公开(公告)号：SG182020A1

公开(公告)日：2012-07-30

申请号：SG2010094282

申请日：2010-12-20

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： CHAN KEEN IAN ,  KEK HIAN BENG ,  LIU YONG WEE

Abstract: A rotor duct for an aircraft, a method for controlling an airflow into a rotor duct, and a kit of parts for controlling an airflow into a rotor duct. The rotor ductcomprises a substantially cylindrical duct wall for circumferentially enclosing the rotor; and an airfoil structure disposed at a leading edge of the duct wall such that a pressure surface of the airfoil structure extends radially outwardly from the duct wall.FIG. 3

公开(公告)号：SG182019A1

公开(公告)日：2012-07-30

申请号：SG2010094027

申请日：2010-12-17

Applicant: SINGAPORE TECHNOLOGIES AEROSPACE LTD

Inventor： CHUA BENG CHOON ,  KEK HIAN BENG ,  LIU YONG WEE

Abstract: System and method for measuring static pressure of an aircraft are disclosed. Thesystem comprises: a plurality of static ports mounted on the fuselage of the aircraft, wherein outputs of each of the static ports are connected to a pressure stabilizer, and the pressure stabilizer is operable to provide average pressure from the plurality of the static ports to a static pressure sensor located on a flight control computer(FCC) board of the aircraft.Figure 7b