Patents for B64D 27 - Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby (3,375)
12/2014
12/10/2014CN203996885U 内燃机动力多旋翼直升机 Combustion engine powered multi-rotor helicopter
12/10/2014CN104192308A 利用风能充电续航的滚翼飞行动力装置 Rechargeable battery life using wind power plant roll-wing flight
12/10/2014CN102689687B 一种平衡螺旋桨后气动旋转力矩的方法 After a balanced pneumatic rotary propeller torque method
12/10/2014CN102083690B 飞机滑行系统 Taxiing system
12/10/2014CN101903243B 用于飞行器辅助动力单元的具有弹性体构件的悬架系统 The suspension system for an aircraft auxiliary power unit having an elastomer member
12/09/2014US8905368 Helicopter engine mounting system and methods
12/09/2014US8904795 Noise reducing device and jet propulsion system
11/2014
11/27/2014US20140346283 Aircraft using turbo-electric hybrid propulsion system for multi-mode operation
11/25/2014US8894351 Retaining ring
11/20/2014US20140339357 System and method for cooling an aircraft wing
11/18/2014US8890343 Electric generator disposed on a rotating turboprop part
11/18/2014US8888038 Driven aircraft, in particular an aircraft designed as a flying wing and/or having a low radar signature
11/18/2014US8888037 Antivibration suspension means for a tie bar of an aircraft power transmission gearbox, an antivibration suspension device, and an aircraft
11/13/2014US20140331496 Intermediate structure for independently de-mountable propulsion components
11/11/2014US8882029 Fire resistant structural mount yoke and system
11/11/2014US8882027 Aircraft power plant, an aircraft, and a method of using a piston engine in a power plant having a conventional gearbox
11/11/2014US8881536 Aircraft engine assembly comprising a turbojet engine with reinforcing structures connecting the fan casing to the central casing
11/04/2014US8876043 Aircraft engine exhaust nozzle system for jet noise reduction
11/04/2014US8876042 Integrated nacelle assembly
10/2014
10/28/2014US8870114 Hybrid drive for helicopters
10/23/2014US20140312167 Ram Air Fan Mounting Bracket
10/21/2014US8864470 Unducted propeller with variable pitch blades for a turbomachine
10/21/2014US8864067 Auxiliary fire resistant mount system for an auxiliary power unit
10/21/2014US8864066 Rigid aircraft pylon fitted with a rib extension for taking up the moment in the lengthways direction
10/14/2014US8857761 Variable geometry aircraft pylon structure and related operation techniques
10/09/2014WO2014165502A1 Airborne kinetic energy conversion system
10/09/2014WO2014164586A1 Engine mounting system
10/09/2014WO2014163688A1 Aircraft power plant
10/09/2014US20140299708 Rocket or ballistic launch rotary wing vehicle
10/08/2014EP2785590A1 System and method for cooling an aircraft wing
10/07/2014US8851417 Self-retaining shear pin for blind mount location
10/02/2014WO2014158247A1 Generator for flight vehicle
10/02/2014WO2014154980A1 Ball-jointed device for suspending a turbomachine from a pylon or for suspending equipment from the body of the turbomachine.
09/2014
09/30/2014US8845292 Blade-retaining device for turbomachine propeller
09/30/2014US8845270 Rotor assembly
09/30/2014US8844862 Aft pylon fairing for aircraft engine suspension system, comprising a heat shield capable of expanding freely
09/30/2014US8844861 Aircraft propulsion system
09/30/2014US8844263 Aircraft turbine engine and use of such a turbine engine
09/25/2014US20140284419 Aircraft
09/25/2014DE102012021155B4 Elektroantriebsbaueinheit Elektroantriebsbaueinheit
09/23/2014US8841584 Electric deicing device for propfan-type propeller blades
09/23/2014US8840062 Pylon mounting system with vibration isolation
09/23/2014US8840061 Strut designed to support an aircraft turbojet engine, and nacelle comprising such a strut
09/23/2014US8839629 Assembly for attaching the hangers from which an aircraft propulsion unit is suspended
09/23/2014CA2571793C Active cancellation and vibration isolation with feedback and feedforward control for an aircraft engine mount
09/18/2014WO2014143451A1 Fire seal end cap and associated multi-member assembly and method
09/18/2014US20140263831 Cross-wing Twin-Fuselage Aircraft
09/18/2014US20140263825 Active Vibration Isolation System
09/18/2014US20140263820 Autorotative Enhancement System
09/18/2014DE102013102558A1 Rotorblatt und Verfahren zur Herstellung eines Rotorblatts The rotor blade and method of producing a rotor blade
09/17/2014EP2778068A2 Blade safety mechanism for open rotor engine system
09/17/2014EP2776318A1 Gas turbine engine with low stage count low pressure turbine
09/16/2014US8834119 Device with counter-rotating propellers having a propeller pitch altering means
09/12/2014WO2014135431A1 Propulsion nacelle for an airplane
09/11/2014US20140252161 De-couple geared turbo-fan engine and aircraft
09/11/2014US20140252160 Reverse flow gas turbine engine removable core
09/11/2014US20140252159 Engine installation
09/11/2014DE102013102194A1 Antriebseinrichtung für ein sich in einem Fluid bewegendes Fahrzeug Drive means for moving in a fluid vehicle
09/10/2014EP2774853A1 Drive nacelle for an airplane
09/10/2014EP2774852A2 Gas turbine engine installation
09/10/2014EP2774839A2 Improved impact resistant and damage tolerant aircraft fuselage
09/10/2014EP2773557A2 Turbo engine attachment pylon
09/09/2014US8827653 Unducted fan with variable-pitch blades for a turbine engine
09/09/2014US8827203 Connecting a propulsion system to a structural element of an aircraft
09/09/2014US8827199 Turboshaft engine supporting pylon covered with a porous material and turboshaft engine/pylon assembly
09/09/2014US8826641 Thermal management system integrated pylon
09/02/2014US8821118 Optimization of downstream open fan propeller position
09/02/2014US8820676 Airplane with pitch and yaw command by propulsion system
08/2014
08/26/2014US8814505 Mechanical arrangement
08/26/2014US8814080 Aerodynamic aft fairing of an aircraft engine suspension pylon
08/26/2014US8814079 Pylon for attaching an aircraft turbine engine comprising aligned front wing ties
08/21/2014US20140231582 Methods and Systems of Constructing a Multi Rotor Aircraft Fuselage
08/20/2014EP2766588A1 An aerodiesel engine
08/14/2014US20140224940 Propulsion system using large scale vortex generators for flow redistribution and supersonic aircraft equipped with the propulsion system
08/13/2014EP2764223A2 Aero compression combustion drive assembly control system
08/13/2014EP2763898A1 Aircraft propulsion assembly
08/13/2014EP2763897A1 Aircraft propulsion assembly
08/13/2014EP2763896A1 A multi-rotor unmanned aerial vehicle
08/12/2014US8800917 Aircraft engine pylon AFT aerodynamic fairing
08/12/2014US8800916 Device for attaching an aircraft engine, comprising blocks for clamping an engine attachment with a wedge effect
08/12/2014US8800299 Jet engine nacelle having dampers for half-shells
08/07/2014US20140217234 Aircraft propulsion assembly
08/07/2014US20140217233 Aircraft propulsion assembly
08/07/2014US20140217232 Mechanically optimized liquid inertia vibration eliminator and aircraft pylon system
08/06/2014CN203753398U 一种多轴飞行器 One kind of multi-axis aircraft
08/06/2014CN103963982A 一种带有电子分压系统的多电机飞行器 Multi-motor aircraft with an electronic system of partial pressure
08/05/2014US8798810 Energy protecting device for aircraft
08/05/2014US8794920 Controlling blade pitch angle
08/05/2014US8794568 Aircraft engine attachment pylon comprising two front wing system attachments with orthogonal shearing pins
07/2014
07/30/2014EP2759469A1 Adaptive solar airframe
07/30/2014CN203740131U 一种采用激光和电喷的蝶形飞行器动力源 One kind of butterfly using laser and EFI vehicle power source
07/30/2014CN203740126U 宽飞行包线变体飞行器 Wide flight envelope variants of the aircraft
07/30/2014CN203740125U 新型飞碟机 The new UFO machine
07/30/2014CN103958348A 具有低级数低压涡轮的燃气涡轮发动机 Having a lower number of low-pressure turbine of a gas turbine engine
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
07/30/2014CN103950541A 基于系统内部气体循环流动的势能获得技术 Access to technology-based system of internal gas circulating potential
07/30/2014CN103950538A 仿雁群扑翼飞行系统 Imitation geese flapping wing flight systems
07/29/2014US8789790 Aircraft engine attachment pylon
07/29/2014CA2803858C Rotary-wing aircraft equipped with a rear rotor and process to optimise the operation of a rear rotor
07/23/2014DE202014005137U1 Hochsichere bemannte Flugzeuge mit Staustrahl Triebwerk mit Kolbenmotor anstatt Brennungskammer und zwei gegenläufige verstellbare Propeller und freie Luftströmungskanäle Highly secure manned aircraft with ramjet engine piston combustion chamber instead and two matching adjustable propeller and free air flow channels
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