Patents for B64D 33 - Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for (2,926)
07/2010
07/07/2010EP2204319A2 Aircraft power and thermal management system with electric co-generation
07/07/2010CN101772454A Nacelle comprising at least one surge trap
06/2010
06/30/2010EP2202152A2 Airplane with a rear propeller engine assembly
06/30/2010CA2689176A1 Gas turbine engine with ejector
06/30/2010CA2689174A1 Gas turbine engine with ejector
06/24/2010WO2010000953A8 Nacelle for turbojet engine
06/24/2010US20100155534 Aircraft Baffle Seal
06/24/2010US20100155526 Aircraft with tail propeller-engine layout
06/23/2010EP2197743A2 Air intake structure to be mounted upstream of a nacelle middle structure for aircraft engine, and nacelle equipped with such air intake structure
06/23/2010CA2688878A1 Automatic shut-off valve for the oil circuit in an airplane engine
06/23/2010CA2688201A1 Combined surface cooler and acoustic absorber for turbomachines
06/17/2010WO2009142793A3 Ice shed reduction for leading edge structures
06/17/2010US20100148012 Aircraft engine nacelle with translating inlet cowl
06/15/2010US7735776 Air inlet for a turbofan engine
06/10/2010US20100140418 Air Induction Control
06/08/2010CA2398653C Air intake for commercial aircraft jet engine nacelle
06/03/2010US20100133378 Acoustic panel having a variable acoustic characteristic
05/2010
05/26/2010EP1928744B1 Engine assembly for an aircraft comprising an engine as well as an engine mounting structure for such an engine
05/25/2010US7721989 Multi-path inlet for aircraft engine
05/20/2010WO2010055224A1 Air intake for an aeroplane engine with unducted propellers
05/20/2010WO2009156120A4 Air duct for supplying ambient air in an aircraft
05/20/2010CA2743009A1 Air intake for an aeroplane engine with unducted propellers
05/19/2010EP2186729A1 Acoustic barrel for aircraft engine nacelle including crack and delamination stoppers
05/06/2010US20100108435 Method for making an acoustic absorption panel in particular for the nacelle of an aircraft engine
05/06/2010DE102008055631A1 Nabenkonus für ein Flugzeugtriebwerk Hub cone for an aircraft engine
05/05/2010EP2181921A2 Noise-suppressing strut support system for an unmanned aerial vehicle
05/05/2010EP2181041A1 Nacelle with an adaptable outlet section
04/2010
04/29/2010US20100102164 System, method and apparatus for widespread commercialization of hydrogen as a carbon-free alternative fuel source
04/28/2010EP2178755A2 Coupling system connecting an internal structure and an external structure of a jet engine nacelle
04/28/2010EP2178754A1 Nacelle comprising at least one surge trap
04/28/2010EP2178753A1 Jet engine nacelle equipped with a system for mechanically inhibiting a thrust reverser
04/28/2010EP2178751A1 Nacelle equipped with at least one excess pressure flap
04/22/2010US20100096213 Coating for acoustic treatment having a hot air icing processing function of frost treatment with hot air
04/22/2010DE202009014217U1 Einteilige Triebwerk-Frontschutzabdeckung One-piece engine-Front cover
04/15/2010WO2010040911A1 Air intake arrangement for an aircraft
04/15/2010WO2010040907A1 Air intake structure for a turbine engine nacelle
04/15/2010WO2010040837A2 Sound absorber for an auxiliary engine of an aircraft
04/15/2010WO2010012899A3 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
04/15/2010DE102008051241A1 Silencer for auxiliary power unit of aircraft, has two groups of outer cells whose volume is greater than volume of inner cells that are surrounded by outer cells and formed in flow channel
04/15/2010CA2737979A1 Air intake arrangement for an aircraft
04/15/2010CA2733602A1 Air intake structure for a turbine engine nacelle
04/13/2010US7695355 Integrated housing for fan and alternate flow check valve
04/08/2010US20100084507 Removable air intake structure for turbojet engine nacelle
04/06/2010US7690601 Reversible space plane
04/06/2010US7690595 System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines
04/01/2010WO2010034922A1 Device for connecting an air inlet with an aircraft nacelle actuator assembly
04/01/2010WO2010034893A1 Nacelle with a variable nozzle section
04/01/2010WO2009156120A3 Air duct for supplying ambient air in an aircraft
04/01/2010CA2734417A1 Nacelle with a variable nozzle section
03/2010
03/31/2010CN101687552A Air intake arrangement for a vehicle, in particular an aircraft
03/24/2010CN101678898A Nacelle rear assembly for turbojet engine
03/24/2010CN101678897A Propulsion assembly for aircraft with sliding nacelle
03/18/2010WO2010001009A3 Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
03/18/2010US20100065691 Modular externally accessible batteries for an aircraft
03/17/2010EP2163748A1 Integrated inlet fan case
03/17/2010EP2162359A2 Nacelle rear assembly for turbojet engine
03/16/2010US7677472 Drilled and integrated secondary fuel nozzle and manufacturing method
03/15/2010CA2671648A1 Auxiliary power unit inlet duct with acoustic silencing
03/09/2010CA2493507C Compressor for an aircraft engine
03/04/2010US20100051756 System, method, and apparatus for throat corner scoop offtake for mixed compression inlets on aircraft engines
03/04/2010DE202009014218U1 CNA Abdeckung CNA cover
02/2010
02/25/2010WO2010022362A2 Jet engine exhaust nozzle and associated system and method of use
02/25/2010US20100044522 Air inlet for a vehicle
02/25/2010DE102008035823A1 Wärmeübertrager für die Außenhaut eines Flugzeugs Heat exchanger for the outer skin of an aircraft
02/24/2010EP1999022B1 Air inlet shroud structure
02/23/2010US7665694 Dual action inlet door and method for use thereof
02/18/2010WO2010018314A1 Inner wall for the nacelle of a turbine engine
02/18/2010CA2733094A1 Inner wall for the nacelle of a turbine engine
02/17/2010EP2152583A1 Coating for acoustic treatment including a rime hot-air treating function
02/17/2010EP2152582A1 Propulsion assembly for aircraft with sliding nacelle
02/17/2010CN201406025Y Layout structure of reverse thrust hydraulic control valve of airplane with tail suspension-type engine
02/11/2010WO2010015758A1 Method for making deicing system on a nacelle panel
02/11/2010US20100031629 Lockable guiding system for a mobile part of a nacelle
02/11/2010DE102008037142A1 Ausfahrbarer Abweiser zum Freisetzen von Struktur schädigenden Fluiden Extendable deflector for releasing structure harmful fluids
02/11/2010CA2732801A1 Method for making deicing system on a nacelle panel
02/10/2010CN101646601A Lockable guiding system for a mobile part of a nacelle
02/04/2010WO2010012899A2 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
02/04/2010US20100025542 Multi-path inlet for aircraft engine
02/04/2010DE102008035160A1 Verfahren zur Verbesserung der Strömungsverhältnisse am Propeller oder Fan eines Flugzeugtriebwerks und danach ausgebildeter Nabenkonus A method for improving the flow conditions at the propeller or fan of an aircraft engine and then trained hub cone
02/04/2010CA2732351A1 Assembly of components connected by a device that maintains the integrity of the surface of one of the components
02/03/2010EP2148815A2 Air intake arrangement for a vehicle, in particular an aircraft
02/03/2010CN100586796C Ram air channel for the supply of ambient air in an aircraft and operation method thereof
01/2010
01/28/2010US20100019101 Gas turbine engine nacelle
01/28/2010US20100019100 Gas turbine engine nacelle
01/27/2010EP2148064A2 Gas turbine engine nacelle
01/27/2010EP2148063A2 Gas turbine engine nacelle
01/27/2010EP2148062A2 Gas turbine engine nacelle
01/27/2010EP2147862A2 Auxiliary power unit inlet door actuation mechanism
01/27/2010EP2147860A2 Heat exchanger assembly for an aircraft control
01/21/2010WO2010007258A1 Aircraft engine nacelle air intake assembly
01/21/2010CA2727864A1 Aircraft engine nacelle air intake assembly
01/14/2010WO2009138833A3 Coupling for inducing high temperature drops between connected parts on an aircraft
01/14/2010WO2009122037A3 Device for reducing turboprop infrared emissions
01/12/2010CA2380677C Jet engine nose inlet cowl with de-icing protection
01/07/2010WO2010001009A2 Measurement instrument support interposed between a drive unit and an air intake of an aircraft nacelle
01/07/2010WO2010001008A1 Method of depositing a coating for improving laminar flow
01/07/2010WO2010000953A1 Nacelle for turbojet engine
01/07/2010WO2009138685A3 Wave attenuation panel inserted between the motor and air inlet of an aircraft nacelle
01/07/2010DE102008027275A1 Air-breathing nacelle for aircraft engine, has circular front contour and sucking unit that is provided for sucking air into nacelle, where sucking unit comprises turbocharger with fan and turbine
01/07/2010CA2711604A1 Nacelle for turbojet engine
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