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公开(公告)号：JP6483853B2
公开(公告)日：2019-03-13
申请号：JP2017553425
申请日：2015-04-13
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公开(公告)号：WO2020127706A1
公开(公告)日：2020-06-25
申请号：PCT/EP2019/086273
申请日：2019-12-19
Applicant: SAFRAN ELECTRONICS & DEFENSE , ST ENGINEERING AEROSPACE LTD
Inventor： WALTER, Eric , FARJON, Julien , DIAZ, Mikaël , CADALEN, Nicolas , TRANIE, Philippe , KWEE CHYE, Ng , TA HUANG JACKSON, Hoon
Abstract: A method for piloting a pre-existing aircraft comprising the following steps: - integrating an alternative piloting system (1) into the pre-existing aircraft; - connecting the aircraft (200) and a ground station in which a ground pilot (207) is positioned; - when the aircraft is in a normal state, having the aircraft piloted by a nominal crew; - using detection means to detect the occurrence of an emergency situation and, when the occurrence of the emergency is detected: - making the ground pilot (207) operational, so that the ground pilot can produce an aircraft ground piloting set- point; - transmitting the ground piloting setpoint to the aircraft; - using the alternative piloting system to acquire and transmit the ground piloting setpoint to the aircraft flight con¬ trol system.
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公开(公告)号：WO2018208220A1
公开(公告)日：2018-11-15
申请号：PCT/SG2017/050241
申请日：2017-05-09
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： CHAN, Keen Ian
Abstract: An aerial vehicle may include a first wing structure. The aerial vehicle may further include a first propeller and a second propeller disposed along the first wing structure. The aerial vehicle may further include a second wing structure disposed to intersect the first wing structure to form a cross configuration. The aerial vehicle may further include a third propeller and a fourth propeller disposed along the second wing structure. In a hovering orientation of the aerial vehicle, respective propeller rotational axes of the first and second propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the first wing structure, and respective propeller rotational axes of the third and fourth propellers may be angled off-vertical in respective planes which may be perpendicular to a transverse axis of the second wing structure.
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公开(公告)号：WO2021145817A1
公开(公告)日：2021-07-22
申请号：PCT/SG2020/050014
申请日：2020-01-13
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： HUDSON, Anthony Ralph Palliser
IPC: B64D11/02
Abstract: There is provided a lavatory unit for installing adjacent an aisle in an aircraft cabin. The lavatory unit comprises a cabinet for dispensing lavatory amenities. The cabinet comprises an amenities cartridge received in a cabinet casing. The amenities cartridge comprises a storage compartment for storing an amenity and an amenity outlet through which the amenity is accessible. The cabinet casing comprises a dispensing opening through which the amenity outlet of the amenities cartridge is accessible, such that the amenity in the amenities cartridge is accessible from the lavatory unit, and a refill opening on a side of the cabinet casing facing the aisle. The amenities cartridge is removable from the cabinet casing through the refill opening, to allow access to the storage compartment from the aisle. The dispensing opening is open-sided on the side of the cabinet facing the aisle, so that as the amenities cartridge is moved through the refill opening, an amenity protruding from the amenity outlet in the amenities cartridge is unobstructed during movement into/out of the dispensing opening.
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公开(公告)号：WO2021040615A1
公开(公告)日：2021-03-04
申请号：PCT/SG2020/050481
申请日：2020-08-19
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： CLUCAS, Daniel William , HUDSON, Anthony Ralph Palliser , JOHNSTONE, Mitchell Andrew , BETTELL, Raymond John
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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Patent Agency Ranking
公开(公告)号：WO2019108126A1
公开(公告)日：2019-06-06
申请号：PCT/SG2017/050585
申请日：2017-11-29
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： HSI, Han Lin
CPC classification number: B29C33/485 , B22C9/103 , B29C33/3835 , B29C33/3842 , B29C70/42 , B29L2031/757 , B33Y80/00
Abstract: A core assembly for moulding and a method of moulding thereof. The core assembly may include a plurality of separable rigid parts configured to be joined together to form a hollow channel therebetween, and at least one insert configured to be removably insertable into the hollow channel and further configured to bear against at least two of the plurality of separable rigid parts so as to maintain the plurality of separable rigid parts in respective positions in an assembled state of the core assembly. An exterior surface of the core assembly in the assembled state may form a moulding surface.
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公开(公告)号：WO2019017833A1
公开(公告)日：2019-01-24
申请号：PCT/SG2017/050356
申请日：2017-07-18
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： CHAN, Keen Ian
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：WO2022093109A1
公开(公告)日：2022-05-05
申请号：PCT/SG2020/050745
申请日：2020-12-14
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： CHAN, Keen Ian
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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公开(公告)号：WO2021158170A1
公开(公告)日：2021-08-12
申请号：PCT/SG2020/050639
申请日：2020-11-06
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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公开(公告)号：WO2021133246A1
公开(公告)日：2021-07-01
申请号：PCT/SG2019/050648
申请日：2019-12-27
Applicant: ST ENGINEERING AEROSPACE LTD.
Inventor： FOO, Chi Hui Frederic , LIEW, Chuan Jen Peter , TAN, Saik Kong Ronald , QUEK, Wei Ling Michelle , TIRUVANMIYUR, Manjunath Ganesh
Abstract: An airport ground collision alerting system and a method of operating an airport ground collision alerting system. 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 unit 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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