Landing gear noise reduction
View Patent ↗An aircraft landing gear ( 1 ) is described including a noise-reducing element that includes an air-deflecting surface, in the form of a fairing ( 4 ), and a perforated airflow-reducing region ( 8 ). In use, some air passes through the perforations, whilst other air is deflected by the fairing away from a noise-generating region of the landing gear. Noise caused by the passing of the landing gear through the air is therefore reduced.
1. An aircraft landing gear including a noise-reducing element that includes
an air-deflecting surface wherein said air-deflecting surface includes a first region encompassing no apertures and a second region encompassing at least ten apertures, the area covered by the first region having a minimum dimension that is at least as great as the maximum dimension of the area covered by the second region, and
an airflow-reducing region having more than 10 apertures through which, in use, air may pass,
whereby the noise-reducing element is able in use to deflect air away from a noise-generating region of the landing gear, whilst allowing some air to pass through the element, thereby reducing the noise caused by the passing of the landing gear through the air.
2. An aircraft landing gear according to claim 1 , wherein the 15 noise-reducing element includes at least 50 apertures.
3. An aircraft landing gear according to claim 1 , wherein the apertures are in the form of perforations.
4. An aircraft landing gear according to claim 1 , wherein the arrangement of the apertures across the air-deflecting surface is non-uniform.
5. An aircraft landing gear according to claim 1 , wherein the first region is near to the periphery of the air-deflecting surface.
6. An aircraft landing gear according to claim 1 , wherein the airflow-reducing region is disposed between two regions defined by the air-deflecting surface.
7. An aircraft landing gear according to claim 1 , wherein the airflow-reducing region covers an area, which would, if the airflow-reducing region were replaced with an extension of the air-deflecting surface, cover at least one stagnation point or cover at least the majority of a stagnation line.
8. An aircraft landing gear according to claim 1 , wherein the noise-reducing element is so arranged that in use it shields at least a part of the landing gear.
9. An aircraft landing gear according to claim 1 , wherein the noise-reducing element is in the form of a fairing that covers at least a part of the landing gear.
10. An aircraft landing gear according to claim 1 , wherein the landing gear is movable from a stored position to an operative position.