Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
09/2014
09/30/2014US8844262 Exhaust for a gas turbine engine
09/30/2014CA2621837C Aircraft engine oil removal system
09/25/2014WO2014151275A1 Nacelle mounted latching system
09/25/2014WO2014150500A1 Nacelle internal and external flow control
09/25/2014DE102012021155B4 Elektroantriebsbaueinheit Elektroantriebsbaueinheit
09/25/2014DE102011015126B4 Flugzeugheckbereich mit einem in dem Flugzeugheckbereich installierten Kühlsystem Aircraft tail region with a cooling system installed in the aircraft tail region
09/23/2014US8840059 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
09/23/2014US8839805 Passive boundary layer bleed system for nacelle inlet airflow control
09/18/2014WO2014143264A1 Engine inlet total air temperature sensor
09/18/2014US20140271169 Nacelle for a high bypass ratio engine with multiple flow paths
09/18/2014US20140263853 Methods Utilizing Cold Spray Techniques for Repairing and Protecting Rotary Components of Aviation Propulsion Systems
09/18/2014US20140260187 Aircraft supplemental thrust device and method of operating the same
09/18/2014US20140260127 Interchangeable inlet protection systems for air intakes of aircraft engines and related method
09/18/2014US20140259947 Engine cowl and inlet cover
09/17/2014EP2776319A1 Composite panel having a built-in sampling scoop
09/16/2014US8834108 Running-gap control system of an aircraft gas turbine
09/14/2014CA2845185A1 Engine starting system using stored energy
09/12/2014WO2014135844A1 Laminated heat exchanger including a heat sink and a thermoelectric device
09/11/2014US20140252167 Reverse core engine thrust reverser for under wing
09/11/2014CA2845161A1 Lubrication oil system for a reduction gearbox
09/10/2014EP2775250A1 Laminated heat exchanger including a heat sink and a thermoelectric device
09/09/2014US8826641 Thermal management system integrated pylon
09/05/2014CA2836709A1 Micro-lattice cross-flow heat exchangers for aircraft
09/02/2014US8820344 Turbojet engine nacelle
09/02/2014US8819937 Auxiliary power unit inlet duct screen assembly
08/2014
08/27/2014EP2768600A2 Filter systems for air intakes of aircraft engines and related methods
08/26/2014CA2659944C Mixed carbon foam/metallic heat exchanger
08/22/2014CA2843075A1 Exhaust section for bypass gas turbine engines
08/21/2014WO2014127213A1 Package and method for filling to limit bricking
08/21/2014DE102013202616A1 Vorrichtung zum Reinigen der Core Engine eines Strahltriebwerks Device for cleaning the core engine of a jet engine
08/19/2014CA2585879C Exhaust assembly for propulsion gases in an aircraft with twist elbow
08/13/2014CN103987624A 用于涡轮发动机机舱的进气口结构 Air intake structure for the turbine engine nacelle
08/13/2014CN103979111A 飞机碎鸟网罩刀 Aircraft broken bird nets knife
08/13/2014CA2841420A1 Brushless alternator for helicopter transmission install
08/12/2014US8800258 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
08/12/2014CA2842327A1 Method for predicting faults in an aircraft thrust reverser system
08/07/2014US20140216088 Aircraft thermal management system for cooling using expendable coolants
08/07/2014US20140215999 Aft exhaust system for rotary wing aircraft
08/06/2014EP2762408A1 Bi-directional ventilation systems for use with aircraft and related methods
08/06/2014EP2760741A1 Lip unit for an electrically deiced turbojet engine nacelle
08/06/2014CN203753413U 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
08/06/2014CN103975142A 安装用凸台以及风扇壳 Attachment boss and the fan case
08/06/2014CN103963996A 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
08/06/2014CN102483169B 具有指引的飞行器流体止回阀组件 Aircraft fluid check valve assembly having guidelines
08/05/2014CA2731205C Personal flight device incorporating radiator cooling passage
08/05/2014CA2720521C 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
07/2014
07/31/2014WO2014099088A3 Environmental defense shield
07/31/2014WO2014086329A3 Intake for an engine of an aircraft
07/31/2014WO2014077922A3 Nacelle scoop inlet
07/31/2014WO2014055152A3 Bifurcated inlet scoop for gas turbine engine
07/31/2014CA2833881A1 Bi-directional ventilation systems for use with aircraft and related methods
07/30/2014CN103958350A 具有内置取样收集器的复合面板 Has built-in sampling a composite panel of the collector
07/30/2014CN103958349A 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
07/30/2014CN103958347A 用于冷却飞行器机翼的系统和方法 System and method for cooling an aircraft wing
07/30/2014CN103950544A 通用亚声速扩压器设计方法 General subsonic diffuser design methods
07/30/2014CN103950543A 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
07/30/2014CN103950542A 减阻风头 Drag Reduction limelight
07/29/2014US8790079 Ram air turbine inlet
07/24/2014WO2014113444A2 Aircraft supplemental thrust device and method of operating the same
07/24/2014US20140203630 Oil level indicator for rotary wing aircraft transmission
07/23/2014CN103935524A 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
07/23/2014CA2831524A1 Dual door fan air modulating valve
07/22/2014US8783412 Sound absorber for a gas turbine exhaust cone, and method for the production thereof
07/22/2014US8782896 Method for the manufacture of an ejector nozzle tube
07/22/2014CA2548138C Methods and apparatus for operating gas turbine engines
07/17/2014WO2014066508A3 Unducted thrust producing system architecture
07/17/2014DE202012012963U1 Elektroantriebsbaueinheit Elektroantriebsbaueinheit
07/16/2014CN103925060A 小型无人直升机水冷动力装置 Small unmanned helicopter water-cooled power plant
07/16/2014CN102428004B 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
07/16/2014CN101903244B 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
07/15/2014US8777154 Apparatus and method for preventing gas turbine engine freezing
07/15/2014CA2628440C Method and system for taxiing an aircraft
07/10/2014WO2014106725A1 Electric de-icing device for turbojet engine nacelle
07/09/2014CN103912418A 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
07/09/2014CN102307783B 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
07/08/2014US8770512 Passive control of ice shedding
07/08/2014CA2585920C Exhaust assembly forming a horizontal elbow for propulsion gases in an aircraft
07/08/2014CA2585878C Exhaust assembly for propulsion gases in an aircraft forming an elbow
07/03/2014WO2014102682A1 Nacelle for aircraft, provided with a built-in system for anti-icing protection and acoustic absorption
07/03/2014US20140182697 Adjustable supersonic air inlet
07/02/2014CN203681872U 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
07/01/2014US8765070 System and method for rejecting heat from equipment via endothermic isomerization
06/2014
06/26/2014WO2014099182A1 Apu exhaust housing perforated ring
06/26/2014US20140179535 Electric drive device for an aircraft
06/26/2014DE102011056826B4 Schallschutzvorrichtung und damit versehenes Triebwerk und Verfahren zur Bereitstellung The sound insulation device and thus provided the engine and method for providing
06/26/2014DE102009061028B4 Flugzeugkühlsystem und Verfahren zum Betreiben eines Flugzeugkühlsystems Aircraft cooling system, and method for operating an aircraft cooling system
06/25/2014CN203666966U 带可动边条的鸭式飞翼布局飞机 With movable edge of the flying wing canard aircraft
06/24/2014US8757540 Nacelle inlet lip
06/19/2014WO2014092757A1 Asymmetric thrust reversers
06/18/2014EP2743178A1 An air inlet combining a filter and a bypass device for use with a turbine engine
06/18/2014CN102131705B Nacelle with a variable nozzle section
06/18/2014CA2835584A1 Gas turbine engine mounting ring
06/12/2014US20140158833 Air inlet combining a filter and a bypass device for use with a turbine engine
06/11/2014EP2739530A1 Aircraft propulsion architecture integrating an energy recovery system
06/11/2014CN101903241B Ice protection system for a multi-segment aircraft component
06/05/2014US20140150649 System for supplying an aircraft with inert gas, method for supplying an aircraft with inert gas, use of a membrance and aircraft
06/05/2014DE102012023718A1 Einlauf für ein Triebwerk eines Luftfahrzeugs Inlet for an engine of an aircraft
06/04/2014EP2737933A1 Inlet particle separator system with air injection
06/04/2014CN203623970U 复合材料整体进气道 Composite overall inlet
06/04/2014CN103832594A Aircraft nacelle comprising a deformable connection between an air intake and a power plant
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