飞机制造商相关的专利数据

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
81	METHOD OF OPTIMIZING THE AVAILABILITY OF AN AIRCRAFT OR OF A FLEET OF AIRCRAFT	US12555345	2009-09-08	US20100063933A1	2010-03-11	Radhouane DJERIDI; Mathieu GLADE
The present invention provides a method of optimizing the operational availability of at least one aircraft or of a fleet of aircraft as a function of constraints associated with maintenance and with the use of said aircraft, the method consisting in: using a forecast maintenance plan for the aircraft; adapting the forecast maintenance plan in real time as a function of maintenance operations carried out and/or as a function of unexpected maintenance operations that result from malfunctions diagnosed in one or more of the pieces of equipment of the aircraft; and adapting the forecast maintenance plan continuously as a function of the actual use of the aircraft so as to provide the manufacturer, the operator, and the maintenance services with a maintenance plan that is forecast and dynamic.
82	Tandem seat for ultra light aircraft	US542403	1983-10-17	US4600170A	1986-07-15	Terry L. Smith
A tandem seat assembly for ultra light aircraft is disclosed which is interchangeable with a single seat configuration. The assembly, which is primarily used for pilot training, is fitted with dual aircraft controls. The single seat must be removable from an ultra light aircraft in order for the tandem seat assembly as described by this invention to be utilized. The tandem seat assembly is thereby placed in the aircraft such that the center of gravity of the seat assembly is near the nominal center of gravity of the aircraft. Universal attachments of the seat assembly to the aircraft frame allow the seat assembly to be used with a number of different manufacturers of ultra light aircraft models.
83	Method for checking the appropriateness of a mass value of an aircraft	US11854477	2007-09-12	US07584073B2	2009-09-01	François Coulmeau
A method for checking the appropriateness of an aircraft ground mass value Ms, communicated to a flight management system of the aircraft by a crew member of the aircraft or by an airline operating the aircraft, the communication taking place before a takeoff of the aircraft from a departure airport to a destination airport. The method includes two checking phases. A first direct appropriateness check, based on a cross-check of independent information related to the mass of the aircraft. A second indirect appropriateness check based on a comparison between values of performance parameters calculated on the basis of the mass value of the aircraft Ms and of the values of the same performance parameters provided by a manufacturer of the aircraft.
84	DIMENSIONALLY STABLE FABRIC	EP04815905	2004-12-29	EP1747257A4	2009-12-23	SCOTT DONALD E

85	Aircraft anti-hijacking system	US10081676	2002-02-22	US20030066929A1	2003-04-10	Gail Valencia; Herbert M. Valencia
This invention allows aircraft manufacturers, operators, and operators of other modes of transportation the ability to deny control of the conveyance to anyone attempting to hijack or otherwise intervene with operation of transport vehicles or facilities.
86	Common flight deck module for family of commercial aircraft	US09944967	2001-08-31	US06497388B1	2002-12-24	Michael G. Friend; Jay R. Huffington; Mark E. Eakins
A common flight deck module for use with a plurality of aircraft platforms. The common flight deck module includes a discrete structure that is independent of the structure of the aircraft fuselage and may includes an avionics system and other hardware, controls and equipment. The common flight deck module is configured to “plug into” the fuselage from each of the aircraft platforms. The “plug in” modularity of the common flight deck module permits the standardization of various components and procedures to thereby make possible efficiency-based cost reductions for both aircraft manufacturers and aircraft consumers.
87	Method and device for accessing the documentation of an aircraft according to alarms generated therein	US12879639	2010-09-10	US08712604B2	2014-04-29	Pierre Campagne; Jerome Treanton; Xavier Geay; Laval Louis Chan Kam Fai; Christophe Jotz; Thierry Paya-Arnaud; Jerome Pouyfaucon
A method and a device for accessing the documentation of an aircraft according to alarms generated therein, where the documentation includes at least one document that is modifiable independently of the manufacturer of the aircraft. After having received at least one indication relating to at least one alarm generated by the avionics of the aircraft, at least one datum relating to the at least one alarm, including a link to at least one element of the documentation, is extracted and displayed.
88	Remote aircraft manufacturing, monitoring, maintenance and management system	US10307818	2002-12-02	US20040106404A1	2004-06-03	Todd W. Gould; Steve R. Stovner; Richard J. Reuter; Stanley W. Engdahl; James M. Parker; Bryan P. Kesterson
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
89	Remote aircraft manufacturing, monitoring, maintenance and management system	US10307818	2002-12-02	US07636568B2	2009-12-22	Todd W. Gould; Steve R. Stovner; Richard J. Reuter; Stanely W. Engdahl; James M. Parker; Bryan P. Kesterson
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
90	Dimensionally Stable Fabric	US10584818	2004-12-29	US20070214843A1	2007-09-20	Donald Scott
A method of producing a dimensionally stable, fire-resistant fabric including the steps of spinning yarn from wool and fire-resistant synthetic fibers, weaving the yarn to form a fabric, and dimensionally stabilizing the fabric to produce a textile that passes aircraft manufacturer specifications.
91	Masking System for Coating Aircraft Components	US13301337	2011-11-21	US20130125812A1	2013-05-23	Jason E. Rayman; Richard W. Brown
The present invention relates to the application of surface coatings to treated aluminum articles utilized on aircraft, and more particularly to a system for masking portions of aluminum aircraft wheel and brake components for application of surface coatings to reduce or prevent wear and/or corrosion to the aluminum article. The system may be utilized for new aluminum aircraft components as well as aircraft components that have been subjected to non-destructive testing. The masking components are constructed and arranged to cooperate with portions of the aluminum component in a sequential manner to allow for application of multiple layers of primer and/or topcoat without removal of prior masking components so that a coated component complies with the manufacturer's written requirements for that component.
92	Dimensionally stable fabric	US10584818	2004-12-29	US07766054B2	2010-08-03	Donald E. Scott
A method of producing a dimensionally stable, fire-resistant fabric including the steps of spinning yarn from wool and fire-resistant synthetic fibers, weaving the yarn to form a fabric, and dimensionally stabilizing the fabric to produce a textile that passes aircraft manufacturer specifications.
93	Masking system for coating aircraft components	US13301337	2011-11-21	US08720369B2	2014-05-13	Jason E. Rayman; Richard W. Brown
The present invention relates to the application of surface coatings to treated aluminum articles utilized on aircraft, and more particularly to a system for masking portions of aluminum aircraft wheel and brake components for application of surface coatings to reduce or prevent wear and/or corrosion to the aluminum article. The system may be utilized for new aluminum aircraft components as well as aircraft components that have been subjected to non-destructive testing. The masking components are constructed and arranged to cooperate with portions of the aluminum component in a sequential manner to allow for application of multiple layers of primer and/or topcoat without removal of prior masking components so that a coated component complies with the manufacturer's written requirements for that component.
94	Remote aircraft manufacturing, monitoring, maintenance and management system	EP10186025.2	2003-11-27	EP2278494A2	2011-01-26	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can; perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.
95	不要登机梯的水陆两用大飞机	PCT/CN2010/070806	2010-03-01	WO2010099730A1	2010-09-10	刘世英

96	AIRCRAFT TRAFFIC DISPLAY	PCT/US2012/021469	2012-01-17	WO2012099835A2	2012-07-26	RUTHERFORD, Steve, M.; POLISCHUK, Dennis
A system and method for displaying additional traffic information beyond that received from an ADS-B or other transponder communication. Such additional traffic information may be displayed on a display screen within a cockpit, and may include such things as an aircraft's make, model, manufacturer, or other information. The additional information may be displayed as text, or one or more pictures, icons, or symbols that correspond to this additional information, or any combination of text and such items. The additional information may be determined from one or more databases that correlate information received in the transponder communication to the additional information that is not contained within the transponder communication.
97	Turbo-machine transport frame	US602368	1984-04-20	US4660796A	1987-04-28	Jean Garrec
In order to facilitate the operations of handling and of transportation when empty between the works of an engine manufacturer and the works of an aircraft manufacturer, a transportation framework is provided with support members which are adjustable. These members, on which the turbo-machine rests, are mounted pivotally on the platform. It is possible to cause them to be adapted so as to take up two positions; a higher position where they support the turbo machine and, a lower position where they are folded on to the platform. The vertical height of the frameworks is thus reduced when empty and enables them to be stacked.
98	AIRCRAFT TRAFFIC DISPLAY	PCT/US2012021469	2012-01-17	WO2012099835A3	2014-04-10	RUTHERFORD STEVE M; POLISCHUK DENNIS
A system and method for displaying additional traffic information beyond that received from an ADS-B or other transponder communication. Such additional traffic information may be displayed on a display screen within a cockpit, and may include such things as an aircraft's make, model, manufacturer, or other information. The additional information may be displayed as text, or one or more pictures, icons, or symbols that correspond to this additional information, or any combination of text and such items. The additional information may be determined from one or more databases that correlate information received in the transponder communication to the additional information that is not contained within the transponder communication.
99	Dna label	JP2004136845	2004-04-05	JP2005293531A	2005-10-20	GOUNAI SHIRO
<P>PROBLEM TO BE SOLVED: To provide a comparatively inexpensive method by which whole information of a product is obtained from the minute remaining of the product. <P>SOLUTION: DNA sequence mixed in components of the product and paint is read and incorporated product information is checked using an inspection method of the DNA sequence also from a part of the product by creating an identification number expressing information such as a production manufacturer, a brand name, a production line, a production period and a serial number, and mixing specific sequence of deoxyribonucleic acid (DNA) corresponding to the identification number one to one in components and paints of construction materials, vessels, aircraft, vehicles and home electronics, etc. <P>COPYRIGHT: (C)2006,JPO&NCIPI
100	Remote aircraft manufacturing, monitoring, maintenance and management system	EP03078744.4	2003-11-27	EP1426870A3	2004-09-29	Stovner, Steve R.; Gould, Todd W.; Reuter, Rick J.; Engdahl, Stanley W.; Parker, James M.
An aircraft wireless data communication system includes an aircraft computer/server in communication with a plurality of aircraft systems. Access to the aircraft systems via the computer/server is available in real-time via wireless communication with a ground-based computer system. The ground-based computer system includes a computer that can be accessed from one or more networks of computers. Each authorized computer user on an airline, manufacturer, or supplier network has remote real-time access to the aircraft computer/server. Properly authorized remote users can: perform comparisons between the aircraft actual configuration identity and an aircraft authorized configuration identity; perform system diagnostic testing; view system status and parameters; collaborate with users from local and remote organizations using real-time aircraft data; and upload and download software and data to and from aircraft systems.

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