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公开(公告)号：US12129024B2
公开(公告)日：2024-10-29
申请号：US17555299
申请日：2021-12-17
CPC分类号： B64C29/0025 , B64C3/38 , B64C21/02 , F02K1/002
摘要： The present disclosure provides systems, apparatuses, and methods relating to a fan apparatus including a lift fan mounted in a duct and a cover for the lift fan. In some examples, a fan apparatus has a louvered cover including louvers having different chord lengths and/or different projection distances relative to one another when the louvers are in an intermediate (transitional) position. In some examples, a fan apparatus includes a louver actuation assembly configured to move louvers of the fan apparatus rotationally and translationally between open and closed positions. In some examples, a fan apparatus includes a fluid-actuated sealing assembly configured to form a seal between a sealing member and a cover, such as a louvered cover.
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公开(公告)号：US20220194575A1
公开(公告)日：2022-06-23
申请号：US17555299
申请日：2021-12-17
摘要： The present disclosure provides systems, apparatuses, and methods relating to a fan apparatus including a lift fan mounted in a duct and a cover for the lift fan. In some examples, a fan apparatus has a louvered cover including louvers having different chord lengths and/or different projection distances relative to one another when the louvers are in an intermediate (transitional) position. In some examples, a fan apparatus includes a louver actuation assembly configured to move louvers of the fan apparatus rotationally and translationally between open and closed positions. In some examples, a fan apparatus includes a fluid-actuated sealing assembly configured to form a seal between a sealing member and a cover, such as a louvered cover.
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公开(公告)号：US20240359826A1
公开(公告)日：2024-10-31
申请号：US18307412
申请日：2023-04-26
申请人： The Boeing Company
CPC分类号： B64F5/60 , G06N3/006 , G07C5/008 , G07C5/0808 , G07C5/0816
摘要： Example implementations relate to predicting the health of an aircraft component based on a hybrid digital twin. A computing system receives nominal operational data and operational data from aircraft sensors based on flights by an aircraft to evaluate an aircraft component on the aircraft. The computing system can estimate first parameters corresponding to the aircraft component based on a nominal digital twin using the nominal operational data outside respective alerts corresponding to the aircraft component and second parameters corresponding to the aircraft component based on an operational digital twin using the operational data. The computing system then estimates a first health parameter and a second health parameter for the aircraft component based on the first parameters and the second parameters, respectively. The computing system performs a comparison between the first health parameter and the second health parameter in order to provide a value for the aircraft component that represents the health of the aircraft component.
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公开(公告)号：US20240359818A1
公开(公告)日：2024-10-31
申请号：US18765268
申请日：2024-07-07
申请人： The Boeing Company
摘要： Systems and methods for enabling charged (ionized) air mass measurement for reliable air data computation onboard an aircraft. Ionic charge sensing may be used to derive air data having improved reliability. The systems and methods for ionic charge sensing employ an emitter electrode and two or more collector electrodes, which electrodes are disposed in proximity to the exterior skin of the aircraft and exposed to ambient air. The emitter electrode is positioned forward of the collector electrodes. The system further includes a solid-state ionic air data module that converts currents from the collector electrodes into air data parameter values. More specifically, the ionic air data module is configured to sense currents induced in the collector electrodes in response to corona discharge produced by the high-voltage emitter electrode.
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公开(公告)号：US20240359480A1
公开(公告)日：2024-10-31
申请号：US18765722
申请日：2024-07-08
申请人： The Boeing Company
CPC分类号： B41J2/18 , B41J2/07 , B41J2/17556 , B41J3/4073 , B05B12/085 , B41J2/17513 , B41J2/17566
摘要： Inkjet printing systems and methods dynamically control meniscus pressure at a nozzle to more reliably deliver ink to a substrate. The systems and methods include inferring an angle of a longitudinal axis of a printhead relative to the vertical reference axis based on an orientation signal from an orientation sensor, determining a target feed fluid pressure upstream of the nozzle and a target recirculation fluid pressure downstream of the nozzle, thereby to maintain a target pressure differentiation across the nozzle based, at least in part, on the inferred angle of the longitudinal axis, and controlling a variable feed pump speed and a variable recirculation pump speed to obtain the target feed fluid pressure and the target recirculation fluid pressure.
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公开(公告)号：US20240356628A1
公开(公告)日：2024-10-24
申请号：US18304277
申请日：2023-04-20
申请人： The Boeing Company
CPC分类号： H04B7/18504 , B64U10/14 , B64U2101/20
摘要： A secondary communication system for an unmanned aerial vehicle (UAV) is provided. The secondary communication system comprises at least one motor on the UAV and a motor controller in each motor that generates a signal from noise generated by the motor. A connector is configured to connect a towed sensor assembly to the UAV. A sensor acts as a receiver for the UAV, wherein the sensor receives a signal from a transmission source other than the UAV. The sensor is towed on the connector at a distance from the UAV sufficient to prevent or minimize interference of the received signal by the noise generated by the motor.
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公开(公告)号：US20240353272A1
公开(公告)日：2024-10-24
申请号：US18302892
申请日：2023-04-19
申请人： The Boeing Company
摘要： A device for analysis of mechanical and thermal loading of structures can include: a first member comprising first material; a second member comprising second material; and a third member comprising the first material. The second member can be fastened at least partially between the first and third members. The device can be configured to mechanically load the first, second, and third members by applying equal and opposite force to protruding ends of the first, second, and third members. A device for analysis of mechanical and thermal loading of structures can include: a first member comprising first material; and a second member comprising second material. The first member can be fastened at least partially between portions of the second member. The device can be configured to mechanically load the first and second members by applying equal and opposite force to protruding ends of the first and second members.
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8.发明公开公开(公告)号：US20240352260A1
公开(公告)日：2024-10-24
申请号：US18758637
申请日：2024-06-28
申请人： The Boeing Company
IPC分类号： C09D5/08 , C08K5/405 , C09D157/00 , C09D187/00
CPC分类号： C09D5/08 , C09D157/00 , C09D187/00 , C08K5/405
摘要： A corrosion inhibition composition includes a carrier and a Schiff base in admixture with the carrier. The carrier includes at least one of water, a hydrocarbon solvent, and a binder.
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公开(公告)号：US20240351245A1
公开(公告)日：2024-10-24
申请号：US18305538
申请日：2023-04-24
申请人： The Boeing Company
发明人： Jacquelynn X. Tian
摘要： A pipe segment for thermoset manufacturing includes a pipe body with an exterior surface, a main inlet portion, a main outlet portion, a secondary inlet portion and a secondary outlet portion. The pipe body defines a main chamber and a secondary chamber. A nozzle for thermoset manufacturing includes a nozzle body with an exterior surface, a main inlet portion, a main outlet portion, a secondary inlet portion and a secondary outlet portion. The nozzle body defines a main chamber and a secondary chamber. The main inlet portion includes at least two main inlet orifices. The main outlet portion includes a main outlet orifice. The secondary inlet portion includes a secondary inlet orifice. The secondary outlet portion includes a secondary outlet orifice. A system for thermoset manufacturing includes a pipe segment, a three-way valve and first, second and third fluid subsystems. A method for thermoset manufacturing is also provided.
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公开(公告)号：US12122511B2
公开(公告)日：2024-10-22
申请号：US17455607
申请日：2021-11-18
发明人： Andrew Heafitz
CPC分类号： B64C39/024 , G06T7/12 , G06T7/13 , G06T7/174 , G06V10/26 , G06V10/60 , B64U2101/30 , B64U2201/10
摘要： A method is provided for horizon detection. The method includes acquiring an image that depicts a view of an environment, and defining a line pattern of lines that divide the image into respective pairs of image segments. The line pattern is formed of lines that are parallel, or intersecting at a common point of intersection. The method includes searching the lines of the line pattern to identify one of the lines as an estimated true horizon in the image that divides the image into a respective pair of image segments at a boundary of greatest difference in average brightness between the image segments from among the respective pairs of image segments. The method includes determining true horizon in the image from the estimated true horizon. The method may also include an evaluation of the estimated true horizon or the true horizon as to verify one or more expected characteristics.
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