Invention Grant
- Patent Title: Chilled working fluid generation and separation for an aircraft
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Application No.: US17691578Application Date: 2022-03-10
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Publication No.: US12291338B2Publication Date: 2025-05-06
- Inventor: Michael Winter
- Applicant: RTX Corporation
- Applicant Address: US CT Farmington
- Assignee: RTX Corporation
- Current Assignee: RTX Corporation
- Current Assignee Address: US CT Farmington
- Agency: CANTOR COLBURN LLP
- Main IPC: B64D13/08
- IPC: B64D13/08 ; B01D45/08 ; B01D53/00 ; B03C1/28 ; B64D13/06 ; B64D27/12 ; B64D33/08 ; B64D37/32 ; F01D15/00 ; F01D25/12 ; F02C6/08 ; F02C7/141 ; F02C7/143 ; F02C7/16 ; F02C7/18 ; F02C9/18 ; F02K3/06 ; F17C7/02 ; F17C7/04 ; F25B9/14 ; F25J3/04
Abstract:
A system for an aircraft includes an engine bleed source of a gas turbine engine. The system also includes a means for chilling an engine bleed air flow from the engine bleed source to produce a chilled working fluid. The system further includes a means for providing the chilled working fluid for an aircraft use.
Public/Granted literature
- US20220194604A1 CHILLED WORKING FLUID GENERATION AND SEPARATION FOR AN AIRCRAFT Public/Granted day:2022-06-23
Information query
