| 序号 | 专利名 | 申请号 | 申请日 | 公开（公告）号 | 公开（公告）日 | 发明人 |
|---|---|---|---|---|---|---|
| 61 | 民航客机驾驶舱电子飞行包支架 | CN201730506677.7 | 2017-10-23 | CN304576071S | 2018-04-10 | 范抗抗; 杨铖; 朱岳清 |
| 1．本外观设计产品的名称：民航客机驾驶舱电子飞行包支架。 2．本外观设计产品的用途：本外观设计产品用于民航客机驾驶舱电子飞行包（EFB）所用载体平板电脑（PAD）的安装与固定。 3．本外观设计产品的设计要点：产品的形状。 4．最能表明本外观设计设计要点的图片或照片：立体图。 5．本外观设计产品由A套件（安装托盘）和B套件（阻尼转轴）组成。 | ||||||
| 62 | 平板电脑（二级电子飞行包EFB） | CN201630094524.1 | 2016-03-28 | CN303978577S | 2016-12-21 | 李敏; 王伟 |
| 1.本外观设计产品的名称：平板电脑（二级电子飞行包EFB）； 2．本外观设计产品的用途：用作平板电脑； 3．本外观设计的设计要点：产品的形状； 4．最能表明设计要点的图片或者照片：立体图1。 | ||||||
| 63 | CIRCUIT ÉLECTRONIQUE ET CAPTEUR DE TEMPS DE VOL COMPRENANT UN TEL CIRCUIT ÉLECTRONIQUE | PCT/EP2017/073512 | 2017-09-18 | WO2018050897A1 | 2018-03-22 | COUILLAULT, Jérôme; GRATZL, Peter |
Un circuit électronique comprend au moins un élément émetteur de rayonnement (2), un régulateur de courant (12) avec une borne de production de courant (O), et un élément de mesure (14) produisant un signal (Vmes) représentatif du courant le traversant. Un interrupteur (6) est commandé par un signal de modulation (M) de manière à successivement ouvrir et fermer un chemin électrique passant par la borne de production de courant (O), l'élément émetteur de rayonnement (2) et l'élément de mesure (14). Un circuit de conversion (16) est par ailleurs interposé entre l'élément de mesure (14) et le régulateur de courant (12) de manière à transformer le signal représentatif (Vmes) en un signal lissé (S) destiné à une borne de régulation (Reg). Un capteur de temps de vol comprenant un tel circuit électronique est également proposé. |
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| 64 | ELECTRONIC FLIGHT BAG MOUNTING BRACKET | EP10706855.3 | 2010-02-25 | EP2401199A1 | 2012-01-04 | DEBUHR, Merritte; BITANT, Jeffrey; RICHARDS, Daniel |
| A mounting bracket for an electronic flight bag (EFB) includes a frame having a track and a mounting assembly that is having a base and a support that is moveably connected to the base and can be selectively fixed in position on the track. The mounting bracket may allow for singlehanded adjustment of the position of the mounting assembly with respect to track at one of at least two discrete locations along the track, or at any desired position along the track. Further, the mounting bracket may provide a single mechanism for both securing the EFB to the mounting assembly and orienting the support with respect to the base. | ||||||
| 65 | Power supply system for an electronic flight bag | EP12175015.2 | 2012-07-04 | EP2543973A2 | 2013-01-09 | Haukom, Michael; Horsager, Thomas; Willenbring, Brett |
A control system for providing electrical power to an electronic flight bag device on an aircraft. The control system including a power switching component coupled to a plurality of power sources and at least one electronic flight bag device. The power switching component is operative and configured to selectively apply electrical power from at least one of the plurality of power sources to the at least one electronic flight bag device based upon a condition of the aircraft.
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| 66 | Next generation electronic flight bag | EP09177675.7 | 2009-12-01 | EP2196775A3 | 2012-06-27 | Pandit, Anil Kumar; Rao, Srikanth; Rao, Nayyar Azam Khan; Bhat, Nagaraj Sham |
An electronic flight bag (100) for an aircraft includes a display device (102) and a processing system (104). The display device (102) is operable to render various images. The processing system (104) is in operable communication with the display. The processing system (104) is configured to receive various types of data from various aircraft systems and is operable, upon receipt of the data, to supply display commands to the display device (102) that cause the display device (102) to automatically render various images. These images may include, among other things, flight manual pages, checklists, approach charts, maintenance data, and various navigation displays. The electronic flight bag (100) may also implement the functions of various other aircraft systems and devices.
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| 67 | Next generation electronic flight bag | EP09177675.7 | 2009-12-01 | EP2196775A2 | 2010-06-16 | Pandit, Anil Kumar; Rao, Srikanth; Rao, Nayyar Azam Khan; Bhat, Nagaraj Sham |
An electronic flight bag (100) for an aircraft includes a display device (102) and a processing system (104). The display device (102) is operable to render various images. The processing system (104) is in operable communication with the display. The processing system (104) is configured to receive various types of data from various aircraft systems and is operable, upon receipt of the data, to supply display commands to the display device (102) that cause the display device (102) to automatically render various images. These images may include, among other things, flight manual pages, checklists, approach charts, maintenance data, and various navigation displays. The electronic flight bag (100) may also implement the functions of various other aircraft systems and devices.
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| 68 | Next generation electronic flight bag | EP15160625.8 | 2009-12-01 | EP2921826A1 | 2015-09-23 | Pandit, Anil Kumar; Rao, Srikanth; Rao, Nayyar Azam Khan; Bhat, Nagaraj Sham |
An electronic flight bag (100) for an aircraft includes a display device (102) and a processing system (104). The display device (102) is operable to render various images. The processing system (104) is in operable communication with the display. The processing system (104) is configured to receive various types of data from various aircraft systems and is operable, upon receipt of the data, to supply display commands to the display device (102) that cause the display device (102) to automatically render various images. These images may include, among other things, flight manual pages, checklists, approach charts, maintenance data, and various navigation displays. The electronic flight bag (100) may also implement the functions of various other aircraft systems and devices.
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| 69 | Power supply system for an electronic flight bag | EP12175015.2 | 2012-07-04 | EP2543973A3 | 2014-01-08 | Haukom, Michael; Horsager, Thomas; Willenbring, Brett |
A control system for providing electrical power to an electronic flight bag device on an aircraft. The control system including a power switching component coupled to a plurality of power sources and at least one electronic flight bag device. The power switching component is operative and configured to selectively apply electrical power from at least one of the plurality of power sources to the at least one electronic flight bag device based upon a condition of the aircraft.
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| 70 | POWER SUPPLY SYSTEM FOR AN ELECTRONIC FLIGHT BAG | US15136589 | 2016-04-22 | US20160239064A1 | 2016-08-18 | Michael Haukom; Thomas J. Horsager; Brett Willenbring |
| A control system for providing electrical power to an electronic flight bag device on an aircraft. The control system including a power switching component coupled to a plurality of power sources and at least one electronic flight bag device. The power switching component is operative and configured to selectively apply electrical power from at least one of the plurality of power sources to the at least one electronic flight bag device based upon a condition of the aircraft. | ||||||
| 71 | Electronic flight bag mounting bracket | US12392275 | 2009-02-25 | US08308114B2 | 2012-11-13 | Merritte DeBuhr; Jeffrey Bitant; Daniel Richards |
| A mounting bracket for an electronic flight bag (EFB) includes a frame having a track and a mounting assembly that is having a base and a support that is moveably connected to the base and can be selectively fixed in position on the track. The mounting bracket may allow for singlehanded adjustment of the position of the mounting assembly with respect to track at one of at least two discrete locations along the track, or at any desired position along the track. Further, the mounting bracket may provide a single mechanism for both securing the EFB to the mounting assembly and orienting the support with respect to the base. | ||||||
| 72 | Electronic Flight Bag Mounting System | US12576780 | 2009-10-09 | US20110084106A1 | 2011-04-14 | Jayson K. Bopp; Sarah L. Palmer |
| According to one embodiment, an electronic flight bag mounting system a cockpit mounting member coupled to an electronic flight bag mounting member. The cockpit mounting member is configured to mount to a cockpit of an aircraft, while the electronic flight bag mounting member is configured to be coupled to an electronic flight bag. The electronic flight bag mounting member is movable from a deployed position in which a display of the electronic flight bag faces a cockpit seat configured in the cockpit to a storage position in which the electronic flight bag faces away from the cockpit seat. | ||||||
| 73 | NEXT GENERATION ELECTRONIC FLIGHT BAG | US12333946 | 2008-12-12 | US20100152924A1 | 2010-06-17 | Anil Kumar Pandit; Srikanth Rao; Nayyar Azam Khan Rao; Nagaraj Sham Bhat |
| An electronic flight bag for an aircraft includes a display device and a processing system. The display device is operable to render various images. The processing system is in operable communication with the display. The processing system is configured to receive various types of data from various aircraft systems and is operable, upon receipt of the data, to supply display commands to the display device that cause the display device to automatically render various images. These images may include, among other things, flight manual pages, checklists, approach charts, maintenance data, and various navigation displays. The electronic flight bag may also implement the functions of various other aircraft systems and devices. | ||||||
| 74 | ELECTRONIC FLIGHT BAG SYSTEM AND METHOD | US11679486 | 2007-02-27 | US20080208399A1 | 2008-08-28 | Tuan A. Pham |
| An electronic flight bag (EFB) system for use on a mobile platform, for example, a commercial or military aircraft. The EFB system includes first and second independent processors that run first and second independent software applications. The first software application may be a Type C application requiring a high level of governmental agency certification for use on an aircraft while the second application may be a commercially available, off-the-shelf software application that requires no certification. The two processors share a common display, although the first processor is provided with control over the display so that use of the display by the second processor can be inhibited or limited by the first processor as may be needed to display more critical flight or aircraft related information. The first processor is also provided with control over a switching subsystem that can interrupt the flow of information from external I/O devices to and from the second processor, if needed. | ||||||
| 75 | Electronic flight bag system and method | US11679486 | 2007-02-27 | US08751067B2 | 2014-06-10 | Tuan A. Pham |
| An electronic flight bag (EFB) system for use on a mobile platform, for example, a commercial or military aircraft. The EFB system includes first and second independent processors that run first and second independent software applications. The first software application may be a Type C application requiring a high level of governmental agency certification for use on an aircraft while the second application may be a commercially available, off-the-shelf software application that requires no certification. The two processors share a common display, although the first processor is provided with control over the display so that use of the display by the second processor can be inhibited or limited by the first processor as may be needed to display more critical flight or aircraft related information. The first processor is also provided with control over a switching subsystem that can interrupt the flow of information from external I/O devices to and from the second processor, if needed. | ||||||
| 76 | Electronic flight bag mounting system | US12576780 | 2009-10-09 | US08701953B2 | 2014-04-22 | Jayson K. Bopp; Sarah L. Palmer |
| According to one embodiment, an electronic flight bag mounting system a cockpit mounting member coupled to an electronic flight bag mounting member. The cockpit mounting member is configured to mount to a cockpit of an aircraft, while the electronic flight bag mounting member is configured to be coupled to an electronic flight bag. The electronic flight bag mounting member is movable from a deployed position in which a display of the electronic flight bag faces a cockpit seat configured in the cockpit to a storage position in which the electronic flight bag faces away from the cockpit seat. | ||||||
| 77 | Methods and devices for forced air cooling of electronic flight bags | EP10006593.7 | 2010-06-24 | EP2275901A3 | 2015-09-16 | Wicks, Curtis |
An electronic flight bag computer (EFB) includes a housing defining first and second compartments that are fluidly isolated from and in thermal communication with one another. The first compartment contains electronic components connected to a user interface on an exterior portion of the housing for providing interactive flight related computation functions to a user. The second compartment contains a forced convection cooling component in thermal communication with the electronic components. The forced convection cooling component directs a flow of cooling fluid into the second compartment to convey heat produced by the electronic components out of the housing, such that the cooling fluid in the second compartment remains fluidly isolated from the electronic components in the first compartment of the housing.
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| 78 | SINGLE PROCESSOR CLASS-3 ELECTRONIC FLIGHT BAG | EP11709520.8 | 2011-02-23 | EP2539818A1 | 2013-01-02 | SHULER, Jason; SCHAAF, Jonathan; LINDGREN, Andrew; FEDKE, Micah; SCHOTZ, Peter; OWCZARSKI, David; GUPTA, Ram; CHERNYAKOVA, Liya; ZOBACHEV, Eugene; HOLUPCHINSKI, Nicholas; CHULA, Stephen; HUNGERFORD, Matthew; HERING, Jeffrey; JONES, David; NEWMAN, Bernard; LEHSTEN, John |
| An electronic flight bag providing computational services for an aircraft and communicating with aircraft avionics may execute aircraft-design-approved Type-C applications together with non-design-approved Type-A/B on a single processor through specific modifications of the operating system to control memory and processor access thereby providing isolation comparable to that of dual processor systems in which the Type-C applications and Type-A/B applications are executed on different processors. | ||||||
| 79 | Methods and devices for forced air cooling of electronic flight bags | EP10006593.7 | 2010-06-24 | EP2275901A2 | 2011-01-19 | Wicks, Curtis |
An electronic flight bag computer (EFB) includes a housing defining first and second compartments that are fluidly isolated from and in thermal communication with one another. The first compartment contains electronic components connected to a user interface on an exterior portion of the housing for providing interactive flight related computation functions to a user. The second compartment contains a forced convection cooling component in thermal communication with the electronic components. The forced convection cooling component directs a flow of cooling fluid into the second compartment to convey heat produced by the electronic components out of the housing, such that the cooling fluid in the second compartment remains fluidly isolated from the electronic components in the first compartment of the housing.
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| 80 | Single processor class-3 electronic flight bag | US13120372 | 2011-02-23 | US09223633B2 | 2015-12-29 | Jason Shuler; Jonathan Schaaf; Andrew Lindgren; Micah Fedke; Peter Schotz; David Owczarski; Ram Gupta; Liya Chernyakova; Eugene Zobachev; Nicholas Holupchinski; Stephen Chula; Matthew Hungerford; Jeffrey Hering; David Jones; Bernard Newman; John Lehsten |
| An electronic flight bag providing computational services for an aircraft and communicating with aircraft avionics may execute aircraft-design-approved Type-C applications together with non-design-approved Type-A/B on a single processor through specific modifications of the operating system to control memory and processor access thereby providing isolation comparable to that of dual processor systems in which the Type-C applications and Type-A/B applications are executed on different processors. | ||||||
