| Patents for B64D 29 - Power-plant nacelles, fairings, or cowlings (1,701) |
|---|
| 09/10/1997 | EP0794118A1 Flow control apparatus for gas turbine engine installation pressure relief doors |
| 08/13/1997 | EP0696985B1 Nacelle arrangement |
| 08/05/1997 | US5653406 For enclosing an engine suspended from a wing of an airplane |
| 07/23/1997 | EP0784564A1 Nacelle and mounting arrangement for an aircraft engine |
| 07/09/1997 | EP0783042A1 Coating for aerospace aluminium parts |
| 07/08/1997 | US5645250 Multi-purpose aircraft |
| 07/02/1997 | EP0781861A1 Coating for aerospace aluminium parts |
| 04/29/1997 | US5624221 Multiple speed fastener |
| 04/29/1997 | US5623820 Flow control apparatus for gas turbine engine installation pressure relief doors |
| 04/15/1997 | US5620212 Low profile hook latch assembly |
| 03/11/1997 | US5609313 Aircraft propulsive power unit |
| 02/18/1997 | US5603471 Ducted fan turbine engine nozzle assembly |
| 02/05/1997 | EP0756557A1 An aircraft propulsive power unit |
| 01/02/1997 | EP0631554B1 An aircraft propulsive power unit |
| 12/17/1996 | US5584447 Noise control using a plate radiator and an acoustic resonator |
| 11/27/1996 | EP0744339A1 Aircraft engine nacelle with a nacelle cowling |
| 11/25/1996 | CA2177123A1 Aircraft engine pod and cowling |
| 09/17/1996 | US5556142 For joining two members under tension and shear loading |
| 07/04/1996 | WO1996020111A1 A mounting arrangement for a gas turbine engine |
| 06/19/1996 | EP0596070B1 Closure default indicator |
| 06/11/1996 | US5524847 Nacelle and mounting arrangement for an aircraft engine |
| 06/11/1996 | US5524846 Fire protection system for airplanes |
| 06/05/1996 | EP0714363A1 Multi-purpose aircraft |
| 05/21/1996 | US5518206 Closure default indicator |
| 04/25/1996 | WO1996011843A1 Nacelle and mounting arrangement for an aircraft engine |
| 04/10/1996 | EP0605525B1 Ducted fan turbine engine nozzle assembly |
| 03/12/1996 | US5497961 Gas turbine engine nacelle assembly |
| 02/21/1996 | EP0696985A1 Nacelle arrangement |
| 02/13/1996 | US5490644 Ducted boundary layer diverter |
| 01/23/1996 | US5485975 Slotted cowl inlet lip for introducing high pressure air |
| 10/26/1995 | WO1995028318A1 An aircraft propulsive power unit |
| 10/11/1995 | EP0489894B1 A composite structural component |
| 08/23/1995 | EP0597861B1 Gas turbine engine nacelle assembly |
| 06/08/1995 | WO1995005974A3 Multi-purpose aircraft |
| 05/30/1995 | CA2064755C A composite structural component |
| 03/14/1995 | CA1334723C Ducted fan turbine engine |
| 03/02/1995 | WO1995005974A2 Multi-purpose aircraft |
| 01/04/1995 | EP0631554A1 An aircraft propulsive power unit. |
| 12/13/1994 | US5372338 Mounting arrangement for a gas turbine engine |
| 12/06/1994 | US5369954 Turbofan engine bypass and exhaust system |
| 11/24/1994 | WO1994026591A1 Nacelle arrangement |
| 09/27/1994 | US5350136 Nacelle arrangement |
| 08/04/1994 | WO1994016945A1 An aircraft propulsive power unit |
| 08/04/1994 | CA2131598A1 An aircraft propulsive power unit |
| 07/13/1994 | EP0605525A1 Ducted fan turbine engine nozzle assembly. |
| 05/31/1994 | US5315820 Composite structural component |
| 05/25/1994 | EP0597861A1 Gas turbine engine nacelle assembly. |
| 05/11/1994 | EP0596070A1 Closure default indicator. |
| 04/19/1994 | US5303508 Access door, especially for an aircraft engine cowling, provided with synchronized pivoting articulated flap |
| 12/09/1993 | WO1993024368A1 Closure default indicator |
| 12/09/1993 | CA2113619A1 Closure default indicator |
| 12/07/1993 | US5267760 Locking mechanism |
| 12/07/1993 | CA1324999C Bodies with reduced surface drag |
| 10/12/1993 | US5251435 For use in an aircraft turbofan engine |
| 08/31/1993 | US5239822 Composite structure for thrust reverser torque box |
| 05/25/1993 | US5213286 Door for aircraft nacelle |
| 05/05/1993 | EP0540193A1 Reverser inner cowl with integral bifurcation walls and core cowl |
| 04/20/1993 | US5203525 Hinge with offset pivot line |
| 04/20/1993 | US5203215 Mechanical component attachment safety system |
| 04/13/1993 | CA1316163C Aircraft pylon |
| 04/01/1993 | WO1993006006A1 Ducted fan turbine engine nozzle assembly |
| 04/01/1993 | CA2119440A1 Ducted fan turbine engine nozzle assembly |
| 03/01/1993 | CA2072417A1 Aircraft engine nacelle having circular arc profile |
| 02/18/1993 | WO1993002920A1 Gas turbine engine nacelle assembly |
| 01/26/1993 | US5181675 Pod for suspending a turbojet engine unit of the bypass type under the wing of an aircraft |
| 12/02/1992 | EP0516468A2 Jet engine fan nacelle |
| 12/01/1992 | CA2065637A1 Jet engine fan nacelle |
| 10/27/1992 | US5157915 Pod for a turbofan aero engine of the forward contrafan type having a very high bypass ratio |
| 10/20/1992 | US5156362 Jet engine fan nacelle |
| 10/20/1992 | US5156360 Flexible fire seal for overlapping cowl side edges |
| 10/14/1992 | EP0508503A1 Flexible fire seal for overlapping cowl side edges |
| 08/18/1992 | US5138753 Cowling closing device |
| 08/11/1992 | US5136839 Ducted fan turbine engine |
| 07/07/1992 | US5127222 Buffer region for the nacelle of a gas turbine engine |
| 06/17/1992 | EP0489894A1 A composite structural component. |
| 05/12/1992 | US5112191 Aircraft propulsion system |
| 04/15/1992 | EP0480827A1 Device for mechanical security |
| 04/07/1992 | US5102069 Aircraft wing pylon extensions for minimized aerodynamic penalties |
| 04/07/1992 | US5101621 Integrated corner for ducted fan engine shrouds |
| 03/18/1992 | EP0475877A1 Aircraft engine cowling roller attachment |
| 03/01/1992 | CA2047912A1 Engine cowling roller attachment |
| 01/21/1992 | US5082424 Connection system for aircraft propeller blades |
| 12/31/1991 | US5076514 Apparatus for latching two parts together |
| 12/29/1991 | WO1992000183A1 A composite structural component |
| 12/17/1991 | US5072898 For an aircraft |
| 10/23/1991 | EP0453360A1 Aviation engine with high bypass ratio and of the type with front contra-rotating fan |
| 10/08/1991 | US5054715 Apparatus and methods for reducing aircraft lifting surface flutter |
| 09/10/1991 | US5046689 Cowling interlock system |
| 07/30/1991 | US5035379 Movable aircraft engine cowling |
| 07/24/1991 | EP0437868A1 Apparatus and methods for reducing aircraft lifting surface flutter |
| 06/19/1991 | EP0432972A1 Aircraft wing pylon extensions for minimised aerodynamic penalties |
| 05/18/1991 | CA2025244A1 Bolt shield for rotating exhaust duct |
| 05/07/1991 | US5012639 Buffer region for the nacelle of a gas turbine engine |
| 03/27/1991 | CN1012152B Centrifugal pressure expanding propeller |
| 03/08/1991 | CA2021087A1 Ultra high bypass engine integrated fan/cowl and transportation/removal |
| 02/19/1991 | US4993663 Engine of an aircraft |
| 12/05/1990 | CA2012246A1 Connection system for aircraft propeller blades |
| 12/01/1990 | CA2012248A1 Hybrid laminar flow nacelle |
| 11/07/1990 | EP0208726B1 Fire-resistant cowls, particularly for aircraft engines |
| 10/30/1990 | US4966338 Aircraft pylon |