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
121	Method and apparatus for creating and updating maintenance plans of an aircraft	US10854632	2004-05-27	US20050187739A1	2005-08-25	Christian Baust; Ferenc Peter; Marek Poleda
An aircraft maintenance monitoring system is provided. The maintenance system monitors the operator's compliance with various technical and safety requirements imposed by various entities such as regulatory agencies, manufacturers, operators, and the like. The maintenance monitoring system provides a data structure that configures various technical objects and maintenance tasks in a hierarchical tree using object links. Such a data structure provides dynamics and flexibility to the aircraft maintenance monitoring system. This, in turn, allows updates to be automatically incorporated to the existing maintenance plans and maintenance schedule without any duplicate operations.
122	Method and apparatus for correlating flight identification data with secondary surveillance radar data	US10744898	2003-12-24	USRE39829E1	2007-09-11	Alexander E. Smith; Bennett Cohen; Carl Evers
A system for correlating secondary surveillance radar (SSR) data and ACARS data which results in a real time correlation of data which are unique to the separate existing systems. More specifically, a method is provided to attach flight identification data from ACARS signals to real time SSR data from Mode S transponders. Aircraft Mode S addresses are decoded and then converted to aircraft registration numbers using an algorithm or lookup table. Registration numbers are then correlated with registration numbers from decoded ACARS signals. The result is a real-time system which may provide an aircraft's registration information, including registration number, owner, make, and model, as well as its current flight identification number, and ACARS messages. As part of an aircraft multilateration system, the system provides an independent air traffic control picture complete with aircraft position and identification by flight number without the use of active radar equipment.
123	Method and apparatus for correlating flight identification data with secondary surveillance	US09466127	1999-12-21	US06384783B1	2002-05-07	Alexander E. Smith; Bennett Cohen; Carl Evers
A system for correlating secondary surveillance radar (SSR) data and ACARS data which results in a real time correlation of data which are unique to the separate existing systems. More specifically, a method is provided to attach flight identification data from ACARS signals to real time SSR data from Mode S transponders. Aircraft Mode S addresses are decoded and then converted to aircraft registration numbers using an algorithm or lookup table. Registration numbers are then correlated with registration numbers from decoded ACARS signals. The result is a real-time system which may provide an aircraft's registration information, including registration number, owner, make, and model, as well as its current flight identification number, and ACARS messages. As part of an aircraft multilateration system, the system provides an independent air traffic control picture complete with aircraft position and identification by flight number without the use of active radar equipment.
124	Method and apparatus for correlating flight identification data with secondary surveillance radar data	US09953560	2001-09-17	US06448929B1	2002-09-10	Alexander E. Smith; Bennett Cohen; Carl Evers
A system for correlating secondary surveillance radar (SSR) data and ACARS data which results in a real time correlation of data which are unique to the separate existing systems. More specifically, a method is provided to attach flight identification data from ACARS signals to real time SSR data from Mode S transponders. Aircraft Mode S addresses are decoded and then converted to aircraft registration numbers using an algorithm or lookup table. Registration numbers are then correlated with registration numbers from decoded ACARS signals. The result is a real-time system which may provide an aircraft's registration information, including registration number, owner, make, and model, as well as its current flight identification number, and ACARS messages. As part of an aircraft multilateration system, the system provides an independent air traffic control picture complete with aircraft position and identification by flight number without the use of active radar equipment.
125	METHOD AND APPARATUS FOR CORRELATING FLIGHT IDENTIFICATION DATA WITH SECONDARY SURVEILIANCE RADAR DATA	US09953560	2001-09-17	US20020130814A1	2002-09-19	Alexander E. Smith; Bennett Cohen; Carl Evers
A system for correlating secondary surveillance radar (SSR) data and ACARS data which results in a real time correlation of data which are unique to the separate existing systems. More specifically, a method is provided to attach flight identification data from ACARS signals to real time SSR data from Mode S transponders. Aircraft Mode S addresses are decoded and then converted to aircraft registration numbers using an algorithm or lookup table. Registration numbers are then correlated with registration numbers from decoded ACARS signals. The result is a real-time system which may provide an aircraft's registration information, including registration number, owner, make, and model, as well as its current flight identification number, and ACARS messages. As part of an aircraft multilateration system, the system provides an independent air traffic control picture complete with aircraft position and identification by flight number without the use of active radar equipment.
126	MOTOR VEHICLE LIGHT SYNCHRONIZATION SYSTEM	PCT/US2012/000098	2012-02-21	WO2012112231A2	2012-08-23	OBERHOLTZER, Steven, L.
A synchronization system for motor vehicles which enable external blinking or flashing lights of one or a number of vehicles to be synchronized. Among a group of motor vehicle, such as those produced by a given motor vehicle manufacturer, when the operators of the vehicles activate the turn signals or emergency flashers, they blink in unison with one another. External timing signals are used to establish the phasing of the flashing or blinking oscillations. Applications for emergency vehicles and aircraft are also disclosed.
127	적어도 하나의 터빈 엔진이 제공된 항공기의 터빈 엔진의 건강 검사를 수행하기 위한 방법 및 장치	KR1020130013619	2013-02-06	KR1020130090850A	2013-08-14	까미,엠마뉘엘; 볼췌괘도
PURPOSE: A method and apparatus for inspecting the health of at least one turbine engine in an aircraft are provided to establish a stability reference for not manually but automatically implementing health inspection. CONSTITUTION: A method for automatically inspecting the health of at least one turbine engine in an aircraft includes: a step (STP3) of obtaining at least one monitoring parameter for the turbine engine; and a step (STP4) of evaluating the health of the turbine engine. The method determines whether or not the aircraft flies in a level forward direction. A method for verifying the stability of the monitoring parameter includes: a step of obtaining at least one measuring signal from one of the monitoring parameters due to sampling regulated by a manufacturer; a step of implementing a first filtering for each signal with a high-pass filter for a long first duration, and then verifying whether or not a first amplitude of the filtered signal excesses a first critical value regulated by the manufacturer; and a step of implementing a second filtering for each signal with the high-pass filter for a second duration shorter than the first duration together with the first filtering by the high-pass filter, and then verifying whether or not a second amplitude of the filtered signal smaller than the first amplitude excesses a second critical value regulated by the manufacturer.
128	MOTOR VEHICLE LIGHT SYNCHRONIZATION SYSTEM	PCT/US2012000098	2012-02-21	WO2012112231A3	2013-01-03	OBERHOLTZER STEVEN L
A synchronization system for motor vehicles which enable external blinking or flashing lights of one or a number of vehicles to be synchronized. Among a group of motor vehicle, such as those produced by a given motor vehicle manufacturer, when the operators of the vehicles activate the turn signals or emergency flashers, they blink in unison with one another. External timing signals are used to establish the phasing of the flashing or blinking oscillations. Applications for emergency vehicles and aircraft are also disclosed.
129	Amphibious Large Aircraft Without Airstairs	US13146966	2010-03-01	US20110284683A1	2011-11-24	Shiying Liu
An amphibious large aircraft without airstairs is provided. The fuselage (7) of the amphibious large aircraft is flat, and the shape of its bottom is rectangular. The longitudinal cross-section of the fuselage has a shape of the cross-section of a win, so the lift can be generated by the fuselage during flight, and the flight efficiency is increased by 30-40%. The fuselage has only one floor, wherein the passenger cabin (6) is set in the front of the fuselage, and the cargo hold (21) is mounted above the rear. The wings (8) are suspended towards two sides from upper side of the fuselage. A jet engine (30) is mounted above the rear of the fuselage and adjacent to the tail wing. Because landing gears (4, 9) can be lifted vertically and the landing gear wells (3, 10) mounted in the fuselage are provided with fore-and-aft sliding doors (32, 33), the fuselage can stop close to the ground. It is no need for the passenger to go on and off the aircraft via the airstairs and escape from the aircraft via the inflator slide in en emergency. It can be more convenient for the cargo to enter or exit the aircraft when the aircraft is used as a freight aircraft. Because the fuselage is flat, the gliding capability and the ground effect of the aircraft are better, and the aircraft can takeoff, land and cruise on the wide water. The full-length, wingspan and height of the aircraft are all reduced by 25-30% compared with the current aircraft of the same scale, thus the floor space and the investment of the manufacturer, the maintenance factory, the garage and the aerodrome are all reduced.
130	Aircraft traffic display	US13351079	2012-01-16	US08736465B2	2014-05-27	Steve M. Rutherford; Dennis Polischuk
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.
131	AIRCRAFT TRAFFIC DISPLAY	US13351079	2012-01-16	US20120182161A1	2012-07-19	Steve M. Rutherford; Dennis Polischuk
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.
132	AIRCRAFT GALLEY	US13432965	2012-03-28	US20120285335A1	2012-11-15	Craig CUNNINGHAM; Sebastien A. RAMUS; Sebastian PETRY; Christopher I. PIRIE; Michiel BLAAUWHOF
An aircraft galley includes a beverage center including one or more hot beverage makers, and one or more combination oven-chiller units for multiple replaceable meal carrier rotables. The beverage center may also include an espresso maker, a milk frothing device, a hot water dispenser, a pull out drip tray, drain pan or sink, and a control panel. The aircraft galley also includes a main work deck with a sliding, pull-out work deck portion, and may include one or more pull-out combination drain-sink drawers including one or more individual drain-sinks.
133	Various-energy storing cycle-combined engine	JP2012160069	2012-07-19	JP2014020291A	2014-02-03	TANIGAWA HIROYASU; TANIGAWA KAZUNAGA
PROBLEM TO BE SOLVED: To improve the existing steam turbine power generation which is equipped with one half of static blades near a 0-output power, so that the steam speed is reduced to 1/10 and the volume is made 43,000 times as large as that of the maximum speed water by damming the steam speed.SOLUTION: The electric power generation is improved by one tenth or less by having one half of stationary vanes of a 0-output with a light steam velocity damming plus a light electric power generation. All dynamic blades are doubly reversed with gears of a horizontal axis 1h to generate a water gravity acceleration power generation in a vacuum of 30 mmHg. For mach 30, 100 sets of water injection turbines are combined. For a power generation amount of 100 times as high as the existing one and a 0 bearing load, a solar heater of an inexpensive electric drive such as a fuel cost of 0 for a power generation cost price of one hundredth is manufactured into a heat supply facility 3D of electricity + liquid air + overheated steam. An automobile, a ship, an airplane or the like is driven by a liquid oxygen compression drive so that one tenth fuel cost and a ten-times speed are achieved at a volume compression power of 21/60000 of the air compression, to acquire a 1/10 fuel cost and a 10-time velocity. The airplane aims at 1/50 ten thousands for reaching the space so that it can fly to anywhere on the earth for one day. The application profit of all manufactures is made the best in the world forever.
134	EXPANDED AIRLINER CONFIGURED SYMMETRICALLY REAR TO FRONT OR REAR TO REAR	US14173165	2014-02-05	US20160009415A1	2016-01-14	Brian Lee Uitdenbogerd
Currently the world's largest airplane is Airbus A380, can carry 525 people in a normal three-class configuration. It can travel nonstop 15,700 kilometers (8,500 nmi; 9,800 mi), at a speed of Mach 0.85 (about 900 Km/h or 560 mph; 490 kn at cursing altitude). To carry twice as many passengers and fly the same distance with the similar performance or better can achieved by joining the two same types of airplanes in the rear to front, (FIG. 1), or rear to rear (FIG. 2), can have the equivalent or better effect, and have similar or better performance than keep on building larger, fatter, airplanes such as A380. For example, Airbus, A350 can carry 350 passengers in a three-class setting, if the two A350s are jointed, it can carry, 700 passengers instead of only 350. This will work on other makers with the two same types of large airplanes.
135	PARTS MANUFACTURING METHODS, SYSTEMS AND USES	PCT/CA2010/000918	2010-06-16	WO2010145018A1	2010-12-23	HARRISON, Arthur
A method for manufacturing a part selected from a plurality of part types is disclosed. The method involves the step of selecting, from a supply of workpieces, a workpiece of a type that is associated with the type of part selected, the workpiece having a void and a substantially annular outer surface. Using a lathe, the selected workpiece is machined into the selected part. The workpiece, during the machining step, is mounted to the lathe by a collet associated with the type of part selected. The collet is an expanding collet which, during machining, is received by the void and engages the workpiece in gripping relation. The part can be a bushing for an aircraft landing gear and the workpiece can be an oversized bushing. The method can be carried out at an aircraft repair facility and the oversized bushings can be procured from specialist fabricators.
136	Aéronef muni d'un cockpit à visibilité extérieure optimisée, et procédé	EP14000637.0	2014-02-24	EP2783987A3	2018-01-10	Baudry, Jean-Pierre; Certain, Nicolas
La présente invention concerne un aéronef muni d'un cockpit, ledit cockpit comprenant une verrière munie de surfaces transparentes fixées à des montants, un pupitre central et deux sièges disposés transversalement de part et d'autre du pupitre central. L'aéronef comporte au moins un support (31, 33) relié au pupitre central et au moins un moyen d'affichage pour afficher de multiples informations d'aide aux pilotage, chaque moyen d'affichage étant porté par au moins un support (31, 32, 33, 34) interposé entre un montant et une position théorique de l'oeil d'un passager assis sur un desdits deux sièges, chaque support (31, 32, 33, 34) masquant visuellement au moins partiellement un montant pour optimiser la visibilité, extérieure au cockpit, offerte à ce passager, la position théorique étant définie par le constructeur.
137	常溫起動及行駛期間污染物排放及濃度降低之測量	TW087119770	1998-11-30	TW455680B	2001-09-21	密嘉勒.帕羅席–安德萊森
本發明特別相關於汽車、船舶、飛機及柴油火車機車,污染物排放之控制。該控制系統可由製造商裝配在新車內亦可由駕駛人買後裝修時裝配在舊車內。污染物排放量低之車輛較難控制,蓋因基於若干理由,測量訊號起伏變化甚大。請參閱圖5,與其他運轉時段相較常溫起動期間之污染物排放量最高。該等車輛將裝一自動起動系統以確保監控不同參數時該車輛可實施最佳起動。在行駛期間,燃燒系統內導致若干人為故障,機載監控系統將確定污染物排放之增加量。若引擎內或廢氣後處理系統發生故障及大氣中污染物含量高時,在常溫起動期間,加裝一吸附系統可降低車輛之污染物排放量。為使吸附劑獲得再生,則將污染物脫附、引進燃燒室而燃燒。
138	Disc-shaped submersible aircraft	US422897	1995-04-17	US5653404A	1997-08-05	Gennady Ploshkin
An aircraft of disc-shaped configuration provides the capability of vertical take-off and landing; straight horizontal flight; and three-dimensional maneuverability in the air by means of a plurality of counter-rotating lifting rotors assembled of fixed pitch or of self-adjusting pitch aerofoil blade elements; and, submersibility of the aircraft in water is achieved by means of a marine propulsion module using two counter-rotating hydrofoil rotors for up or down thrust, and a tunneled conventional marine propeller for horizontal travel. The marine propulsion module is detachable for emergency and for use with the main frame aircraft of a variety of other detachable modules for different tasks and missions. Exceptionally adaptable for any existing power plant, including nuclear, it is best suited for the environment-friendly types, like integrated steam motor on hydrogen and oxygen burning. The simplicity of the design and its mechanical efficiency are combined with several novel safety features, while displaying an attractive technological continuity for any conventional aircraft manufacturer. The downstream of air from the lifting rotors utilized for maneuvering by a system of vanes positioned below the rotors.
139	SYSTEM AND METHOD FOR MITIGATING AND DIRECTING AN EXPLOSION ABOARD AN AIRCRAFT	US12908077	2010-10-20	US20110168004A1	2011-07-14	Douglas W. Henegar
A method and a portable inhibitor which will focus a blast from an improvised explosive device aboard a pressurized aircraft in flight by using current Federal Aviation Administration least risk bomb location (LRBL) procedures. The portable LRBL is created using a collection of inflatable cubes which interlock with one another. The cubes are made from a resilient inner bladder which is filled with halon gas or other such fire retardant gas. The outer shell is made from ballistic material such as Kevlar. The portable LRBL is stored in a deflated mode. In order for the device to be used, it must be inflated. Once inflated, the cubes will be assembled and placed at a pre-determined position on the aircraft. This location will vary depending on the type and manufacturer of the aircraft. Once the cubes are connected and stacked, the structure will provide multi layered protection to the aircraft and passengers. In addition to providing ballistic protection to the passengers, the LRBL will be filled with halon gas which is a fire retardant gas which will minimize any fireball that may be caused as a result of an explosion. The LRBL structure acts to focus the detonation of an IED in a specific direction which will blow open the door of an aircraft and the pressure inside the cabin will force the explosion outside.
140	COFFEE MAKER WATER HEATER	US14023891	2013-09-11	US20140069353A1	2014-03-13	Marcos Jimenez
Embodiments of the present invention provide improved heating methods for use in coffee makers and other beverage makers that use hot water for various beverages and other purposes. These improvements find particular use on-board aircraft or other passenger transport vehicles, where quick heating and reduced power consumption are particularly desirable and beneficial. Further embodiments also relate to improved water level sensing, improved water reservoirs, and improved carafe features.

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