Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926) |
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09/30/2014 | US8844262 Exhaust for a gas turbine engine |
09/30/2014 | CA2621837C Aircraft engine oil removal system |
09/25/2014 | WO2014151275A1 Nacelle mounted latching system |
09/25/2014 | WO2014150500A1 Nacelle internal and external flow control |
09/25/2014 | DE102012021155B4 Elektroantriebsbaueinheit Elektroantriebsbaueinheit |
09/25/2014 | DE102011015126B4 Flugzeugheckbereich mit einem in dem Flugzeugheckbereich installierten Kühlsystem Aircraft tail region with a cooling system installed in the aircraft tail region |
09/23/2014 | US8840059 Assembly of components connected by a device that maintains the integrity of the surface of one of the components |
09/23/2014 | US8839805 Passive boundary layer bleed system for nacelle inlet airflow control |
09/18/2014 | WO2014143264A1 Engine inlet total air temperature sensor |
09/18/2014 | US20140271169 Nacelle for a high bypass ratio engine with multiple flow paths |
09/18/2014 | US20140263853 Methods Utilizing Cold Spray Techniques for Repairing and Protecting Rotary Components of Aviation Propulsion Systems |
09/18/2014 | US20140260187 Aircraft supplemental thrust device and method of operating the same |
09/18/2014 | US20140260127 Interchangeable inlet protection systems for air intakes of aircraft engines and related method |
09/18/2014 | US20140259947 Engine cowl and inlet cover |
09/17/2014 | EP2776319A1 Composite panel having a built-in sampling scoop |
09/16/2014 | US8834108 Running-gap control system of an aircraft gas turbine |
09/14/2014 | CA2845185A1 Engine starting system using stored energy |
09/12/2014 | WO2014135844A1 Laminated heat exchanger including a heat sink and a thermoelectric device |
09/11/2014 | US20140252167 Reverse core engine thrust reverser for under wing |
09/11/2014 | CA2845161A1 Lubrication oil system for a reduction gearbox |
09/10/2014 | EP2775250A1 Laminated heat exchanger including a heat sink and a thermoelectric device |
09/09/2014 | US8826641 Thermal management system integrated pylon |
09/05/2014 | CA2836709A1 Micro-lattice cross-flow heat exchangers for aircraft |
09/02/2014 | US8820344 Turbojet engine nacelle |
09/02/2014 | US8819937 Auxiliary power unit inlet duct screen assembly |
08/27/2014 | EP2768600A2 Filter systems for air intakes of aircraft engines and related methods |
08/26/2014 | CA2659944C Mixed carbon foam/metallic heat exchanger |
08/22/2014 | CA2843075A1 Exhaust section for bypass gas turbine engines |
08/21/2014 | WO2014127213A1 Package and method for filling to limit bricking |
08/21/2014 | DE102013202616A1 Vorrichtung zum Reinigen der Core Engine eines Strahltriebwerks Device for cleaning the core engine of a jet engine |
08/19/2014 | CA2585879C Exhaust assembly for propulsion gases in an aircraft with twist elbow |
08/13/2014 | CN103987624A 用于涡轮发动机机舱的进气口结构 Air intake structure for the turbine engine nacelle |
08/13/2014 | CN103979111A 飞机碎鸟网罩刀 Aircraft broken bird nets knife |
08/13/2014 | CA2841420A1 Brushless alternator for helicopter transmission install |
08/12/2014 | US8800258 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure |
08/12/2014 | CA2842327A1 Method for predicting faults in an aircraft thrust reverser system |
08/07/2014 | US20140216088 Aircraft thermal management system for cooling using expendable coolants |
08/07/2014 | US20140215999 Aft exhaust system for rotary wing aircraft |
08/06/2014 | EP2762408A1 Bi-directional ventilation systems for use with aircraft and related methods |
08/06/2014 | EP2760741A1 Lip unit for an electrically deiced turbojet engine nacelle |
08/06/2014 | CN203753413U 一种航空发动机进口整流帽罩的防冰传热结构 An anti-icing heat transfer structure aeroengine import cap of rectification |
08/06/2014 | CN103975142A 安装用凸台以及风扇壳 Attachment boss and the fan case |
08/06/2014 | CN103963996A 横向压力梯度可控的乘波前体与进气道一体化设计方法 Front transverse pressure gradient controlled Waverider body and inlet integrated design methods |
08/06/2014 | CN102483169B 具有指引的飞行器流体止回阀组件 Aircraft fluid check valve assembly having guidelines |
08/05/2014 | CA2731205C Personal flight device incorporating radiator cooling passage |
08/05/2014 | CA2720521C Air inlet of an aircraft turbine engine, aircraft equipped with such an air inlet and process for optimizing the operation of an aircraft turbine engine through an air inlet |
07/31/2014 | WO2014099088A3 Environmental defense shield |
07/31/2014 | WO2014086329A3 Intake for an engine of an aircraft |
07/31/2014 | WO2014077922A3 Nacelle scoop inlet |
07/31/2014 | WO2014055152A3 Bifurcated inlet scoop for gas turbine engine |
07/31/2014 | CA2833881A1 Bi-directional ventilation systems for use with aircraft and related methods |
07/30/2014 | CN103958350A 具有内置取样收集器的复合面板 Has built-in sampling a composite panel of the collector |
07/30/2014 | CN103958349A 用于特别地具有一体式环形后部的飞机涡轮发动机舱的致动器 For aircraft turbine engines in particular having an integral annular compartment rear actuator |
07/30/2014 | CN103958347A 用于冷却飞行器机翼的系统和方法 System and method for cooling an aircraft wing |
07/30/2014 | CN103950544A 通用亚声速扩压器设计方法 General subsonic diffuser design methods |
07/30/2014 | CN103950543A 一种具有可变放气系统的飞行器超声速进气道 Having a variable bleed system aircraft supersonic inlet |
07/30/2014 | CN103950542A 减阻风头 Drag Reduction limelight |
07/29/2014 | US8790079 Ram air turbine inlet |
07/24/2014 | WO2014113444A2 Aircraft supplemental thrust device and method of operating the same |
07/24/2014 | US20140203630 Oil level indicator for rotary wing aircraft transmission |
07/23/2014 | CN103935524A 一种内部融合辅助进气道的高性能亚声速进气道 An internal integration of the auxiliary inlet performance subsonic inlet |
07/23/2014 | CA2831524A1 Dual door fan air modulating valve |
07/22/2014 | US8783412 Sound absorber for a gas turbine exhaust cone, and method for the production thereof |
07/22/2014 | US8782896 Method for the manufacture of an ejector nozzle tube |
07/22/2014 | CA2548138C Methods and apparatus for operating gas turbine engines |
07/17/2014 | WO2014066508A3 Unducted thrust producing system architecture |
07/17/2014 | DE202012012963U1 Elektroantriebsbaueinheit Elektroantriebsbaueinheit |
07/16/2014 | CN103925060A 小型无人直升机水冷动力装置 Small unmanned helicopter water-cooled power plant |
07/16/2014 | CN102428004B 用于飞机冷却系统的冷却器、飞机冷却系统和飞机冷却系统的操作方法 Cooler operation method for an aircraft cooling system, the aircraft cooling system, the aircraft cooling system and |
07/16/2014 | CN101903244B 用于冷却将从航空器排放的热气的装置 Means for cooling the hot gases from aircraft emissions for |
07/15/2014 | US8777154 Apparatus and method for preventing gas turbine engine freezing |
07/15/2014 | CA2628440C Method and system for taxiing an aircraft |
07/10/2014 | WO2014106725A1 Electric de-icing device for turbojet engine nacelle |
07/09/2014 | CN103912418A 一种具有新型空气滤清器的增程式无人机 Program by having a new air filter UAV |
07/09/2014 | CN102307783B 特别适宜于飞行器发动机舱空气入口的声学处理用的面板 Particularly suitable for an aircraft engine compartment air inlet acoustic panels processing |
07/08/2014 | US8770512 Passive control of ice shedding |
07/08/2014 | CA2585920C Exhaust assembly forming a horizontal elbow for propulsion gases in an aircraft |
07/08/2014 | CA2585878C Exhaust assembly for propulsion gases in an aircraft forming an elbow |
07/03/2014 | WO2014102682A1 Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption |
07/03/2014 | US20140182697 Adjustable supersonic air inlet |
07/02/2014 | CN203681872U 一种用于飞机辅助动力系统的排气及通风冷却装置 Exhaust and ventilation cooling system for an aircraft auxiliary power systems |
07/01/2014 | US8765070 System and method for rejecting heat from equipment via endothermic isomerization |
06/26/2014 | WO2014099182A1 Apu exhaust housing perforated ring |
06/26/2014 | US20140179535 Electric drive device for an aircraft |
06/26/2014 | DE102011056826B4 Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung The sound insulation device and thus provided the engine and method for providing |
06/26/2014 | DE102009061028B4 Flugzeugkühlsystem und Verfahren zum Betreiben eines Flugzeugkühlsystems Aircraft cooling system, and method for operating an aircraft cooling system |
06/25/2014 | CN203666966U 带可动边条的鸭式飞翼布局飞机 With movable edge of the flying wing canard aircraft |
06/24/2014 | US8757540 Nacelle inlet lip |
06/19/2014 | WO2014092757A1 Asymmetric thrust reversers |
06/18/2014 | EP2743178A1 An air inlet combining a filter and a bypass device for use with a turbine engine |
06/18/2014 | CN102131705B Nacelle with a variable nozzle section |
06/18/2014 | CA2835584A1 Gas turbine engine mounting ring |
06/12/2014 | US20140158833 Air inlet combining a filter and a bypass device for use with a turbine engine |
06/11/2014 | EP2739530A1 Aircraft propulsion architecture integrating an energy recovery system |
06/11/2014 | CN101903241B Ice protection system for a multi-segment aircraft component |
06/05/2014 | US20140150649 System for supplying an aircraft with inert gas, method for supplying an aircraft with inert gas, use of a membrance and aircraft |
06/05/2014 | DE102012023718A1 Einlauf für ein Triebwerk eines Luftfahrzeugs Inlet for an engine of an aircraft |
06/04/2014 | EP2737933A1 Inlet particle separator system with air injection |
06/04/2014 | CN203623970U 复合材料整体进气道 Composite overall inlet |
06/04/2014 | CN103832594A Aircraft nacelle comprising a deformable connection between an air intake and a power plant |