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Patent Agency Ranking
公开(公告)号：US11927349B2
公开(公告)日：2024-03-12
申请号：US17812897
申请日：2022-07-15
Applicant: General Electric Company
Inventor： Vijayaraj Sukumar , Perumallu Vukanti , Pradeep Naik , Ajoy Patra , Karthikeyan Sampath , Rimple Rangrej , Hiranya Nath , Krishnendu Chakraborty , Narasimhan S. Sahana , Saket Singh , Ravindra Shankar Ganiger
CPC classification number: F23R3/002 , F23R3/60 , F23R3/04 , F23R3/10 , F23R2900/00017 , F23R2900/03045
Abstract: A deflector assembly for a combustor defining an operational fluid flow. The deflector assembly includes an upstream surface and a downstream surface opposite the upstream surface. One or more fastening mechanisms each extends through the deflector assembly. One or more cooling holes extend through the deflector assembly from the upstream surface to the downstream surface. The one or more cooling holes are located about the one or more fastening mechanisms to operably direct cooling air about the one or more fastening mechanisms at the downstream surface.
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公开(公告)号：US20230313992A1
公开(公告)日：2023-10-05
申请号：US17811771
申请日：2022-07-11
Applicant: General Electric Company
Inventor： Ranganatha Narasimha Chiranthan , Hiranya Nath , Girish Kamath Cannanore , Ravindra Shankar Ganiger , Pradeep Naik , Saket Singh , Deepti Bhandari , Vijayaraj Sukumar
CPC classification number: F23R3/002 , F23R3/60 , F23R2900/03043 , F23R2900/00014 , F23R2900/00017
Abstract: A liner assembly for a combustor. The liner assembly includes a liner defining a combustion chamber of the combustor. The liner includes a looped section at a forward end of the liner. The looped section includes one or more bends such that the looped section forms a compliant joint and vibrations are dampened through the liner downstream of the looped section.
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公开(公告)号：US12234987B2
公开(公告)日：2025-02-25
申请号：US17811771
申请日：2022-07-11
Applicant: General Electric Company
Inventor： Ranganatha Narasimha Chiranthan , Hiranya Nath , Girish Kamath Cannanore , Ravindra Shankar Ganiger , Pradeep Naik , Saket Singh , Deepti Bhandari , Vijayaraj Sukumar
Abstract: A liner assembly for a combustor. The liner assembly includes a liner defining a combustion chamber of the combustor. The liner includes a looped section at a forward end of the liner. The looped section includes one or more bends such that the looped section forms a compliant joint and vibrations are dampened through the liner downstream of the looped section.
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公开(公告)号：US20240247802A1
公开(公告)日：2024-07-25
申请号：US18598467
申请日：2024-03-07
Applicant: General Electric Company
Inventor： Vijayaraj Sukumar , Perumallu Vukanti , Pradeep Naik , Ajoy Patra , Karthikeyan Sampath , Rimple Rangrej , Hiranya Nath , Krishnendu Chakraborty , Narasimhan S. Sahana , Saket Singh , Ravindra Shankar Ganiger
CPC classification number: F23R3/002 , F23R3/60 , F23R3/04 , F23R3/10 , F23R2900/00017 , F23R2900/03045
Abstract: A deflector assembly for a combustor defining an operational fluid flow. The deflector assembly includes an upstream surface and a downstream surface opposite the upstream surface. One or more fastening mechanisms each extends through the deflector assembly. One or more cooling holes extend through the deflector assembly from the upstream surface to the downstream surface. The one or more cooling holes are located about the one or more fastening mechanisms to operably direct cooling air about the one or more fastening mechanisms at the downstream surface.
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公开(公告)号：US20230324047A1
公开(公告)日：2023-10-12
申请号：US17812897
申请日：2022-07-15
Applicant: General Electric Company
Inventor： Vijayaraj Sukumar , Perumallu Vukanti , Pradeep Naik , Ajoy Patra , Karthikeyan Sampath , Rimple Rangrej , Hiranya Nath , Krishnendu Chakraborty , Narasimhan S. Sahana , Saket Singh , Ravindra Shankar Ganiger
CPC classification number: F23R3/002 , F23R2900/03045 , F23R2900/00017 , F23R3/60
Abstract: A deflector assembly for a combustor defining an operational fluid flow. The deflector assembly includes an upstream surface and a downstream surface opposite the upstream surface. One or more fastening mechanisms each extends through the deflector assembly. One or more cooling holes extend through the deflector assembly from the upstream surface to the downstream surface. The one or more cooling holes are located about the one or more fastening mechanisms to operably direct cooling air about the one or more fastening mechanisms at the downstream surface.
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