Apparatus to prevent air leakage in turbine engines
Apparatus are disclosed for a turbofan comprising: a bifurcation including a first track; and an outer casing including an airflow inlet and an airflow outlet, the outer casing adjustable into a closed position and an open position, the outer casing positioned around the bifurcation, the outer casing including a first slider for movement between the closed position and the open position that mates with the first track, the first track including a brush seal holder and a brush seal including a plurality of bristles having a compressed state in the closed position and a decompressed state in the open position.
1 . A turbofan comprising:
a bifurcation including a first track;
an outer casing including an airflow inlet and an airflow outlet, the outer casing adjustable into a closed position and an open position, the outer casing positioned around the bifurcation, the outer casing including a first slider for movement between the closed position and the open position that mates with a first track, the first track including a brush seal holder and a brush seal including a plurality of bristles having a compressed state in the closed position and a decompressed state in the open position; and
a forward core cowl including a hinge, wherein the brush seal is within at least one of the first track or the hinge.
2 . The turbofan of claim 1 , wherein the brush seal is positioned radially outward of the first track.
3 . The turbofan of claim 1 , wherein the brush seal is located between the first track and the first slider.
4 . The turbofan of claim 1 , wherein the brush seal is at an end of the first track.
5 . The turbofan of claim 1 , wherein the brush seal includes at least one of nickel alloy, cobalt alloy, stainless steel, rubber, plastic, silicone, or fiber.
6 . The turbofan of claim 1 , wherein the plurality of bristles has a length range from 0.1 inch to 1 inch.
7 . The turbofan of claim 1 , wherein the plurality of bristles has a density range from 10 to 1000 bristles per a square inch of a strip surface area.
8 . The turbofan of claim 1 , wherein a core cowl is movable via a second slider along a second track of the bifurcation and includes at least one brush seal.
9 . The turbofan of claim 1 , further including at least one of a bulb seal, a P-seal, a labyrinth seal, or a compression seal.
10 . An outer duct of a turbine engine, the outer duct comprising:
a forward core cowl including a hinge;
a first outer duct section including an airflow inlet;
a second outer duct section including an airflow outlet, having a closed position and an open position, the outer duct longitudinally movable from the closed position to the open position, the second outer duct section including:
a slider that is received by a track to facilitate movement of the second outer duct section from the closed position to the open position; and
a brush seal holder and a brush seal including a plurality of bristles having a compressed state in the closed position and a decompressed state in the open position,
wherein the brush seal is within at least one of the track or the hinge.
11 . The outer duct of claim 10 , wherein the brush seal is positioned radially outward of the track.
12 . The outer duct of claim 10 , wherein the brush seal is in between the track and the slider.
13 . The outer duct of claim 10 , wherein the brush seal is at an end of the track.
14 . The outer duct of claim 10 , further including a bifurcation including the track.
15 . The outer duct of claim 10 , wherein the brush seal includes at least one of nickel alloy, cobalt alloy, stainless steel, rubber, plastic, silicone, or fiber.
16 . The outer duct of claim 11 , further including at least one of a bulb seal, a P-seal, a labyrinth seal, or a compression seal.
17 . A turbofan comprising:
a core cowl; and
a nacelle having an airflow inlet and an airflow outlet, the nacelle including:
a forward core cowl including a hinge;
a first nacelle section including a first perimeter and a first track;
a second nacelle section, including a second perimeter, having a closed position and an open position, the second nacelle section longitudinally movable from the closed position to the open position along the first track; and
a brush seal runner extending along at least a portion of the first perimeter and at least a portion of the second perimeter, the brush seal runner including a first brush seal including a plurality of bristles having a compressed state in the closed position and a decompressed state in the open position,
wherein the first brush seal is within at least one of the first track or the hinge.
18 . The turbofan of claim 17 , wherein the core cowl further includes a second brush seal with a plurality of bristles.
19 . The turbofan of claim 17 , wherein the first brush seal includes at least one of nickel alloy, cobalt alloy, stainless steel, rubber, plastic, silicone, or fiber.
20 . A turbofan comprising:
a bifurcation including a first track and a second track; and
an outer casing including an airflow inlet and an airflow outlet, the outer casing adjustable into a closed position and an open position, the outer casing positioned around the bifurcation, the outer casing including a first slider for movement between the closed position and the open position that mates with a first track, the first track including a brush seal holder and a first brush seal including a plurality of bristles having a compressed state in the closed position and a decompressed state in the open position;
wherein a core cowl is movable via a second slider along the second track of the bifurcation and includes a second brush seal.