Abstract: A new and distinct variety of white nectarine tree denominated ‘NECTARCIEL’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh and slightly greenish at maturity time, and a red pigmentation into and around the stone cavity, and an attractive skin with a high percentage of luminous purple red blush on skin surface, on a red background.

Abstract: A new and distinct variety of white nectarine tree denominated ‘NECTARDALI’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh at maturity time, and a red pigmentation into and around the stone cavity, and an attractive skin with a luminous purple red blush on skin surface, on a red background.

Abstract: A new and distinct variety of white peach tree denominated ‘SWEETJAZZY’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh at maturity time, having a slightly pink pigmentation around the stone cavity, and an attractive skin with a luminous purple red blush on skin surface, on a purple red background.

Abstract: A new and distinct variety of white peach tree denominated ‘SWEETABBY’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet cream white flesh at maturity time, and an attractive skin with a luminous dark purple red blush on skin surface, on a purple red background.

Abstract: A method and device for adjusting performance variables of an aircraft. The device which is intended for adjusting performance variables, the performance variables being generated by at least one performance module, includes an auxiliary data input unit for entering into a flight management system correction data intended to be used for adjusting at least one associated performance variable, and a correction unit for carrying out a correction, the correction including adjusting the associated performance variable on the basis of the input correction data.

Abstract: A method and device for adjusting performance variables of an aircraft. The device which is intended for adjusting performance variables, the performance variables being generated by at least one performance module, includes an auxiliary data input unit for entering into a flight management system correction data intended to be used for adjusting at least one associated performance variable, and a correction unit for carrying out a correction, the correction including adjusting the associated performance variable on the basis of the input correction data.

Abstract: The vertical profile management device includes a flight management system unit that selects a plurality of successive standard cruise sections, each comprising a level phase and a transition phase. The cruise sections are defined by a plurality of features, including waypoints corresponding to a section starting point and a section ending point, a transition type, a transition mode, a transition speed, a level altitude, and a level speed. The flight management system unit also joins together the successive cruise sections in order to form a vertical profile of a flight plan. The cruise sections are configured to be added, removed, or re-sequenced in the flight plan because each section ending point is configured to be the section starting point of a next cruise section in the series.

Abstract: The device includes means for determining a plurality of successive standard flight sections (S1A, S2A, S3A, S4A) comprising a level and a transition phase for reaching this level, and means for joining together these successive flight sections (S1A, S2A, S3A, S4A) in order to form the vertical profile (PV1) of the flight plan.

Abstract: Disclosed is a method and device for guiding an aircraft flying along a flight trajectory. The flight trajectory has at least one constrained section, and the aircraft flies at a required speed within the constrained section to comply with a required arrival time at a predetermined waypoint in the constrained section. Auxiliary speed setpoints are determined to guide the aircraft to arrive at an auxiliary arrival tune at an auxiliary waypoint, with the auxiliary speed setpoints being applied by a guidance system to guide the aircraft.

Abstract: 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 units and used to verify if there is a terrain collision risk for the aircraft, a fourth unit for emitting an alarm signal in the event of detection of a collision risk by the third unit, at least one aircraft performance database relating to an avoidance maneuvering gradient which can be flown by the aircraft according to particular flight parameters, and a fifth unit for determining the effective values of the particular parameters during the flight of the aircraft. The third unit is formed such that it is possible to determine the avoidance trajectory according to information received from the database and the fifth unit.

Abstract: A system determines a limit angle of climb corresponding to a climb angle of an aircraft for flying over the ground along an avoidance path and displays a characteristic sign representing the limit angle of climb on a display screen.

Abstract: A device for constructing and securing a low altitude flight path intended to be followed by an aircraft. The device includes a first processing unit which has a Design Assurance Level (DAL) C requirement level and which determines a low altitude flight path, using data coming from a first database qualified according to a Data Process Assurance Level (DPAL) 2 standard, and a second processing unit which has a DAL A requirement level and which checks the flight path determined by said first processing unit, using data corning from a second database qualified according to a DPAL1 standard.

Abstract: Method and device for ensuring the safety of a low-altitude flight of an aircraft. A device (1) for ensuring the safety of a low-altitude flight comprises information sources (5) able to determine current flight conditions, a monitoring unit (6) for realizing, with the aid of said current flight conditions, a function for global and autonomous monitoring of said low-altitude flight of the aircraft, making it possible to preserve the integrity of said aircraft during said flight, and means (13) for presenting the results of the monitoring function realized by said monitoring unit (6) to an operator.

Abstract: A flight control indicator for an aircraft has a set of information sources, a computation unit which determines, on the basis of information emanating from the set of information sources, an item of information regarding actual thrust of an engine of the aircraft, and a display device which is a head-up display device and which presents, on a display screen, an indication of the item of information regarding actual thrust. The item of information regarding actual thrust is associated with a thrust scale and both are presented superimposed on the environment prevailing in front of the aircraft.

Abstract: The device (1) comprises means (9, 11) for transposing a time constraint to entry to a constrained section of a flight trajectory having to be followed by the aircraft.

Abstract: The device (1) comprises a first means (2) knowing the profile of the terrain at least that which is located at the front of the aircraft, a second means (3) for determining an avoidance trajectory, a third means (4) which is connected to the first and second means (2, 3) and used to verify if there is a terrain collision risk for the aircraft, a fourth means (7) for emitting an alarm signal in the event of detection of a collision risk by the third means (4), at least one aircraft performance data base (Bi) relating to an avoidance maneuvering gradient which can be flown by the aircraft according to particular flight parameters, and a fifth means (9) for determining the effective values of the particular parameters during the flight of the aircraft, wherein the third means (3) is formed in such a way that it is possible to determine the avoidance trajectory according to the information received from the data base (Bi) and the fifth means (9).

Abstract: A new and distinct variety of white nectarine tree denominated ‘NECTARCIEL’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh and slightly greenish at maturity time, and a red pigmentation into and around the stone cavity, and an attractive skin with a high percentage of luminous purple red blush on skin surface, on a red background.

Abstract: A new and distinct variety of white nectarine tree denominated ‘NECTARDALI’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh at maturity time, and a red pigmentation into and around the stone cavity, and an attractive skin with a luminous purple red blush on skin surface, on a red background.

Abstract: A new and distinct variety of white peach tree denominated ‘SWEETJAZZY’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet white flesh at maturity time, having a slightly pink pigmentation around the stone cavity, and an attractive skin with a luminous purple red blush on skin surface, on a purple red background.

Abstract: A new and distinct variety of white peach tree denominated ‘SWEETABBY’ which has fruits with high eating quality and very long shelf life without alteration before and after harvesting, with a semi-sweet cream white flesh at maturity time, and an attractive skin with a luminous dark purple red blush on skin surface, on a purple red background.