Damping structure and applications
First Claim
Patent Images
1. A damping structure having an internal cavity (2) and comprising:
- an aggregate (8) which comprises at least solid bodies (9) in contact and which completely fills said internal cavity (2); and
a rigid plate (11) for closing off said internal cavity (2), characterized in that it additionally comprises an elastic means (12) which exerts elastic pressure on said rigid plate (11) so as to constrain said aggregate (8).
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Accused Products
Abstract
A composition for reducing vibrations, including both damping structure borne vibrations and reducing radiated airborne noise. The composition is either a mixture of at least two different granular materials, or is a granular material having a bulk sound speed of less than 90 m/s. The damping properties of a mixture can be calculated from the bulk densities and stiffnesses of its individual components.
21 Citations
43 Claims
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1. A damping structure having an internal cavity (2) and comprising:
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an aggregate (8) which comprises at least solid bodies (9) in contact and which completely fills said internal cavity (2); and
a rigid plate (11) for closing off said internal cavity (2), characterized in that it additionally comprises an elastic means (12) which exerts elastic pressure on said rigid plate (11) so as to constrain said aggregate (8). - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 41, 42, 43)
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14. A damping structure having an internal cavity (2) and comprising:
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an aggregate (8) which comprises at least solid bodies (9) in contact and which completely fills said internal cavity (2); and
a rigid plate (11) for closing off said internal cavity (2), characterized in that it additionally comprises at least one internal partition (13) which is arranged inside said internal cavity (2) and which is at least partially pierced. - View Dependent Claims (15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25)
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26. A damping structure with an internal cavity (2) and comprising:
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an aggregate (8) which comprises at least solid bodies (9) in contact and which completely fills said internal cavity (2); and
means (10) for closing off the internal cavity (2) and pressing said aggregate (8) into said internal cavity (2), characterized in that it is rigid. - View Dependent Claims (27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39)
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40. A suspension system for a rotary wing aircraft, particularly helicopter, gearbox, said suspension system comprising a number of suspension bars (15),
characterized in that at least one of said suspension bars (15) comprises a damping structure (1) with an internal cavity (2) and comprising: -
an aggregate (8) which comprises at least solid bodies (9) in contact and which completely fills said internal cavity (2); and
a rigid plate (11) for closing off said internal cavity (2).
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Specification