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公开(公告)号：US20210277829A1
公开(公告)日：2021-09-09
申请号：US16863218
申请日：2020-04-30
发明人： Daniel K. Van Ness , Anthony R. Bifulco , David A. Topol , David A. Knaul , Michael Raymond LaFavor
摘要： Disclosed is an acoustic liner for a gas turbine engine, having: a face sheet; a first plurality of resonator chamber cavities, distributed non-uniformly against the face sheet, the first plurality of resonator chamber cavities defining a first aggregated volume that is configured to target noise attenuation at a first frequency, the first plurality of resonator chamber cavities include first and second resonator chamber cavities fluidly coupled to each other, which have different configurations with respect to each other; and a second plurality of resonator chamber cavities, distributed non-uniformly against the face sheet, the second plurality of resonator chamber cavities define a second aggregated volume that differs from the first aggregated volume and is configured to target noise attenuation at a second frequency, the second plurality of resonator chamber cavities include third and fourth resonator chamber cavities fluidly coupled to each other, which have different configurations with respect to each other.
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公开(公告)号：US11339720B2
公开(公告)日：2022-05-24
申请号：US16863218
申请日：2020-04-30
发明人： Daniel K. Van Ness , Anthony R. Bifulco , David A. Topol , David A. Knaul , Michael Raymond LaFavor
摘要： Disclosed is an acoustic liner for a gas turbine engine, having: a face sheet; a first plurality of resonator chamber cavities, distributed non-uniformly against the face sheet, the first plurality of resonator chamber cavities defining a first aggregated volume that is configured to target noise attenuation at a first frequency, the first plurality of resonator chamber cavities include first and second resonator chamber cavities fluidly coupled to each other, which have different configurations with respect to each other; and a second plurality of resonator chamber cavities, distributed non-uniformly against the face sheet, the second plurality of resonator chamber cavities define a second aggregated volume that differs from the first aggregated volume and is configured to target noise attenuation at a second frequency, the second plurality of resonator chamber cavities include third and fourth resonator chamber cavities fluidly coupled to each other, which have different configurations with respect to each other.
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公开(公告)号：US20210324748A1
公开(公告)日：2021-10-21
申请号：US16851696
申请日：2020-04-17
IPC分类号： F01D5/30
摘要： A component of a rotor system is provided and includes a disk and a reinforcing ring. The disk includes an airfoil element, a web extending radially inwardly from the airfoil element and an arm element extending axially from the web. The reinforcing ring is formed of fiber reinforced materials and is disposed to fit about the arm element.
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公开(公告)号：US20240125237A1
公开(公告)日：2024-04-18
申请号：US17967361
申请日：2022-10-17
发明人： David A. Knaul
CPC分类号： F01D5/147 , F01D5/34 , F05D2230/23 , F05D2240/303
摘要： An integrally bladed rotor for a gas turbine engine, including: a plurality of blades integrally formed with a hub as a single component, each of the plurality of blades having a blade body extending from the hub to an opposing blade tip surface along a longitudinal axis, each blade body having a pressure side and a suction side each extending between a leading edge and a trailing edge of the blade body; and each of the plurality of blades including a leading edge shield secured to the leading edge of the blade body.
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公开(公告)号：US11268388B2
公开(公告)日：2022-03-08
申请号：US16851696
申请日：2020-04-17
摘要： A component of a rotor system is provided and includes a disk and a reinforcing ring. The disk includes an airfoil element, a web extending radially inwardly from the airfoil element and an arm element extending axially from the web. The reinforcing ring is formed of fiber reinforced materials and is disposed to fit about the arm element.
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