About 90 results
https://drivepatents.com/patents/1002810 · 2 May 2012
The aircraft nacelle (10) has limiting element (19) with at least one lock that is integral with the rest of nacelle or respectively the cowl (14). One part of lock occupies locked state in which lock interferes with the cowl and prevents deformation that ...
https://drivepatents.com/patents/1003253 · 18 Apr 2012
The nacelle has a lip (114) extended inside and outside the nacelle by inner and outer walls (116, 118), respectively. A front frame (122) connects the inner wall and the outer wall that delimits an annular pipe (124). A rear frame (126) connects the walls...
https://drivepatents.com/patents/1003899 · 28 Mar 2012
The device (20) has a rotating door (24) comprising inner and outer flaps (26, 28) secured and articulated around a pivot axle (58) that is remote from the inner flap in a direction from the outer flap to the inner flap when the door is in closing position...
https://drivepatents.com/patents/1005835 · 25 Jan 2012
The nacelle has a variable section nozzle cowl (1) including a movable cowl part (3) with a thrust reverser arranged so that translational movement of the part allows the passage of the part from a stow position (5) of the reverser to a thrust reversal pos...
https://drivepatents.com/patents/1007337 · 7 Dec 2011
The aircraft has a heat exchanger exchanging heat between first fluid e.g. fuel, and second fluid e.g. oil. A preheating device preheats the first fluid in upstream from narrow pipes (22) of the exchanger. The preheating device comprises a number of condui...
https://drivepatents.com/patents/1008749 · 12 Oct 2011
The device has a switch (205) to simulate a defect of an electrical supply (105) of primary and secondary supplies. A detection unit i.e. engine interface function (210), detects connection of an igniter on a hand to the switch, which is connected on anoth...
https://drivepatents.com/patents/1009835 · 24 Aug 2011
The system (1) has interface units (9) providing a determined strategy defined by specific values taken by flight parameters to a reference point. The interface units select and set a value of a parameter from the flight parameters for generating and provi...
https://drivepatents.com/patents/1010746 · 27 Jul 2011
The propulsion unit has an air vein (13) guiding pressurized air towards an air pipe (20) arranged between an outer wall (6) and an inner wall (60) of a nacelle (10). A cooler (14) has two surface cooling units (145, 146) i.e. fins, on its corresponding ou...
https://drivepatents.com/patents/1010742 · 27 Jul 2011
The propulsion unit has an air vein (13) guiding pressurized air towards an air pipe (20) arranged between an outer wall (6) and an inner wall (60) of a nacelle (10). A cooler (45) has a parallelepiped volumetric cooling unit (14) i.e. blade, positioned in...
https://drivepatents.com/patents/1014889 · 16 Mar 2011
The method involves acquiring information of equipments, and determining a context that corresponds to an instantiation of a predetermined hierarchical context model. Information are filtered based on a regulation for selecting one of the information, wher...