专利检索 ap:("Rohr, Inc.") AND inv:"PramodaKumar Nayak" 第 1 页

1.

发明公开
THERMAL ANTI-ICING SYSTEM FOR AN AIRCRAFT PROPULSION SYSTEM 审中-公开

公开(公告)号：US20240077018A1

公开(公告)日：2024-03-07

申请号：US18241693

申请日：2023-09-01

申请人： Rohr, Inc.

发明人： PramodaKumar Nayak , Ashok Babu Saya

IPC分类号： F02C7/047 , B64D33/02

CPC分类号： F02C7/047 , B64D33/02 , B64D2033/0233

摘要： An assembly is provided for an aircraft propulsion system. This assembly includes a nacelle inlet structure and a nozzle. The nacelle inlet structure extends circumferentially about an axial centerline. The nacelle inlet structure includes an inlet lip, a bulkhead and an internal cavity formed by and axially between the inlet lip and the bulkhead. The nozzle is configured to direct gas into the internal cavity axially towards the bulkhead.