AIR GUIDING FLAP OF AN AIRCRAFT COMPRISING CONTROL OF THE PRESSURE FORCES IMPINGING THEREON, PROCESS FOR ADJUSTING THE POSITION OF AN AIR GUIDING FLAP AND RAM AIR SYSTEM INCLUDING SUCH AN AIR GUIDING FLAP

WIPO Patent Application WO2005063564

A3

The invention relates to an air guiding flap of an aircraft wherein one surface (28) thereof faces an air duct and is exposed to a prevailing pressure in the air duct and whose opposite surface (30) is exposed to the pressure of the relative wind flowing past the aircraft. The air guiding flap comprises an actuator (34) for automatically opening and closing the air guiding flap which actuator (34) cooperates with a device for controlling the position of the air guiding flap. In order to keep the stress on the air guiding flap low a force detecting device (36) is provided which detects the force impinging on the actuator (34) based on a difference between the prevailing pressure in the air duct and the pressure of the relative wind flowing past the aircraft. The controlling device adjusts the position of the air guiding flap such that the force impinging on the actuator (34) at any one time is at least essentially zero.

WO/2012/098322	NACELLE FOR AN AIRCRAFT BYPASS TURBOJET ENGINE
WO/2014/200590	INTERCHANGEABLE INLET PROTECTION SYSTEMS FOR AIR INTAKES OF AIRCRAFT ENGINES AND RELATED METHODS

SCHMIDT RUEDIGER (DE)
SOLNTSEV ALEXANDER (DE)

PCT/EP2004/014856

September 22, 2005

December 30, 2004

Click for automatic bibliography generation  

AIRBUS GMBH (DE)
SCHMIDT RUEDIGER (DE)
SOLNTSEV ALEXANDER (DE)

B64D33/02; B64D33/04; F02C6/08; F02C7/042; F02C7/057; (IPC1-7): B64D33/02; B64D33/04; F02C7/042; F02C7/057

US6272838B1	2001-08-14
FR886438A	1943-10-14
FR942092A	1949-01-28

View/Download PDF      PDF Help

Previous Patent: SHOCK ABSORBER FOR ADJUSTABLE PITCH PROPELLER WITH FEATHERING BLADES, PARTICULARLY FOR SAILERS

Next Patent: COOLING SYSTEM AND METHOD FOR EXPELLING HEAT FROM A HEAT SOURCE LOCATED IN THE INTERIOR OF AN AIRCRA...