to pump at least one of the lubricant, and a lubricant mist from a de-oiler tank inlet fluidly coupled with the lubrication system tank to a de-oiler tank outlet fluidly coupled with the lubrication system tank;
configuring the helical sinus to pump the air to a de-oiler air vent outlet in the absence of lubricant;
fluidly coupling the fuel turbine impelling section with a fuel inlet and a fuel outlet, the fuel turbine impelling section comprising impellers;
configuring the impellers to receive a fluid flow of fuel and translate a flow energy from the fluid flow into a mechanical rotational energy and impart the mechanical rotational energy into the de-oiler;
locating the fuel turbine impelling section radially outboard from the lubricant pumping section relative to the axis of the de-oiler; and
locating the fuel turbine impelling section between an exterior wall and the lubricant to fuel divider of the de-oiler.
13 . The process of claim 12 , wherein the helical sinus comprises lubricant impellers, and the process further comprises:
forming the lubricant impellers as contiguous helix shaped paddles that define a continuous flow passage with pockets serially aligned along an axis of the de-oiler;
configuring the lubricant impellers to impart mechanical rotary and axial motion to the lubricant mist and air to pump the lubricant mist and air through the de-oiler.
14 . The process of claim 13 , further comprising:
configuring the lubricant impellers to impart centrifugal forces into the lubricant mist and air causing the lubricant to separate from the air.
15 . The process of claim 12 , further comprising:
configuring the lubricant to fuel divider to transfer thermal energy from the lubricant pumping section to the fuel impelling section, such that the lubricant warms the fuel passing through the de-oiler.
16 . The process of claim 12 , further comprising:
forming a perforated divider within the lubricant pumping section;
configuring the perforated divider to separate the lubricant pumping section into a radially inner region and a radially outer region.
17 . The process of claim 16 , further comprising:
forming perforations in the perforated divider;
configuring the perforations for fluid communication between the radially inner region and the radially outer region.