Patents
Sitemap › B64 - Aircraft; Aviation; Cosmonautics › B64D - Equipment for fitting in or to aircraft; Flying suits; Parachutes; Arrangements or mounting of power plants or propulsion transmissions › B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
06/2014
06/03/2014US8740135 Auxiliary power unit inlet
05/2014
05/30/2014WO2013166419A9 Mounting system for a nacelle fire detection system
05/29/2014US20140147270 Aircraft Nacelle Comprising A Reinforced Connection Between An Air Intake And A Means Of Propulsion
05/28/2014CN103826971A 用于电除冰的涡轮喷气发动机机舱的唇缘组件 Turbojet engine nacelle for electric deicing lip assembly
05/28/2014CA2833758A1 Aircraft gearbox gaseous cooling system
05/27/2014US8733694 Arrangement for maintaining flow to an air inlet of an auxiliary power unit assembly
05/27/2014CA2581827C Low noise exhaust ducting system
05/22/2014WO2014077922A2 Nacelle scoop inlet
05/22/2014US20140140871 Power plant, an application of such a power plant and a method of operating such a power plant
05/21/2014CN102105358B 用于在飞机中供应周围空气的空气管道 For the supply of ambient air in the aircraft air duct
05/20/2014US8727267 Variable contraction ratio nacelle assembly for a gas turbine engine
05/15/2014WO2014074144A1 Clocked thrust reversers
05/15/2014WO2014074143A1 Aircraft with forward sweeping t-tail
05/15/2014WO2014072615A1 Aircraft propelled by a turbojet engine with contrarotating fans
05/15/2014US20140131515 Aircraft turbojet engine thrust reverser with a reduced number of latches
05/14/2014EP2730507A2 Methods for directing cooling flow into the surge plenum of an exhaust eductor cooling system
05/14/2014CN103786890A 能悬停的飞行器 The aircraft can hover
05/14/2014CN103786889A 一种能避免鸟撞飞机发动机的装置 One kind of bird strike can be avoided aircraft engine unit
05/14/2014CA2833050A1 Passive cooling of transmission using mast mounted heat pipes
05/08/2014WO2014068261A1 Turbomachine casing
05/07/2014CN203581388U 高超声速飞行器与进气道内外乘波一体化装置 Hypersonic vehicle and integration of devices inside and outside the inlet Waverider
05/07/2014CN103770946A 用于使能悬停的飞行器的传动装置冷却的系统和方法 System and method for enabling transmission of hovering aircraft cooled
05/07/2014CN103770929A 一种具有网格加强筋的飞机整体壁板结构 A kind of grid reinforcement of the overall structure of the aircraft panel
05/06/2014US8714477 Turbomachine support pylon for aircraft
04/2014
04/30/2014EP2724940A2 Turboshaft engine having improved inlet particle scavenge systems and method for the manufacture thereof
04/30/2014DE102012021155A1 Elektroantriebsbaueinheit Elektroantriebsbaueinheit
04/30/2014CN103754374A Engine radiating mechanism for unmanned aerial vehicles
04/30/2014CA2822240A1 Methods and apparatus for sealing variable area fan nozzles of jet engines
04/26/2014CA2828643A1 Helicopter gearbox auxiliary cooling system
04/23/2014CN203558213U Disassembling device for boundary layer of airplane air intake duct
04/23/2014CN103748337A Adjustable supersonic air inlet
04/22/2014CA2551306C Helicopter with an auxiliary lubricating circuit
04/16/2014EP2719621A2 Aft exhaust system for rotary wing aircraft
04/16/2014EP2719620A2 Upturned exhaust system for rotary wing aircraft
04/16/2014EP2719619A2 Rotary wing aircraft having collocated exhaust duct and propeller shaft
04/16/2014CN203544375U Outboard motor radiator for agricultural helicopter
04/16/2014CN102124197B Inner wall for the nacelle of a turbine engine
04/15/2014CA2554385C One-piece baffle infrared suppressor apparatus and method
04/10/2014US20140096501 Upturned exhaust system for rotary wing aircraft
04/09/2014EP2715094A1 A structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section
04/09/2014EP2714519A1 Air inlet structure for turbojet engine nacelle
04/08/2014US8690098 Air ejector nozzle tube for an oil heat exchanger of an aircraft engine
04/08/2014US8690097 Variable-geometry rotating spiral cone engine inlet compression system and method
04/08/2014CA2587068C Power and control system for electrical equipment of an aircraft engine or its environment
04/03/2014WO2014052061A1 Turbomachine thrust reverser
04/02/2014EP2712805A1 System and method for cooling a hover-capable aircraft transmission
04/01/2014US8685302 Monolithic acoustically-treated composite structures and methods for fabricating the same
04/01/2014US8685126 Device for filtering the intake air of an internal combustion engine having ventilation means
04/01/2014US8684301 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle
04/01/2014CA2554151C Infrared suppressor apparatus and method
03/2014
03/27/2014US20140084107 Flexible and fireproof APU drainage device
03/27/2014US20140084080 Infrared Suppressing Exhaust System
03/27/2014US20140083518 Structural element of an air vehicle air intake composed of an array of passages with a hexagonal cross section
03/27/2014DE102012217469A1 Kühlsystem für Komponenten in (Luft-)Fahrzeugstrukturen Cooling system components (air) vehicle structures
03/26/2014CN203497182U Reinforcement propelling plant of volute air cushion
03/26/2014CN203497181U Silencer plate structure for air inlet area of aircraft engine
03/26/2014CN103662087A Hypersonic aerocraft and air inlet internal and external waverider integrated design method
03/26/2014CN103661953A Heat exchanger system and method for controlling airflow cooling
03/26/2014CN102483170B Fluid pipeline structure and fluid check valve assembly
03/25/2014CA2756214C Jet engine nozzle exit configurations and associated systems and methods
03/20/2014WO2014042857A2 Metallic sandwich structure having small bend radius
03/20/2014WO2014041297A1 Method for mounting an acoustic panel in a housing of a turbomachine and turbomachine comprising an acoustic panel
03/20/2014WO2013121139A3 Device for supplying air to an auxiliary power unit of an aircraft and associated aircraft
03/19/2014CN103648909A Leading edge structure, in particular for an air inlet of an aircraft engine nacelle
03/13/2014WO2014037650A1 Accessory drive gearbox for controlling the flaps of an aircraft
03/13/2014US20140072400 Serpentine Cooling of Nozzle Endwall
03/12/2014CN203473243U Flow guide equipment of large civil airplane
03/12/2014CN103625646A Air door for air inlet channel of APU (Auxiliary Power Unit)
03/12/2014CN102099556B Air intake structure for turbojet engine nacelle with pneumatic de-icing
03/12/2014CA2826419A1 Mounting device and method of assembling the same
03/05/2014EP2703624A1 Adjustable supersonic air inlet
03/04/2014US8662453 Relating to air-breathing flight vehicles
02/2014
02/27/2014US20140053532 Nacelle scoop inlet
02/19/2014CN203439266U An aircraft thermal management system guaranteeing reliable fuel supply for an engine
02/19/2014CN203439265U Aircraft heat management system improving heat dissipation performance
02/19/2014CN103587705A Unmanned helicopter with engine radiating cover
02/19/2014CN103587704A Combined subsonic air intake device of aircraft
02/19/2014CN103587703A Ram outlet header
02/19/2014CN102417036B Multifunctional high-speed sailing aircraft
02/18/2014US8651415 Engine cowl and inlet cover
02/18/2014US8650853 Noise reduction assembly for aircraft turbojet
02/06/2014WO2014020267A1 Helicopter engine air intake with improved bypass flow
02/05/2014EP2691304A2 Airborne cooling system
02/05/2014CN203419261U Integrated acoustic-treatment composite structure
02/05/2014CN103562068A Air inlet structure for turbojet engine nacelle
02/04/2014US8640986 Turbojet nacelle and method for controlling separation in a turbojet nacelle
01/2014
01/29/2014EP2690018A2 Hybrid hinge and latch beam
01/29/2014EP2688801A1 Aircraft tail region with a cooling system installed in aircraft tail region
01/29/2014EP2688707A1 Method of inspecting impacts observed in fan casings
01/29/2014EP2034159B1 Active flow control for nacelle air intake
01/29/2014CN103538727A Method for designing pneumatic layout of axial-symmetry air-breathing hypersonic aircraft
01/29/2014CN102056803B Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
01/29/2014CN101952171B Aircraft propulsion assembly comprising hot air bleed systems
01/29/2014CN101784444B Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
01/28/2014US8636051 Free air stream heat exchanger design
01/23/2014WO2014014072A1 Unmanned helicopter
01/22/2014CN103523235A Aircraft engine compartment air inlet flue fairing
01/22/2014CN102448822B Aircraft engine nacelle comprising a mobile cowl moved by electric motors
01/15/2014CN103507961A Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
01/13/2014CA2819942A1 Aircraft ice protection system and method
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