Standard Search
About 45 results
https://drivepatents.com/patents/1073555 · 5 Oct 2005
The structure has an annular part which defines a fan case ducting that includes inner and outer casings (16, 17). A rigidifying bar (20) has ends (24, 22) integrated to the respective casings and to front and rear stiffening frames (18, 19) respectively. ...
https://drivepatents.com/patents/1073556 · 5 Oct 2005
The frame (20) has an intermediate portion (28) that acts as an inflection zone as curvature between the portion and an inner end portion (20i) is not null. Height (H) of the frame is defined between an outer end portion (20e) and a normal projection of th...
https://drivepatents.com/patents/1073542 · 5 Oct 2005
The process involves utilizing a line that realizes a connection between a source and load and includes several remote cables connected by a cut-off connector. Segments of each cable are dimensioned independent of the other cables. The line and the cables ...
https://drivepatents.com/patents/1073714 · 28 Sep 2005
The pipe has an internal skin (2) inside which circulates a primary air flow (FP) and which comprises chevrons (4), at an external end. An external skin (3) partially surrounds the internal skin and along which flows a secondary air flow (FS). The external...
https://drivepatents.com/patents/1074969 · 17 Aug 2005
The method involves determining an effective distance between a current position of an aircraft and a particular flying point. Aircraft deceleration and acceleration times are determined from respective convergence curves. The curves are different and form...
https://drivepatents.com/patents/1075195 · 10 Aug 2005
The process involves determining static temperature at the level of an aircraft, using dynamic temperature outside the aircraft. A temperature value related to temperature at destination altitude is measured using the static temperature. A difference betwe...
https://drivepatents.com/patents/1077375 · 1 Jun 2005
The device has a coupling unit (10) with a front trunnion (14) having triangular shackles placed in a vertical plane oriented along a direction inclined with respect to longitudinal and transversal directions of an aircraft. The shackles are situated in a ...
https://drivepatents.com/patents/1079488 · 9 Mar 2005
The aircraft has engines (5-8) whose speed is controlled by throttles (11-14). The inner engines (5, 6) have thrust reversers (9, 10) passing from inactive folded position to an active deployed position, and vice versa. A detector (33) detects the deployme...
https://drivepatents.com/patents/1080109 · 9 Feb 2005
The method involves controlling fueling of jet engines to one set value that is common to the engines and depends on an automatic power order and conditions of flying of the aircraft. The set value is converted into another set value related to speed of ro...
https://drivepatents.com/patents/1080855 · 12 Jan 2005
The system has a braking control unit controlled by a braking unit (3) based on deceleration command calculated by a calculation unit (5). The unit (5) determines pairs of distance and speed of an aircraft on a runway that has multiple exits. An interface ...