LIP SKIN FOR AN AIRCRAFT AEROSTRUCTUREAn air inlet section (40) for an aircraft propulsion system nacelle (24) includes an outer skin (48), an inner skin (50), and a lip skin (54). The lip skin (54) extends between and to an outer end (70…DRIVE·Feb 25·2 min readFollowB64D15/00ROHR INC [US]
ICE PROTECTION SYSTEM FOR A COMPONENT OF AN AERODYNAMIC SYSTEMDisclosed is an ice protection system (140) for an aerodynamic surface of an aircraft, a surface having a flow facing side and an inwardly facing side that opposes the flow facing side, the system hav…DRIVE·Mar 27·1 min readFollowB64D15/00GOODRICH CORP [US]
METHOD AND SYSTEM TO PROMOTE ICE SHEDDING FROM ROTOR BLADES OF AN AIRCRAFT ENGINEA method of operating an aircraft engine (10) having a bladed rotor (12) coupled thereto during an icing condition is provided. The method comprises controlling the aircraft engine (10) to alternating…DRIVE·May 3·1 min readFollowB64D15/00PRATT & WHITNEY CANADA [CA]
THERMAL ANTI-ICING SYSTEM WITH MICROWAVE SYSTEMAn assembly (52) is provided for an aircraft propulsion system (20). This aircraft propulsion system assembly (52) includes an aircraft propulsion system structure (22) and a microwave system (94). Th…DRIVE·Apr 12·1 min readFollowB64D15/00ROHR INC [US]
Heat transfer arrangement for fluid-washed surfacesThe invention concerns a heat transfer arrangement for a fluid-washed body (25;123;124) having first (26;128) and second (32;132) ends and a fluid-washed surface extending there-between. The arrangeme…DRIVE·Dec 7·1 min readFollowB64D15/00ROLLS ROYCE PLC [GB]
