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公开(公告)号：US10450085B2
公开(公告)日：2019-10-22
申请号：US15384978
申请日：2016-12-20
Applicant: THE BOEING COMPANY
Inventor： Jeffrey L. Williams , Jason W. Clark , Susan A. Foster , Samantha A. Schwartz , Aaron D. Pilcher
Abstract: A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
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公开(公告)号：US10147330B2
公开(公告)日：2018-12-04
申请号：US15475260
申请日：2017-03-31
Applicant: THE BOEING COMPANY
Inventor： Samantha A. Schwartz , Garoe Gonzalez Parra , Adam Karwan , Marcin Zadroga
Abstract: A flight path holding pattern system is configured to determine an efficient holding pattern for an aircraft. The flight path holding pattern system includes a holding pattern determination unit that is configured to automatically generate the holding pattern for the aircraft based on one or more of current air traffic in relation to a destination airport, historical holding patterns in relation to the destination airport, current weather conditions in relation to the destination airport, and fuel consumption of one or both of the aircraft and at least one other aircraft.
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公开(公告)号：US20170101193A1
公开(公告)日：2017-04-13
申请号：US15384978
申请日：2016-12-20
Applicant: THE BOEING COMPANY
Inventor： Jeffrey L. Williams , Jason W. Clark , Susan A. Foster , Samantha A. Schwartz , Aaron D. Pilcher
IPC: B64D45/00
CPC classification number: B64D45/00 , B64D43/00 , B64D2045/0075 , G01C21/00 , G04B99/00 , G04G9/0064
Abstract: A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
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14.发明申请WEARABLE ELECTRONIC DISPLAY AND METHOD FOR DISPLAYING INFORMATION TO A PILOT 有权用于向导航台显示信息的可佩戴的电子显示器和方法公开(公告)号：US20160347472A1
公开(公告)日：2016-12-01
申请号：US14722449
申请日：2015-05-27
Applicant: THE BOEING COMPANY
Inventor： Jeffrey L. Williams , Jason W. Clark , Susan A. Foster , Samantha A. Schwartz , Aaron D. Pilcher
IPC: B64D45/00
CPC classification number: B64D45/00 , B64D43/00 , B64D2045/0075 , G01C21/00 , G04B99/00 , G04G9/0064
Abstract: A wearable electronic display system detects aircraft flight related conditions, compares the detected flight related conditions with rules or procedures, retrieves flight condition information relating to phase of flight, and displays small amounts of contextually relevant flight condition information on a display screen.
Abstract translation: 可穿戴电子显示系统检测飞行器飞行相关条件，将检测到的飞行相关条件与规则或程序进行比较，检索与飞行相关的飞行情况信息，并在显示屏幕上显示少量上下文相关飞行状况信息。
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公开(公告)号：US09376216B2
公开(公告)日：2016-06-28
申请号：US14291279
申请日：2014-05-30
Applicant: The Boeing Company
Inventor： Samantha A. Schwartz , Andreas Godehart , Nils Kneuper , Andre Lutz , Mariusz Nawotczynski
CPC classification number: B64D45/00 , B64D37/005 , B64D43/00 , B64D2045/0075 , G05D1/00
Abstract: A method and apparatus for predicting fuel for an aircraft. Remaining amounts of fuel that will be present for types of fuel use for the aircraft at a destination are predicted. Flight times for the types of fuel use are calculated from the remaining amounts of fuel predicted for the types of fuel use for the aircraft at the destination. Graphical indicators are displayed indicating the types of fuel use and the flight times for the types of fuel use.
Abstract translation: 一种用于预测飞机燃料的方法和装置。 预测将在目的地为飞机燃料使用的剩余燃料量。 燃料使用类型的飞行时间是根据目的地的飞机燃料类型预测的剩余燃料量计算的。 显示图形指示器，指示燃料使用的类型和燃料使用类型的飞行时间。
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Patent Agency Ranking
公开(公告)号：US20240265818A1
公开(公告)日：2024-08-08
申请号：US18163677
申请日：2023-02-02
Applicant: The Boeing Company
Inventor： Samantha A. Schwartz , Garoe Gonzalez
CPC classification number: G08G5/065 , B64D43/00 , G08G5/0073
Abstract: A system and method are provided for an aircraft at an airport surrounded by an environment, the aircraft having a first engine and a second engine wherein the second engine is to be started after the first engine. The system and method are configured for determining a minimum amount of warm-up time needed for starting the second engine to meet predetermined start-up requirements for the second engine, based on one or more of engine-related information relating to the second engine, aircraft-related information relating to the aircraft, airport-related information relating to the airport, and environment-related information relating to the environment, and producing an alert based on the minimum amount of warm-up time needed.
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公开(公告)号：US20240262527A1
公开(公告)日：2024-08-08
申请号：US18163678
申请日：2023-02-02
Applicant: The Boeing Company
Inventor： Samantha A. Schwartz , Garoe Gonzalez
Abstract: A system and method for determining which engine of an aircraft to start first for a taxiing operation and/or for estimating a total amount of fuel needed by the aircraft for conducting the taxiing operation includes receiving or accessing historical fuel usage data for each of the first and second engines, receiving or accessing taxiway information, determining which of the first and second engines to start before the other based on optimizing one or more predetermined factors, and producing a first-to-start alert indicating which of the first and second engines is a first-to-start engine. An engine use plan may be determined, the total amount of fuel needed for executing the taxiing operation may be estimated, and a fuel-estimate indication may be produced.
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公开(公告)号：US11335202B2
公开(公告)日：2022-05-17
申请号：US16861492
申请日：2020-04-29
Applicant: The Boeing Company
Inventor： Miriam Cornel , Michelle Wenzel , Garoe Gonzalez , Samantha A. Schwartz
IPC: G08G5/00
Abstract: A computer-implemented method. The method includes receiving a data structure being a network having nodes linked by links. The nodes have corresponding classes representing corresponding distinct notices to airmen (NOTAMs). The nodes are linked such that any given node is linked to at least one other node. The links represent corresponding pre-determined mathematical degrees of relevance between pairs of linked nodes. The links point from a corresponding less relevant node to a corresponding more relevant node. The nodes are pre-ranked in a prioritized order according to the pre-determined mathematical degree of relevance. The method also includes receiving a request to display the NOTAMs on a display device. The method also includes retrieving the NOTAMs associated with the nodes in the prioritized order. The method also includes commanding the NOTAMS to be displayed on the display device in the prioritized order.
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公开(公告)号：US20210343151A1
公开(公告)日：2021-11-04
申请号：US16861492
申请日：2020-04-29
Applicant: The Boeing Company
Inventor： Miriam Cornel , Michelle Wenzel , Garoe Gonzalez , Samantha A. Schwartz
IPC: G08G5/00
Abstract: A computer-implemented method. The method includes receiving a data structure being a network having nodes linked by links. The nodes have corresponding classes representing corresponding distinct notices to airmen (NOTAMs). The nodes are linked such that any given node is linked to at least one other node. The links represent corresponding pre-determined mathematical degrees of relevance between pairs of linked nodes. The links point from a corresponding less relevant node to a corresponding more relevant node. The nodes are pre-ranked in a prioritized order according to the pre-determined mathematical degree of relevance. The method also includes receiving a request to display the NOTAMs on a display device. The method also includes retrieving the NOTAMs associated with the nodes in the prioritized order. The method also includes commanding the NOTAMS to be displayed on the display device in the prioritized order.
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公开(公告)号：US20190156682A1
公开(公告)日：2019-05-23
申请号：US15821526
申请日：2017-11-22
Applicant: The Boeing Company
Inventor： Samantha A. Schwartz , Andres C. Fermon , Brian A. Azcuenaga , Melissa I. Blackstun
Abstract: An airport computing system is communicatively coupled to a first airplane and to one or more second airplanes over a network system. The airport computing system comprises a plurality of sensors associated with the first airplane. The airport computing system comprises a data module configured to receive data from the first airplane over the network. The data comprises runway data sampled using the plurality of sensors while the first airplane is on a runway. The airport computing system also comprises a parameter module configured to determine one or more parameters that describe a condition for the runway based on the received runway data. The airport computing system further comprises a transmission module configured to transmit the one or more parameters to the one or more second airplanes over the network.
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