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公开(公告)号：WO2020127710A1
公开(公告)日：2020-06-25
申请号：PCT/EP2019/086279
申请日：2019-12-19
Applicant: SAFRAN ELECTRONICS & DEFENSE , ST ENGINEERING AEROSPACE LTD
Inventor： WALTER, Eric , FOUGERES, Loïc , DIAZ, Mikaël , TRANIE, Philippe , KWEE CHYE, Ng , SIEW LIONG, Tay
Abstract: A configuration system (80) arranged to configure an aircraft in a single-pilot mode and a two-pilot mode, comprising: - acquisition means (84) and authentication means (83) arranged to acquire and authenticate a configuration order that defines the selected mode and controls the configuration system (80) to configure the aircraft in the selected mode; - first activation means (85) arranged to activate equipment dedicated to piloting by a single-pilot on board when the aircraft is configured in single-pilot mode, and to deactivate dedicated equipment when the aircraft is configured in two-pilot mode; - verification means (87) arranged to, when the aircraft is configured in the single-pilot mode, verify that single-pilot flight conditions are met and inform the sole pilot on board and a ground station of the results of these checks.
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公开(公告)号：WO2019108127A1
公开(公告)日：2019-06-06
申请号：PCT/SG2017/050586
申请日：2017-11-29
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： ZHENG, Guo Ying
Abstract: A method of manufacturing a composite sandwich structure. The method may include individually providing a plurality of planar materials to form a stack. The plurality of planar materials may be free from physical interconnection from each other, and at least one of the plurality of planar materials may include one or more substantially continuous fiber layer as a constituent material of a plurality of constituent materials of the composite sandwich structure. The method may further include simultaneously applying heat and compression to the stack between a male mold and a female mold to form the composite sandwich structure.
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公开(公告)号：WO2019017834A1
公开(公告)日：2019-01-24
申请号：PCT/SG2017/050359
申请日：2017-07-19
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： HSI, Han Lin
IPC: B64D11/06
Abstract: A seat-back (100) for a passenger seat. The seat-back (100) may include a core framework (110) having a backing frame layer (120) and a back-rest boundary frame structure (130) connected to the backing frame layer (120). The seat-back (100) may further include a flexible cover (150) which may be fitted over the core framework (110) and which may be configured to substantially enclose the core framework (110), such that a back-rest portion (152) of the flexible cover (150) may be suspended across the back-rest boundary frame structure (130) and a backing portion (154) of the flexible cover (150) may be extended over the backing frame layer (120), so as to tension the back-rest portion (152) of the flexible cover (150) across the back-rest boundary frame structure (130) for supporting and cushioning a back of a user received on the back-rest portion (152) of the flexible cover (150).
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公开(公告)号：US12106675B2
公开(公告)日：2024-10-01
申请号：US17757876
申请日：2019-12-27
Applicant: ST Engineering Aerospace Ltd.
Inventor： Chi Hui Frederic Foo , Chuan Jen Peter Liew , Saik Kong Ronald Tan , Wei Ling Michelle Quek , Manjunath Ganesh Tiruvanmiyur
CPC classification number: G08G5/045 , G08G5/0008 , G08G5/0013 , G08G5/0021 , G08G5/0078 , G08G5/065
Abstract: The airport ground collision alerting system comprises an automatic dependent surveillance-broadcast, ADS-B, receiver; a first database coupled to the ADS-B receiver and configured for look-up of aircraft type data based on aircraft ID data received via the ADS-B receiver and for storing aircraft position and heading data received via the ADS-B receiver; a second database configured to store digital map data for one or more airports; a processor coupled to the first and second databases and an application programming interface, API, configured to couple the airport ground collision alerting system to a display device.
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公开(公告)号：US20230050381A1
公开(公告)日：2023-02-16
申请号：US17797981
申请日：2020-11-06
Inventor： Chun Yong, Andrew NGO , Vinod Kumar S/O SIVARAJA , Jun Yuan James TAN , Joshua VANU
IPC: G01N25/72
Abstract: A method (10) for detecting a thermal anomaly in a composite structure (12) is provided. The method (10) includes radiatively heating (14) the composite structure (12) for a period of between about 15 seconds (s) and about 25 s, cooling (24) the heated composite structure (12), monitoring (26) temperature changes of the composite structure (12) as the composite structure (12) cools, and generating (30) a thermal image of the composite structure (12) based on the temperature changes.
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Patent Agency Ranking
公开(公告)号：US11358719B2
公开(公告)日：2022-06-14
申请号：US16632233
申请日：2017-07-18
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： Keen Ian Chan
Abstract: An aerial vehicle including a first wing structure and a second wing structure which intersects the first wing structure perpendicularly at a position offset from a midpoint of a transverse axis of the first wing structure in a direction towards a first wingtip of the first wing structure. The aerial vehicle may further include a first set of at least two propellers with respective propeller rotational axes disposed side-by-side along a portion of the first wing structure extending between the midpoint of the transverse axis of the first wing structure and a second wingtip of the first wing structure. The aerial vehicle may further include a second set of at least two propellers with respective propeller rotational axes disposed side-by-side along a first portion of the second wing structure extending from a first surface of the first wing structure. The aerial vehicle may further include a third set of at least two propellers with respective propeller rotational axes disposed side-by-side along a second portion of the second wing structure extending from a second surface of the first wing structure.
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公开(公告)号：US20220306297A1
公开(公告)日：2022-09-29
申请号：US17606083
申请日：2020-08-19
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： Daniel William CLUCAS , Anthony Ralph Palliser HUDSON , Mitchell Anderw JOHNSTONE , Raymond John BETTELL
IPC: B64D11/02
Abstract: An accessible lavatory unit (103) for an aircraft cabin (102) is disclosed. The lavatory unit (103) is configurable between an able-bodied configuration and a PRM-accessible configuration. In the able-bodied configuration the lavatory unit has a first internal floor space (132) and there is a cabin floor space (130) external to the lavatory unit (103). The lavatory unit (103) is expandable into the PRM-accessible configuration in which the lavatory unit (103) is expanded to have a second internal floor space (132), the second internal floor space (132) encompassing a region of the cabin floor space (130). A sink for an aircraft lavatory unit is also disclosed.
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公开(公告)号：US20220063795A1
公开(公告)日：2022-03-03
申请号：US17416335
申请日：2019-12-19
Applicant: SAFRAN ELECTRONICS & DEFENSE , ST ENGINEERING AEROSPACE Ltd
Inventor： Eric WALTER , Loïc FOUGERES , Mikaël DIAZ , Philippe TRANIE , Ng KWEE CHYE , Tay SIEW LIONG
IPC: B64C13/12
Abstract: A configuration system (80) arranged to configure an aircraft in a single-pilot mode and a two-pilot mode, comprising: acquisition means (84) and authentication means (83) arranged to acquire and authenticate a configuration order that defines the selected mode and controls the configuration system (80) to configure the aircraft in the selected mode; first activation means (85) arranged to activate equipment dedicated to piloting by a single-pilot on board when the aircraft is configured in single-pilot mode, and to deactivate dedicated equipment when the aircraft is configured in two-pilot mode; verification means (87) arranged to, when the aircraft is configured in the single-pilot mode, verify that single-pilot flight conditions are met and inform the sole pilot on board and a ground station of the results of these checks.
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公开(公告)号：US20200172243A1
公开(公告)日：2020-06-04
申请号：US16632233
申请日：2017-07-18
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： Keen Ian CHAN
Abstract: An aerial vehicle including a first wing structure and a second wing structure which intersects the first wing structure perpendicularly at a position offset from a midpoint of a transverse axis of the first wing structure in a direction towards a first wingtip of the first wing structure. The aerial vehicle may further include a first set of at least two propellers with respective propeller rotational axes disposed side-by-side along a portion of the first wing structure extending between the midpoint of the transverse axis of the first wing structure and a second wingtip of the first wing structure. The aerial vehicle may further include a second set of at least two propellers with respective propeller rotational axes disposed side-by-side along a first portion of the second wing structure extending from a first surface of the first wing structure. The aerial vehicle may further include a third set of at least two propellers with respective propeller rotational axes disposed side-by-side along a second portion of the second wing structure extending from a second surface of the first wing structure.
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公开(公告)号：US20230084519A1
公开(公告)日：2023-03-16
申请号：US17800192
申请日：2020-12-14
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： Keen Ian CHAN
IPC: B64C27/10 , B64C27/467
Abstract: A method and system for generating a set of values for respective ones of a set of parameters used in determining rotor blade profiles for a corotating coaxial rotor system. The method comprises establishing a ratio of respective desired thrusts of an upper rotor and a lower rotor of the corotating coaxial rotor system based on a desired performance of the corotating coaxial rotor system; and determining the set of values of the set of parameters from the desired thrusts ratio based on an equal rotation speed condition between the upper rotor and the lower rotor of the corotating coaxial rotor system, wherein the set of parameters includes torques of the upper rotor and the lower rotor.
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