Patent application number | Description | Published |
20090008501 | LANDING GEAR - An aircraft landing gear door assembly includes a door, which is moveable to an open position, in which an aperture is exposed, the landing gear being able to be deployed through said aperture, and moveable to a closed position, in which the door is closed across the aperture. The door is arranged for rotational movement of a first type, in which the door rotates about an axis that is substantially parallel to the length of the aircraft, between the closed position and the open position. The door is also arranged for movement of a second type, different from the first type, in which the door rotates, about an axis that is substantially transverse to the length of the aircraft, to a position in which it acts as a fairing to reduce the noise caused by the landing gear or a part thereof. In one embodiment, the second type of movement is rotational movement about an axis that is substantially parallel to the door when in the closed position and the door forms a ramp type fairing. In another embodiment, the second type of movement is rotational movement about an axis that is substantially transverse to the door when in the closed position and the door forms a V-shaped fairing (when viewed from above) with an opposite door. | 01-08-2009 |
20090078821 | LANDING GEAR - An aircraft noise-reduction apparatus ( | 03-26-2009 |
20090321559 | Aircraft noise reduction apparatus - The invention relates to aircraft noise reduction apparatus, in particular, but not exclusively, to noise reduction apparatus on an aircraft landing gear. The aircraft noise reduction apparatus comprises a noise reduction attachment for a landing gear of an aircraft. The noise reduction apparatus is movable between a first position in which it deflects air away from a noise inducing component of the landing gear and a second position in which it allows access to the noise inducing component. The movement of the noise reduction attachment between the first and second positions is actuated by a part of the landing gear. | 12-31-2009 |
20100006696 | Landing gear noise reduction assembly - An aircraft noise reduction apparatus including an aircraft landing gear assembly ( | 01-14-2010 |
20100012778 | Torque link set - An aircraft landing gear ( | 01-21-2010 |
20100155529 | Landing gear with noise reduction fairing - An aircraft noise reduction apparatus is provided which includes an aircraft landing gear assembly and a noise reduction fairing | 06-24-2010 |
20100288876 | BLUFF BODY NOISE CONTROL - An aircraft noise-reduction apparatus comprise a flow-facing element ( | 11-18-2010 |
20110139926 | Landing gear with noise reduction apparatus - An aircraft landing gear assembly comprises a landing gear ( | 06-16-2011 |
20110168483 | BLUFF BODY NOISE CONTROL - The present invention provides a method of and apparatus for, reducing noise caused by the interaction of airflow between two bluff bodies which are in a generally tandem arrangement, the method comprising providing flow control such that the peak turbulence is at least partially displaced from, or reduced at, the surface of the downstream body. The invention also provides an aircraft noise reduction device, and a method of using such a device, comprising a flow control apparatus ( | 07-14-2011 |
20130193268 | BLUFF BODY NOISE CONTROL - An aircraft noise-reduction apparatus comprise a flow-facing element ( | 08-01-2013 |
20130313360 | LANDING GEAR FOR AN AIRCRAFT - The invention provides a landing gear | 11-28-2013 |
Patent application number | Description | Published |
20140058708 | COMPUTER-IMPLEMENTED METHOD OF SIMPLIFYING A COMPLEX PART IN A GEOMETRIC MODEL - A computer-implemented method of simplifying a complex part in a geometric model by approximating its shape, including creating a two-dimensional cross-sectional plane through the complex part in at least two of three mutually orthogonal axes of the part, to give two or three planes, each reproducing the shape of the complex part at the cross section; and performing a combination operation on the planes to form a new body from the planes. | 02-27-2014 |
20140359130 | PROCESS MIGRATION METHOD, COMPUTER SYSTEM AND INTERMEDIATE COMPUTING RESOURCES - A process migration method comprising
| 12-04-2014 |
20140365184 | METHOD AND APPARATUS FOR PREPARATION OF A COMPUTATIONAL FLUID DYNAMICS MODEL - A method of preparation of a Computational Fluid Dynamics (CFD) model of a multi-component product including a plurality of individual components for simulation, the method including providing a simplified model employing a simplified obstacle to fluid flow in place of one or more components in the model; solving the simplified model; and using the solution of the simplified model to add to modeling data by providing starting values for fluid flow in the simulation of the CFD model. | 12-11-2014 |
20140379308 | DECOUPLED PARALLEL MESHING IN COMPUTER AIDED DESIGN - A method of meshing, for use in a computer-aided design (CAD) or computer-aided engineering (CAE) system, includes a procedure of: carrying out in parallel a plurality of CAD meshing processes so as to generate one or more meshes of the said CAD domain, each CAD meshing process of the said plurality being different from the other meshing processes in the said plurality; determining which of the meshes so generated satisfies one or more preset meshing criteria which are indicative of the quality of the mesh; and selecting for use in a subsequent CAD/CAE process one of the generated meshes which satisfies the said one or more preset meshing criteria. | 12-25-2014 |