Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
ADAPTIVE TRANS-CRITICAL CO2 COOLING SYSTEMS FOR AEROSPACE APPLICATIONS
Document Type and Number:
WIPO Patent Application WO/2014/158280
Kind Code:
A3
Abstract:
A cooling system for an aircraft includes a first cooling circuit (702) having a first evaporator (706) and a second evaporator (708), and a second cooling circuit (704) having a third evaporator (712) and a fourth evaporator (714). One of the first and second cooling circuits (702,704) includes a first set of valves arranged to direct refrigerant through a first cooling sub-circuit, a second cooling sub-circuit, or both the first and second cooling sub-circuits based on ambient conditions. Two of the evaporators are installed on a first side of the aircraft, and the other two of the four evaporators are installed on a second side of the aircraft opposite the first side, and the first and second cooling circuits reject heat, via a heat exchanger, from their respective cooling circuit to air passing into an engine of the aircraft.

Inventors:
VAISMAN IGOR (US)
SNYDER DOUGLAS J (US)
SWEENEY PATRICK C (US)
Application Number:
PCT/US2013/078155
Publication Date:
December 04, 2014
Filing Date:
December 28, 2013
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
ROLLS ROYCE CORP (US)
ROLLS ROYCE NAM TECH INC (US)
International Classes:
B64D13/06; F25B9/06
Foreign References:
US2963879A1960-12-13
US20070068178A12007-03-29
EP1762491A22007-03-14
JP2008224118A2008-09-25
US20060162371A12006-07-27
US20130233003A12013-09-12
Attorney, Agent or Firm:
LALONE, Douglas, P. (Fishman & Grauer PLLC39533 Woodward Avenue,Suite 14, Bloomfield Hills MI, US)
Download PDF: