-
31.发明申请公开(公告)号：US20170137132A1
公开(公告)日：2017-05-18
申请号：US14942946
申请日：2015-11-16
Applicant: CESSNA AIRCRAFT COMPANY
Inventor： ROBERT GLYNN WIEGERS , DARREL DUANE HORNBAKER
IPC: B64D13/06
CPC classification number: B64D13/06 , B64D2013/0618
Abstract: An Environmental Control System (ECS) for aircraft is provided. The ECS includes a heat exchanger (HX) and an air conditioning unit (ACU) upstream of the heat exchanger. The heat exchanger receives flows of hot air bled from a plurality of aircraft engines and flows of cold ambient air drawn from the aircraft exterior for use by the heat exchanger and ACU for heating and cooling the interior cabin of the aircraft. The ECS may operate in one of several modes, whether the heat exchanger and air conditioning unit are operating normally or have failed. In a normal mode, the ACU and heat exchanger operate in series. In an “ACU only” mode, the ACU operates without the heat exchanger. In an “HX only” mode, the heat exchanger operates without the ACU. In an “ECS off” mode, both the heat exchanger and ACU are bypassed.
-
公开(公告)号：US09637225B1
公开(公告)日：2017-05-02
申请号：US14942943
申请日：2015-11-16
Applicant: CESSNA AIRCRAFT COMPANY
Inventor： Thomas Dean Zickuhr
IPC: B64C23/06
CPC classification number: B64C23/065 , B64C23/069 , Y02T50/164
Abstract: Embodiments of the present invention relate to a winglet for an end or tip of an aircraft wing. The winglet includes an inner portion that curves upward having a large radius of curvature near the wing, a middle portion having a small radius of curvature forming a bend, and an outer portion having a large radius of curvature extending to a tip of the winglet. The winglet lowers induced drag of the wing and improves aircraft performance especially for wing tip extensions that extend upwards about equal to or slightly more than outwards.
-
公开(公告)号：US20170021749A1
公开(公告)日：2017-01-26
申请号：US15218806
申请日：2016-07-25
Applicant: Cessna Aircraft Company
Inventor： Barry John Ward , Prasannakomar Shriram Bohnge , Dave Michael Kuhn , Dave Wayne Davis
IPC: B60N2/46
Abstract: An articulating armrest includes a first protrusion and a second protrusion that protrude from a member a predetermined spacing apart. Each protrusion aligns within a separate track within a housing configured for stowing the armrest within a seat back. The two tracks include straight and curved portions configured to articulate the armrest. Specifically, the armrest moves along a curvilinear path between stowed and deployed positions by translating along the tracks and pivoting about the second protrusion. The armrest may stow in a seat back and beneath the seat bottom to provide a full length armrest when deployed, and the armrest may stow flush with the seat back for sitting against. Mechanical tension may be provided to automatically deploy the armrest, and a rotational damper and a gas spring may be used to control the speed at which the armrest deploys.
Abstract translation: 铰接扶手包括第一突起和从构件以预定间隔分开地突出的第二突起。 每个突起在构造成用于将扶手放置在座椅靠背内的壳体内的单独轨道内对齐。 两个轨道包括被配置为铰接扶手的直的和弯曲的部分。 具体来说，扶手通过沿着轨道平移并围绕第二突起枢转沿着收起位置和展开位置之间的曲线路径移动。 扶手可以放置在座椅靠背和座椅底部下方，以在展开时提供全长扶手，扶手可以与座椅靠背齐平地坐在一起。 可以提供机械张力以自动地部署扶手，并且可以使用旋转阻尼器和气弹簧来控制扶手部署的速度。
-
公开(公告)号：US20160201941A1
公开(公告)日：2016-07-14
申请号：US15074468
申请日：2016-03-18
Applicant: CESSNA AIRCRAFT COMPANY
Inventor： DANIEL W. HODGES , NALLUSAMY PARAMAN , ROBERT FERENC
CPC classification number: B64D13/06 , B23P6/00 , B64D2013/0644 , B64D2013/0662 , F24F13/22 , F24F2013/227 , F25D21/00 , F25D21/14 , F25D2321/00 , F25D2321/14 , Y02T50/56 , Y10T29/49721
Abstract: A method for retrofitting an aircraft air conditioning unit drainage system comprises the step of removing drain pipe from the unit housing. A hole from which the drain pipe extends is plugged. A first location within a unit housing is determined where during operation of the unit air pressure is lower than at a second location. A second location below the first location is also determined where pooling occurs. A first and a second conduit with first and second internal diameters are respectively located at the first and the second locations. The first conduit and the second conduit are connected to a third conduit which extends generally vertically and which has a third internal diameter that is generally equal to the first internal diameter. A fourth conduit with a fourth internal diameter that is less than the second internal diameter is connected to the third conduit below the second location.
Abstract translation: 一种用于改装飞机空调机排水系统的方法，包括从单元壳体上移除排水管的步骤。 排水管延伸的孔被堵塞。 确定单元壳体内的第一位置，其中在单元空气压力的操作期间比在第二位置低。 在第一个位置下方的第二个位置也被确定在哪里发生池。 具有第一和第二内径的第一和第二导管分别位于第一和第二位置。 第一导管和第二导管连接到大致垂直延伸的第三导管，其具有大致等于第一内径的第三内径。 具有小于第二内径的第四内径的第四导管连接到位于第二位置下方的第三导管。
-
公开(公告)号：US09322570B2
公开(公告)日：2016-04-26
申请号：US13664026
申请日：2012-10-30
Applicant: Cessna Aircraft Company
Inventor： Daniel W. Hodges , Nallusamy Paraman , Robert Ferenc
CPC classification number: B64D13/06 , B23P6/00 , B64D2013/0644 , B64D2013/0662 , F24F13/22 , F24F2013/227 , F25D21/00 , F25D21/14 , F25D2321/00 , F25D2321/14 , Y02T50/56 , Y10T29/49721
Abstract: A system and method for removing condensate from an air conditioning unit is disclosed. A conduit includes an outlet portion that is connected to a chamber of a housing of the unit at a first location, and an inlet portion that is connected to the chamber at a second location where condensate accumulates. A gravitational separator portion which extends below the second location is connected to the outlet portion and the inlet portion. A draining portion having an orifice for allowing condensate to exit the conduit is connected to the gravitational separator portion below the second location. The first location is chosen such that during operation of the unit the pressure at the first location is less than the pressure at the second location.
Abstract translation: 公开了一种用于从空调单元去除冷凝物的系统和方法。 导管包括出口部分，其在第一位置处连接到单元的壳体的室，以及入口部分，其在冷凝物积聚的第二位置处连接到室。 在第二位置下方延伸的重力分离器部分连接到出口部分和入口部分。 具有用于允许冷凝物离开导管的孔的排出部分连接到第二位置下方的重力分离器部分。 选择第一位置使得在单元的操作期间，第一位置处的压力小于第二位置处的压力。
-
Patent Agency Ranking
公开(公告)号：US20160027312A1
公开(公告)日：2016-01-28
申请号：US14643492
申请日：2015-03-10
Applicant: Cessna Aircraft Company
Inventor： Jeremy Joseph Kneuper , John Robert Lanier
IPC: G08G5/00
CPC classification number: G08G5/0047 , G01C23/005 , G06F3/0481 , G06F3/04817 , G06F3/04847 , G08G5/0004 , G08G5/0008 , G08G5/0021 , G08G5/0052 , G08G5/0078 , G08G5/025
Abstract: Systems, methods and computer-storage media are provided for use of navigational aids. Three-dimensional graphical representations of flight plans, flight paths, waypoints, etc., may be displayed to improve situational awareness. Additionally, dynamic monitoring of airports, waypoints, traffic, etc., may be performed so that real-time updates are available to users. The real-time updates will not only include updated location information and any relevant navigational markers (e.g., updated waypoints, new traffic, etc.) but will also include detailed information related to the navigational markers such as a distance from the marker, an airspeed of the marker (if applicable), and the like.
Abstract translation: 提供系统，方法和计算机存储介质，用于导航辅助。 可以显示飞行计划，飞行路线，航点等的三维图形表示，以提高情境意识。 此外，可以执行机场，航点，交通等的动态监控，以便用户可以实时更新。 实时更新不仅包括更新的位置信息和任何相关的导航标记（例如，更新的航点，新的交通等），还将包括与导航标记相关的详细信息，例如距离标记的距离，空速 的标记（如果适用）等。
-
公开(公告)号：US20150356873A1
公开(公告)日：2015-12-10
申请号：US14643464
申请日：2015-03-10
Applicant: Cessna Aircraft Company
Inventor： Jeremy Joseph Kneuper , John Robert Lanier , Jason Michael Decker
IPC: G08G5/00
CPC classification number: G08G5/0047 , B64D43/02 , B64D47/08 , G01C23/00 , G06F3/03547 , G06F3/041 , G06F3/04817 , G06F3/0482 , G06F3/0484 , G06F3/0485 , G06F3/04883 , G06F2203/04806 , G06T11/206 , G06T2200/24 , G08G5/0021 , G08G5/0034 , G08G5/0039 , G08G5/0052 , G08G5/0065 , G08G5/0091 , G08G5/025 , G09B29/003
Abstract: The invention described herein provides a flight crew with an easier, more intuitive, system and method to create a flight plan. A flight planning system is presented for navigation of an aircraft utilizing a touch screen display device mounted in an aircraft cockpit spanning the width and height of the instrument panel. The system provides navigational views, an interactive map, charts, a radio frequency component, a weather component, and a virtual flight plan. A flight planning method is presented that uses an interactive map on a touch screen device in an aircraft cockpit. The method accepts user inputs and displays a desired flight plan on the map. A method for providing a chart on a touch screen device is presented that includes presenting a list of menu options on a touch screen mounted in an aircraft cockpit. The method provides the flight crew with heads-up operation, providing greater situational awareness.
Abstract translation: 本文所述的发明为飞行机组提供了一种更简单，更直观的系统和方法来创建飞行计划。 飞行计划系统被提供用于使用安装在跨越仪表板的宽度和高度的飞行器驾驶舱中的触摸屏显示装置的飞机导航。 该系统提供导航视图，交互式地图，图表，射频分量，天气分量和虚拟飞行计划。 提出了一种在飞机驾驶舱中使用触摸屏设备上的交互式地图的飞行计划方法。 该方法接受用户输入并在地图上显示所需的飞行计划。 提供了一种用于在触摸屏设备上提供图表的方法，其包括在安装在飞行器驾驶舱中的触摸屏上呈现菜单选项的列表。 该方法为飞行机组人员提供单机操作，提供更大的情境意识。
-
公开(公告)号：US09193439B2
公开(公告)日：2015-11-24
申请号：US14195419
申请日：2014-03-03
Applicant: Cessna Aircraft Company
Inventor： Steven G. Hagerott , Stephen Eddy , Jeremy Phillip Taylor
Abstract: An improved flight control system is described, providing for increased or reduced pilot input forces necessary to cause desired control surface deflections.
Abstract translation: 描述了改进的飞行控制系统，其提供增加或减少导致所需控制表面偏转所必需的先导输入力。
-
公开(公告)号：US09051062B1
公开(公告)日：2015-06-09
申请号：US13763427
申请日：2013-02-08
Applicant: Cessna Aircraft Company
Inventor： Richard Boone , Benjamin De Putter
CPC classification number: B64F5/0009 , B29C65/02 , B29C65/483 , B29C65/7841 , B29C66/112 , B29C66/131 , B29C66/524 , B29C66/532 , B29C66/5326 , B29C66/61 , B29C66/721 , B29C66/7212 , B29C66/73751 , B29C66/73753 , B29C66/73754 , B29C66/73941 , B29D99/0014 , B29L2031/3082 , B64C1/061 , B64C1/064 , B64C1/069 , B64C1/12 , B64C2001/0072 , B64F5/10 , Y02T50/43 , B29K2307/04 , B29K2309/08
Abstract: A method for making a fuselage section comprises the steps of assembling a support system. The support system comprises fiber reinforced composite material and includes at least three frames and six stringers. The support system is partially cured via a fast cure process such that the support system attains about eighty percent of its fully cured strength. A skin comprising uncured fiber reinforced composite material is globally positioned such that an inner surface of the skin corresponds to an outer surface of the support system. The skin and the support system are fully cured together. The support system is assembled on a bonding tool having a bonding surface corresponding to an inner surface of the skin.
Abstract translation: 一种用于制造机身部分的方法包括组装支撑系统的步骤。 支撑系统包括纤维增强复合材料，并且包括至少三个框架和六个桁条。 支撑系统通过快速固化工艺部分固化，使得支撑体系达到其完全固化强度的约百分之八十。 包含未固化纤维增强复合材料的皮肤是全局定位的，使得皮肤的内表面对应于支撑体系的外表面。 皮肤和支撑系统完全固化在一起。 支撑系统组装在具有对应于皮肤内表面的粘合表面的粘合工具上。
-
公开(公告)号：US09050757B1
公开(公告)日：2015-06-09
申请号：US13763584
申请日：2013-02-08
Applicant: Cessna Aircraft Company
Inventor： Richard Boone , Benjamin De Putter
CPC classification number: B29C70/34 , B29C70/44 , B32B37/10 , Y10T156/10
Abstract: An internally heated and pressurized system for fabricating a composite laminate structure and method for use thereof is disclosed. One of a plurality of thin, thermally conductive bond tools, prepreg fiber reinforced composite layers, and a pressure applying membrane are nested within a heated base, and then covered by a pressure sealed cover. The system is pressurized through the pressure sealed cover. The pressure causes the pressure applying membrane to force the prepreg fiber reinforced composite layers onto the upper surface of the bond tool. The heated base transfers heat to the composite layers via the bond tool, which heats and cures the composite layers together and to a shape determined by the upper surface of the bond tool. Each bond tool is formed with a generic lower surface for nesting within the heated base and an upper surface for forming composite layers into the shape of a specific part.
Abstract translation: 公开了用于制造复合层压结构的内部加热和加压系统及其使用方法。 多个薄导热粘合工具，预浸料纤维增强复合层和压力施加膜中的一个嵌套在加热的基底内，然后被压力密封的盖覆盖。 系统通过压力密封盖加压。 压力导致压力施加膜将预浸料纤维增强复合层强制到粘结工具的上表面上。 加热的基座通过粘合工具将热量传递到复合层，该粘合工具将复合层加热并固化在一起并且由粘结工具的上表面确定的形状。 每个焊接工具形成有用于嵌套在加热的基底内的通用下表面和用于将复合层形成为特定部分的形状的上表面。
-
-
-
-
-
-
-
-
-
Search Results
90
records
(took 0.034 seconds)
