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公开(公告)号：US11827374B2
公开(公告)日：2023-11-28
申请号：US17041093
申请日：2019-03-25
申请人： SAFRAN , SAFRAN ELECTRICAL & POWER , SAFRAN HELICOPTER ENGINES , SAFRAN POWER UNITS , SAFRAN ELECTRONICS & DEFENSE
发明人： Thomas Klonowski , Thomas Barraco , Camel Serghine
CPC分类号： B64D35/02 , B64C27/08 , B64D27/24 , H02J7/0063 , B64D2027/026 , B64D2221/00 , B64U30/20
摘要： In the field of multi-rotor rotary-wing aircraft a propulsion system for such an aircraft includes a reconfigurable electric network for supplying the electric motors driving the rotors. The system includes: a supply source, a supply bus connected to the supply source, at least four drive units each including an electric motor and its control circuit, and an electrical ring network including: an electrical line which is interrupted at each drive unit and whose ends are connected to the supply bus, and, for each drive unit, a first switch and a second switch that are connected between the control circuit and the electrical line, on either side of the interruption.
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公开(公告)号：US20210139154A1
公开(公告)日：2021-05-13
申请号：US17041093
申请日：2019-03-25
申请人： SAFRAN , SAFRAN ELECTRICAL & POWER , SAFRAN HELICOPTER ENGINES , SAFRAN POWER UNITS , SAFRAN ELECTRONICS & DEFENSE
发明人： Thomas KLONOWSKI , Thomas BARRACO , Camel SERGHINE
摘要： In the field of multi-rotor rotary-wing aircraft a propulsion system for such an aircraft includes a reconfigurable electric network for supplying the electric motors driving the rotors. The system includes: a supply source, a supply bus connected to the supply source, at least four drive units each including an electric motor and its control circuit, and an electrical ring network including: an electrical line which is interrupted at each drive unit and whose ends are connected to the supply bus, and, for each drive unit, a first switch and a second switch that are connected between the control circuit and the electrical line, on either side of the interruption.
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公开(公告)号：US12065986B2
公开(公告)日：2024-08-20
申请号：US17790048
申请日：2020-12-23
申请人： SAFRAN NACELLES , SAFRAN LANDING SYSTEMS , SAFRAN ELECTRONICS & DEFENSE , SAFRAN AIRCRAFT ENGINES
CPC分类号： F02K1/32 , B64C25/426 , B64D45/00 , G05D1/101
摘要： This system (36) for controlling an aircraft thrust reversal means comprises a reverse idle control means (38), a first detection means (31) configured to detect, when the reverse idle control is active, a condition for activation of the thrust reversal means, and an actuation means (52) configured to activate the thrust reversal means when the first detection means (31) detects a condition for activation of the thrust reversal means.
It further comprises a second detection means (42, 44, 46, 48, 49) configured to detect a condition for activation of the reverse idle control, the control means (38) being configured to activate the reverse idle control when the second detection means (42, 44, 46, 48, 49) detects a condition for activating the reverse idle control.-
4.发明申请公开(公告)号：US20230137045A1
公开(公告)日：2023-05-04
申请号：US17913386
申请日：2021-03-18
申请人： SAFRAN AIRCRAFT ENGINES , SAFRAN ELECTRONICS & DEFENSE , SAFRAN LANDING SYSTEMS , SAFRAN NACELLES
发明人： Hakim MAALIOUNE , Laurent Christian Vincent Roger MIRALLES , Christophe BASTIDE , Jérémy Edmond FERT , Vincent HUPIN
摘要： A system for managing the deceleration of an aircraft enabling the control in real time of the position of the aircraft on a braking axis, includes a braking system; a calculator configured to: calculate, from aircraft data and from external data, a sequence of use of the braking system intended to brake the aircraft over a predetermined braking distance which associates a predetermined position on the braking axis with each braking instant; update in real time the sequence of use as a function of the difference between the position of the aircraft and the predetermined position; and a controller configured to control the braking system as a function of the sequence of use.
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公开(公告)号：US20230193515A1
公开(公告)日：2023-06-22
申请号：US17925595
申请日：2020-12-10
发明人： Paula Rebeca Realyvazquez Guevara , Mario Gerardo Herrera Murillo , Benjamin Py , James Woodington , Ghassen Ben Amor , Gérald Cotta , Adrien Beauvais
CPC分类号： D01F1/103 , B64D11/0647 , B60N2/75 , B60N3/002 , B60N2/60
摘要： Described are self-cleaning covers for attaching to passenger seats. Embodiments of self-cleaning covers can include an antimicrobial fabric having at least one antimicrobial fiber interwoven with a second fiber, as well as an attachment element connected with the antimicrobial fabric for removably affixing the cover to the seat. The antimicrobial fabric and the attachment element can be shaped to partially enclose and to removably attach the self-cleaning cover to at least a portion of the passenger seat, such as a seat cushion, armrest, or headrest.
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公开(公告)号：US20200040461A1
公开(公告)日：2020-02-06
申请号：US16305783
申请日：2017-05-30
发明人： Julien GURT SANTANACH , Alain VIOLA , Jean-Baptiste CAMBON , Rémy TURBAN , Jérémie Christian, André COTINOT
摘要： A method of chromating a part including an aluminum-based alloy, the method including the steps of providing the part including a layer based on aluminum oxide on at least one of its surfaces, of immersing the part in a chromating bath including chromium III, and of performing chemical conversion of the part in the chromating bath. The invention also provides a part obtained by the method.
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公开(公告)号：US20240105070A1
公开(公告)日：2024-03-28
申请号：US18265103
申请日：2021-12-01
申请人： SAFRAN AIRCRAFT ENGINES , SAFRAN ELECTRONICS & DEFENSE , SAFRAN LANDING SYSTEMS , SAFRAN NACELLES
CPC分类号： G08G5/025 , G08G5/0026
摘要： Said method for determining aircraft landing runway conditions comprises the steps of: acquiring a set of data groups of different types (D1, D2) for evaluating and monitoring runway degradation conditions; deriving weighting coefficients (Ki) from each data group; filtering the data; determining, for each data group, a partial runway condition; modifying the weighting coefficients of each data group; and combining the partial runway conditions to derive a runway condition coefficient (RWYCC) associated with a confidence index (C1) derived from the modified weighting coefficients.
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公开(公告)号：US20220412287A1
公开(公告)日：2022-12-29
申请号：US17790048
申请日：2020-12-23
申请人： SAFRAN NACELLES , SAFRAN LANDING SYSTEMS , SAFRAN ELECTRONICS & DEFENSE , SAFRAN AIRCRAFT ENGINES
摘要： This system (36) for controlling an aircraft thrust reversal means comprises a reverse idle control means (38), a first detection means (31) configured to detect, when the reverse idle control is active, a condition for activation of the thrust reversal means, and an actuation means (52) configured to activate the thrust reversal means when the first detection means (31) detects a condition for activation of the thrust reversal means.
It further comprises a second detection means (42, 44, 46, 48, 49) configured to detect a condition for activation of the reverse idle control, the control means (38) being configured to activate the reverse idle control when the second detection means (42, 44, 46, 48, 49) detects a condition for activating the reverse idle control.-
公开(公告)号：US12071250B2
公开(公告)日：2024-08-27
申请号：US17282549
申请日：2019-10-01
CPC分类号： B64D27/24 , H02J1/14 , H02J7/345 , B64D27/026 , H02J2310/44
摘要： An aircraft with hybrid thermal/electrical propulsion includes a turbomachine; a first electrical source; a second electrical source equipped with an electrical energy storage device; a non-propulsion electrical distribution network; a low-voltage electrical distribution network; and a propulsion electrical distribution network. The three electrical distribution networks are electrically supplied by the first and second electrical sources and electrically interconnected by static converters.
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公开(公告)号：US11655053B2
公开(公告)日：2023-05-23
申请号：US16759539
申请日：2018-10-26
申请人： COMPAGNIE GENERALE DES ETABLISSEMENTS MICHELIN , SAFRAN , SAFRAN LANDING SYSTEMS , SAFRAN ELECTRONICS & DEFENSE
发明人： Michael Arnoux , Eric Carin Neba
CPC分类号： B64F5/60 , B60C23/02 , B60C23/0479 , B64C25/36 , B64F5/40 , B64D2045/0085
摘要： A method determines an inflation pressure expected in an aircraft tire provided with a pressure and temperature sensor. Also disclosed is a method for assistance in the maintenance for an aircraft tire and also a portable electronic device intended for assistance in the maintenance.
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