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| Number | Title | Issue Date |
| 8152095 | Aircraft having a reduced acoustic signature An aircraft, the propulsive units of which include engines, and which is distinguished by reduced noise emissions, includes a wing structure fixed to an upper region of the fuselage, and a vertical tail system having at least two vertical stabilizers which are gener... | 04/10/2012 |
| 8151643 | Device for non-destructive testing of a structure by vibratory analysis A device for non-destructive testing of a structure likely to contain a defect, including microsensors for measuring vibratory waves emitted by the structure at different points of a surface of the structure, the aforementioned microsensors being integrated in a fle... | 04/10/2012 |
| 8148639 | Electrical cable provided with external marking and method of crimping the barrel of a contact onto an electrical cable provided with external marking An electrical cable (1) provided with a sheath (2) having external marking. The marking is formed from a block (3) of two patterns (4, 5), the two patterns being consecutive along a length of the cable, said block being repeated at least ... | 04/03/2012 |
| 8146863 | Aircraft doorway The invention concerns a doorway in an aircraft fuselage comprising a door frame in which a door is mounted, this frame comprising an outer framework, an inner framework and a core placed between the inner framework and the outer framework, capable of absorbing ener... | 04/03/2012 |
| 8135399 | Method for determining an identifier corresponding to a frequency set on a display unit of the cockpit and system of implementation A method for the determining, on board an aircraft, of an identifier of a communications center with which an aircraft crew wishes to enter into contact, includes the following operations: a) the writing, by the crew, of a radio-communications frequency to a display... | 03/13/2012 |
| 8132757 | Pitch-oscillation limitation system applied to an aircraft A pitch-oscillation limitation system, applied to an aircraft having main landing gear located toward the center of the aircraft and forward landing gear located under the nose of the aircraft, wherein the system includes means for automatically applying, in the eve... | 03/13/2012 |
| 8125351 | Process for transmitting data between at least one cockpit display screen and at least one remote client system A process for transmitting data between at least one display screen in a cockpit and at least one remote client system includes at least one computer, in which the display screen displays a first request to send a message in a first communication protocol; this mess... | 02/28/2012 |
| 8123166 | Primary structure for aircraft of composite material with improved crash resistance and associated energy-absorbing structural element The disclosed embodiments relate essentially to a primary structure of an aircraft fuselage that has at least a first strut linked at one end to a crossbeam and at the other end to a reinforcing frame. A second strut has one end fastened to the structure below the e... | 02/28/2012 |
| 8113464 | Autonomous plane architecture for the transport and the replacement of propulsion engines To be able to transport and replace in an autonomous manner one of its failing propulsion engines, a plane includes: a fuselage; propulsion engines maintained above the fuselage; maintenance wells traversing the fuselage substantially vertically with respect to the ... | 02/14/2012 |
| 8100362 | Cockpit and aircraft including such cockpit A cockpit and an aircraft including such cockpit. The cockpit includes a front section of an aircraft. Such cockpit includes a pressure bulkhead sealing the section and a pressurization system for pressurizing such section. ... | 01/24/2012 |
| 8100358 | Method of reducing the compressibility drag of a wing, and container implementing the method The present invention provides a method of reducing the compressibility drag of wing, and it also provides a container implementing the method. The container (10, 10′, 10″) is provided successively with a front portion (11) in the vicinity of its l... | 01/24/2012 |
| 8096190 | Process for conducting adherence tests for a coating on a substrate In order to conduct tests designed to determine the adherence properties of a coating on a substrate, a pull plate of a hardenable material is molded directly to the surface of a coating applied to a substrate. The pull plate geometry is determined by the mold cavit... | 01/17/2012 |
| 8095251 | System for monitoring anemobaroclinometric parameters for aircraft The disclosed embodiments concerns a system for monitoring anemobaroclinometric parameters in an aircraft, including a primary detection circuit having at least one measurement channel. The measurement channel includes a device for... | 01/10/2012 |
| 8091832 | Nacelle cowling for turbojet and nacelle comprising at least one such cowling A nacelle cowling for a turbojet, characterized in that it is provided with a fixed part and a mobile part, the mobile part being adapted to slide along the fixed part, from a closed position wherein the mobile part extends in the extension of the fixed part, up to ... | 01/10/2012 |
| 8091197 | Device and process for assembling oriented objects A device and a method for assembling oriented objects, such as parts of a pipeline. The device includes means for rotational displacement about a rotational axis of a first and second base. The first base has a first main axis which is perpendicular to the rotationa... | 01/10/2012 |
| 8083182 | Monolithic self-stiffened panels A composite panel having a first skin forming the outer wall of the panel, known as the lower face (1), and a second skin forming part of the inner wall of the panel. The second skin is formed hollow such as to produce an inner reinforcing frame (2) in... | 12/27/2011 |
| 8066221 | Aircraft ventral fairing partition wall and aircraft equipped with a ventral fairing The invention concerns a wall (10) of vertical partitioning for a ventral cowling of an aircraft including a plurality of vertical panels (11, 12, 12′, 13, 13′), each panel being linked to an adjacent panel by a vertical post (14, 15, 16). A... | 11/29/2011 |
| 8065899 | Advanced feed device for a superplastic press forming system A feed device for a superplastic press-forming press has a slide that moves vertically and a base between which is held a tool having a cover and a bottom die enclosing a forming tool, which includes at least one heating shuttle to transport the bottom die, equipped... | 11/29/2011 |
| 8028955 | Landing gear casing provided with a box structure A reduced-volume landing gear casing for the landing gear of an aircraft including a box structure to which the landing gear is fixed and which takes up the loads acting thereon. The box structure can include, in particular, means for receiving the fixing bearings o... | 10/04/2011 |
| 8019495 | Method and device for assisting the flying of an aircraft during an autonomous approach An aircraft guidance system defines a main approach path and a corrected approach path, which has an extra vertical margin related to the ground over which the craft is flying as compared with a main approach path representing a category-1 precision approach. The gu... | 09/13/2011 |
| 8019337 | Aircraft data transmission system for transmitting data between an aircraft and a transmission station located outside thereof The invention relates to an aircraft data transmission system for transmitting data between the aircraft and a transmission station located outside thereof. The inventive system includes a transmitting/receiving device for transmitting and receiving data messaged fr... | 09/13/2011 |
| 8014912 | Method and device for aiding the piloting of an airplane during an approach phase A method and device for aiding the piloting of an airplane includes: (1) determining current values of flight parameters of the airplane, (2) determining, with the aid of the current values, an approach distance that corresponds to a distance in a horizontal plane b... | 09/06/2011 |
| 8014910 | Assisted take-off method for aircraft A reference value is arbitrarily selected from a range of possible aircraft rotation speeds. A position of a trimmable horizontal stabilizer is angled in accordance with a centering of the reference value. A deviation between the reference value and an accelerating ... | 09/06/2011 |
| 8011613 | Aircraft with reduced environmental impact An aircraft includes a fuselage and at least one engine provided with at least one propeller and mounted at a rear part of the fuselage, on the back thereof, with the at least one engine having an axis substantially parallel to the longitudinal axis of the fuselage,... | 09/06/2011 |
| 8010288 | Aircraft terrain avoidance and alarm method and device An aircraft terrain avoidance system include a device having a first unit knowing a profile of the terrain that is located at the front of the aircraft, a second unit for determining an avoidance trajectory, a third unit which is connected to the first and second un... | 08/30/2011 |
| 8006931 | Aircraft wing arrangement comprising an engine attachment pylon defining, in the forward region, a lateral airflow channel An aircraft wing arrangement including a wing and at least one strut for attaching the aircraft engine suspended under the wing and including a front zone situated projecting towards the front with respect to a leading edge of the wing. The front zone includes a lat... | 08/30/2011 |
| 8006803 | Ladder system, especially for vehicles The invention relates to a ladder comprising a single post (1) provided with a fixing means (4) on the upper end (1S) thereof, said ladder comprising an anchoring means (9, 10) which is especially adapted to said fixing means (4) a... | 08/30/2011 |
| 8005614 | Method for monitoring the integrity of an aircraft position computed on board A method for monitoring the integrity of an aircraft position computed on board including on-board means for monitoring the aircraft position that are able to detect common-mode failures. Dissimilar computing channels of the aircraft position are utilized, the dissi... | 08/23/2011 |
| 8005583 | Method and device for determining the air turbulence likely to be encountered by an aircraft A method and device for determining the air turbulence likely to be encountered by a first aircraft may use a turbulence indication from a second aircraft so as to make and use a prediction of the impact of the turbulence on the first aircraft if it is located in a ... | 08/23/2011 |
| 8004815 | Lightning protection system and an aircraft having such a system A lightning protection system for a composite structure has an outer surface designed to be subject to an air flow. This system has an electrically conductive strip and fasteners from the strip to the structure. Since the structure has holes designed for the ... | 08/23/2011 |
| 8000845 | Method and device for dynamically alleviating loads generated on an airplane A device detects an air disturbance and controls the deflection of aircraft control surfaces when the disturbance is detected. ... | 08/16/2011 |
| 8000844 | Flight control system for aircraft and test for testing such a flight control system A test system for testing a flight control system of an aircraft includes a test device that: (1) accesses information available from the flight control system and (2) controls a computer of the flight control system. ... | 08/16/2011 |
| 7997061 | Turbojet engine for aircraft, propulsion unit comprising such a turbojet engine and aircraft comprising such a propulsion unit A propulsion unit comprises a turbojet engine and a thermal exchanger, situated above the turbojet engine. The turbojet engine comprises a regulation device to regulate an air flow-rate in a cooling air lead-in conduit conveying a stream of cooling air into a therma... | 08/16/2011 |
| 7996121 | Device and method for assisting in the management of an engine failure on an aircraft A device and method for assisting in the management of an engine failure on an aircraft: (1) determine, when an engine failure occurs, flight profiles allowing the closest airports to be reached according to flight strategies and (2) present, on a screen, the airpor... | 08/09/2011 |
| 7996120 | Method and device for flying an aircraft according to at least one flying line The device for flying an aircraft includes a first unit for determining a control value corresponding to an instruction value representing the actuation of a control member by a pilot, a second unit for determining an effective control value corresponding to the ins... | 08/09/2011 |
| 7996118 | Method and device for carrying out at least one flight testing on an aircraft and the use thereof An aircraft device includes a rudder, a control unit that applies a deflection instruction to the rudder, a measuring section that measures a recovery characteristic of aircraft movement in response to the rudder deflection instruction, a recorder that records an ap... | 08/09/2011 |
| 7990285 | Method and device for audible warning when an aircraft autopilot is deactivated The invention relates to a method for producing an audible warning when an aircraft autopilot is deactivated. The method includes a) transmitting a first sound in the aircraft cockpit during a time ranging from a first predetermined value and a second predetermined ... | 08/02/2011 |
| 7987709 | Device and method for measuring the flow speed and direction of a gaseous fluid A device for measuring the flow speed of a fluid as well as its direction and its orientation, based on a thermal-sensor measurement principle, that comprises at least three flow measurement probes each having a sensitive member and an obstacle masking a predetermin... | 08/02/2011 |
| 7980610 | Device for slinging a piece with stress compensation and hoisting system containing this device A slinging device for a piece includes a sling with a nonextensible part and a section with a spring device, enabling an elastic lengthening or shortening of the sling under load by a limited amplitude in response to a limited change in the load on the piece, the de... | 07/19/2011 |
| 7974812 | Method for determining the total temperature of an airflow surrounding an aircraft A method for determining the total temperature of the air stream surrounding an aircraft, including the following operations; measuring a parameter of static temperature, measuring a parameter of total temperature, determining a value of speed of the air stream, det... | 07/05/2011 |
