公开(公告)号：US07873446B2

公开(公告)日：2011-01-18

申请号：US11706671

申请日：2007-02-13

Applicant: Christopher J. Shehi ,  Jary E. Engels

Inventor： Christopher J. Shehi ,  Jary E. Engels

IPC: G06F17/00

CPC classification number: G01C5/005

Abstract: A system and method for storing altimeter setting values on an aircraft display includes simultaneously rendering an altimeter and an active altimeter setting field, and selectively rendering a standby altimeter setting field simultaneously with the altimeter and the active altimeter setting field. An active altimeter setting value is rendered in the active altimeter setting field, and a stored altimeter setting value may be rendered in the standby altimeter setting field. Preferably, the stored altimeter setting value is selectively rendered in the standby altimeter setting field when the standby altimeter setting field is simultaneously rendered with the altimeter and the active altimeter setting field.

Abstract translation: 用于在飞行器显示器上存储高度计设置值的系统和方法包括同时呈现高度计和活动高度计设置字段，并且与高度计和活动高度计设置字段同时选择性地呈现备用高度计设置字段。 有效高度计设置值在有效高度计设置字段中呈现，并且可以在备用高度计设置字段中显示存储的高度计设置值。 优选地，当备用高度计设定栏与高度计和有效高度计设定栏同时呈现时，存储的高度计设定值被选择性地呈现在备用高度计设定区域中。

公开(公告)号：US20100219986A1

公开(公告)日：2010-09-02

申请号：US12599640

申请日：2008-05-05

Applicant: Laurent Azoulai

Inventor： Laurent Azoulai

IPC: G08B21/00 ,  G01S3/02 ,  G01L7/20

CPC classification number: G01C5/005

Abstract: Method and device for monitoring a horizontal position of an aircraft rolling on the ground. The device (1) comprises an altimeter (3) and means (4, 6, 8, 10, 12) for detecting, with the aid of measurements carried out by the altimeter (3), an error of an indication of horizontal position emitted by a positioning device (2).

Abstract translation: 用于监测在地面上滚动的飞行器的水平位置的方法和装置。 装置（1）包括高度计（3）和用于借助于高度计（3）进行的测量来检测发射的水平位置的指示的误差（4,6,8,10,12） 通过定位装置（2）。

公开(公告)号：US20090229632A1

公开(公告)日：2009-09-17

申请号：US12321321

申请日：2009-01-16

Applicant: Mohamed Emam Labib ,  Chung-Yue Lai ,  Yacoob Tabani

Inventor： Mohamed Emam Labib ,  Chung-Yue Lai ,  Yacoob Tabani

IPC: B08B9/027 ,  B08B3/08 ,  A61L2/22

CPC classification number: C11D3/48 ,  A61B90/70 ,  A61B2090/701 ,  A61L2/18 ,  A61L2/22 ,  A61M1/1682 ,  A61M1/169 ,  B01D65/02 ,  B01D65/022 ,  B01D2321/04 ,  B01D2321/185 ,  B01D2321/28 ,  B08B9/032 ,  B08B9/0326 ,  B08B9/0327 ,  B08B2209/022 ,  C11D3/044 ,  C11D3/3956 ,  C11D11/0041 ,  C23G1/00 ,  C23G5/00 ,  G01C5/005

Abstract: An apparatus and method for cleaning passageways and the like with a two-phase mixture of gas under pressure and an aqueous cleaning solution. The two-phase cleaning mixture is generated in a module and is passed out of the module at a predetermined rate that determines droplet size, velocity and droplet density at the pipeline surface to be cleaned. The droplets impact the walls of the passageway to be cleaned, thereby fragmenting, eroding and removing contaminants in said passageway. These are then flushed out of the passageway by the two-phase flow. The flow of cleaning solution can be steady or pulsed. The apparatus and process include a clean-in-place system that is useful in food, beverage, pharmaceutical and similar process industries.

Abstract translation: 一种用于在压力下与气体两相混合物和水性清洗溶液清洗通道等的装置和方法。 两相清洁混合物在模块中产生，并以预定的速率流出模块，该预定速率决定待清洁的管道表面上的液滴尺寸，速度和液滴密度。 液滴冲击待清洁通道的壁，从而破碎，侵蚀和去除所述通道中的污染物。 然后通过两相流将它们冲出通道。 清洁液的流动可以是稳定的或脉冲的。 该设备和方法包括在食品，饮料，制药和类似加工工业中有用的现场清洁系统。

公开(公告)号：US07551990B2

公开(公告)日：2009-06-23

申请号：US10908261

申请日：2005-05-04

Applicant: Ratan Khatwa

Inventor： Ratan Khatwa

IPC: G08G5/04 ,  G01S13/94

CPC classification number: G01C5/005

Abstract: Systems and methods for managing a visual display in a ground proximity warning system. In one embodiment, a system includes at least one aircraft sensor system operable to acquire aircraft data and a ground proximity warning computer coupled to the aircraft sensor system that is operable to process the aircraft data to generate ground proximity warning data corresponding to a sensed ground obstruction. An indicating system includes at least one visual display device that is operable to display terrain elevations and to display a visual symbol corresponding to at least one of the ground obstructions, wherein at least one of the computer and the visual display device is controllable to selectively alter an appearance of the visual symbol relative to the terrain elevations.

Abstract translation: 用于管理地面接近警报系统中的视觉显示的系统和方法。 在一个实施例中，系统包括可操作以获取飞行器数据的至少一个飞行器传感器系统和耦合到飞行器传感器系统的地面接近警告计算机，其可操作以处理飞行器数据以产生对应于感测到的地面障碍物的地面接近警告数据 。 指示系统包括至少一个视觉显示装置，其可操作以显示地形高度并显示对应于至少一个地面障碍物的视觉符号，其中计算机和视觉显示装置中的至少一个是可控制的，以选择性地改变 相对于地形高程的视觉符号的外观。

公开(公告)号：US07433781B2

公开(公告)日：2008-10-07

申请号：US11719032

申请日：2005-10-18

Applicant: Elias Bitar ,  Nicolas Marty

Inventor： Elias Bitar ,  Nicolas Marty

IPC: G08G5/04 ,  G05D1/06

CPC classification number: G08G5/0086 ,  G01C5/005 ,  G01C23/00 ,  G08G5/0021

Abstract: This device furnishes a map for assisting navigation at low-level altitude while representing the zone flown over with points shown in false colors and/or textures or symbols corresponding to the vertical speeds needed to fly over them.

Abstract translation: 该装置提供用于辅助低水平高度导航的地图，同时代表以虚拟颜色和/或对应于飞过它们所需的垂直速度的纹理或符号所示的点而飞越的区域。

公开(公告)号：US20080215195A1

公开(公告)日：2008-09-04

申请号：US11908786

申请日：2006-03-01

Applicant: Christophe Jourdan ,  Pierre Fabre ,  Stephane Walter ,  Isabelle Lacaze

Inventor： Christophe Jourdan ,  Pierre Fabre ,  Stephane Walter ,  Isabelle Lacaze

IPC: G05D1/08 ,  G08G5/04

CPC classification number: G05D1/0646 ,  G01C5/005 ,  G08G5/045

Abstract: The invention concerns a terrain avoidance method and system for an aircraft. The system comprises a collision alarm device (3) and an auto-pilot device (5) including means (7) for determining a climbing order with optimal slope for the aircraft, means (12) for checking whether a first altitude gain at the relief, by applying the optimal slope climbing order, is sufficient for clearing said relief, means (11) for finding if there exists at least one heading variation value, for which the corresponding altitude gain is sufficient to clear the relief, and means (17, 22) for applying to the aircraft, if the first altitude gain is sufficient, an optimal slope climbing order with an order to maintain the current heading and, if the first altitude gain is insufficient, a particular climbing order sufficient to clear the relief, with a heading order which corresponds to the selected heading variation value.

Abstract translation: 本发明涉及一种用于飞机的地形避免方法和系统。 该系统包括碰撞报警装置（3）和自动导向装置（5），包括用于确定飞行器具有最佳斜率的爬坡顺序的装置（7），用于检查救护装置上的第一高度增益的装置（12） 通过应用最佳坡度攀爬顺序，足以清除所述浮雕，用于查找是否存在至少一个航向变化值的装置（11），对于该航向变化值，相应的高度增益足以清除浮雕，以及装置（17） 22）如果第一高度增益是足够的，则适用于第一高度增益的最佳斜坡爬坡顺序，以保持当前航向，如果第一高度增益不足，则具有足以清除浮雕的特定爬坡顺序， 对应于所选择的航向变化值的航向顺序。

公开(公告)号：US07394402B2

公开(公告)日：2008-07-01

申请号：US11161368

申请日：2005-08-01

Applicant: Yasuo Ishihara ,  Steve C. Johnson

Inventor： Yasuo Ishihara ,  Steve C. Johnson

IPC: G08B23/00

CPC classification number: G05D1/0676 ,  G01C5/005

Abstract: Systems, methods and computer program products for alerting a flight crew during landing that the tailwind exceeds acceptable limits. The system determines a base tailwind threshold speed for a candidate runway based on a performance constant associated with an aircraft and candidate runway information and determines present tailwind speed. If the tailwind speed is greater than the base tailwind threshold speed, a tailwind alert is generated. Also, the system determines if the aircraft is in a tailwind alerting mode based on configuration of the aircraft and activates tailwind alerting, if it is determined that the aircraft is in the tailwind alerting mode.

Abstract translation: 系统，方法和计算机程序产品，用于在着陆期间提醒飞行机组人员，后排超过可接受的限制。 系统基于与飞行器和候选跑道信息相关联的性能常数来确定候选跑道的基本倒带阈值速度，并确定当前的顺风速度。 如果顺风速度大于基本的倒档门限速度，则会产生顺风警报。 此外，如果确定飞行器处于顺风警报模式，则系统基于飞行器的配置来确定飞行器是否处于顺风警报模式，并启动顺风警报。

公开(公告)号：US20070013558A1

公开(公告)日：2007-01-18

申请号：US11160509

申请日：2005-06-27

Applicant: Yasuo Ishihara

Inventor： Yasuo Ishihara

IPC: G08B21/00

CPC classification number: G08G5/0086 ,  G01C5/005 ,  G01S13/882 ,  G08G5/025

Abstract: A method, computer software product, and system to generate altitude callouts according to proximity to a runway at an airport or heliport includes determining whether the helicopter is flying in proximity to the runway and automatically selecting an altitude threshold increment set based upon the determination. The threshold increment set including a plurality of altitude threshold values. A calculated terrain clearance value is calculated for each of the plurality of altitude threshold values. A suitable warning is automatically generated according to the comparison. Selecting an altitude threshold increment set includes selecting one of the group consisting of first altitude threshold increment set including a plurality of higher altitude threshold values and a second altitude increment set including the plurality of higher altitude threshold values and further including a plurality of lower altitude threshold values.

Abstract translation: 根据机场或直升机场的跑道附近产生高度标注的方法，计算机软件产品和系统包括确定直升机是否在靠近跑道的地方飞行，并且基于该确定自动选择设置的高度阈值增量。 包括多个高度阈值的阈值增量集合。 为多个高度阈值中的每一个计算出计算出的地形距离值。 根据比较自动生成合适的警告。 选择高度阈值增量集合包括选择由包括多个较高海拔阈值的第一高度阈值增量集合和包括多个较高高度阈值的第二高度增量集合组成的组中的一个，并且还包括多个较低高度阈值 价值观。

公开(公告)号：US20060102797A1

公开(公告)日：2006-05-18

申请号：US11122104

申请日：2005-05-05

Applicant: Franck Artini ,  Edward Strongman

Inventor： Franck Artini ,  Edward Strongman

IPC: G05D1/10

CPC classification number: G01C5/005 ,  G05D1/105

Abstract: The device (1) for guiding an aircraft at least over an intermediate trajectory between a first flight trajectory for a low-altitude flight and a second flight trajectory which starts at an initial point, and from which trajectory a parachute drop is carried out, comprises means (9) for determining a point of transition which lies on the first flight trajectory which represents the start of the intermediate trajectory, and which corresponds to the point where the aircraft must exit the first flight trajectory so as to reach the initial point under predetermined flight conditions, and means (13A, 13B) which use the point of transition to aid the guidance of the aircraft between the first and second flight trajectories.

Abstract translation: 用于引导飞行器至少在用于低空飞行的第一飞行轨迹和从初始点开始的第二飞行轨迹之间的中间轨迹以及执行降落伞降落的轨迹的装置（1）包括 用于确定位于第一飞行轨迹上的转换点的装置（9），其表示中间轨迹的开始，并且对应于飞机必须退出第一飞行轨迹的点，以便达到预定的初始点 飞行条件和使用转换点的方式（13A，13B）来帮助飞机在第一和第二飞行轨迹之间的引导。

公开(公告)号：US20050258979A1

公开(公告)日：2005-11-24

申请号：US11123175

申请日：2005-05-06

Applicant: Franck Artini ,  Edward Strongman

Inventor： Franck Artini ,  Edward Strongman

IPC: G01C5/00 ,  G01C21/00 ,  G05D1/00 ,  G05D1/06 ,  G08B23/00

CPC classification number: G05D1/0646 ,  G01C5/005

Abstract: Method and device for determining a safe altitude for an aircraft. The device (1) includes means (2) for determining a clear zone corresponding to a lateral area dependent on the flight of the aircraft, means for determining the highest altitude of the ground that is located under this clear zone, and means (8) for determining a safe altitude, by calculating the sum of said highest altitude and a guard height.

Abstract translation: 用于确定飞机安全高度的方法和装置。 装置（1）包括用于确定对应于取决于飞行器的飞行的横向区域的清除区域的装置（2），用于确定位于该清除区域下的地面的最高高度的装置，以及装置（8） 通过计算所述最高高度和防护高度的总和来确定安全高度。