PASSIVELY DAMPED END FITTINGS AND BRACKETS
A passively damped mechanical system is disclosed, for example for use in aerospace applications where vibration can adversely affect navigational and operational instruments. In one example, the passively damped mechanical system includes an end fitting of a strut used to connect a structural element to a payload. The end fitting may include outer and inner cylindrical hubs, with a space between the outer and inner cylindrical hub at least partially filled with a viscoelastic material. In a further example, the passively damped mechanical system includes legs used to connect a structural element to a bracket configured to support a payload. Each leg may include a hollow interior having a lattice structure to add strength and a viscoelastic material to provide passive damping.
1 . A passively damped mechanical structure, comprising:
a structural element;
a bracket configured to hold a payload;
one or more legs each having a length extending between and connecting the structural element to the bracket, each leg having a wall and a hollow interior, a leg of the one or more legs comprising:
a lattice structure provided within the hollow interior along at least a portion of the leg; and
a viscoelastic material (VEM) provided within the hollow interior along at least a portion of the lattice structure, the VEM adhering to the wall and the lattice structure.
2 . The passively damped mechanical structure of claim 1 , wherein the VEM dissipates vibrational energy and prevents at least a portion of the vibrational energy from reaching the bracket.
3 . The passively damped mechanical structure of claim 1 , wherein the VEM dissipates shear loads exerted on the VEM by the lattice structure.
4 . The passively damped mechanical structure of claim 1 , wherein the one or more legs comprise four spaced apart legs.
5 . The passively damped mechanical structure of claim 1 , wherein the lattice structure comprises a lattice of repeating truss structures.
6 . The passively damped mechanical structure of claim 5 , wherein the lattice of repeating truss structures comprises a tetrahedral core of joined crosspieces.
7 . The passively damped mechanical structure of claim 5 , wherein the lattice of repeating truss structures comprises one of 3D Kagome, octahedral, hexagonal or pyramidal truss structures.
8 . The passively damped mechanical structure of claim 1 , wherein the lattice structure is formed of titanium.
9 . The passively damped mechanical structure of claim 1 , wherein the VEM occupies all cross-sectional area of a leg not occupied by the lattice structure.
10 . The passively damped mechanical structure of claim 1 , wherein an amount of the VEM added into a leg is selected to optimally tune at least one of damping and response to shock loads.
11 . The passively damped mechanical structure of claim 1 , wherein a leg with a predefined amount of VEM is selected for use in the passively damped mechanical structure to optimally tune at least one of damping and response to shock loads.
12 . The passively damped mechanical structure of claim 1 , wherein a length of the VEM column within a leg is selected to optimally tune at least one of damping and response to shock loads.
13 . The passively damped mechanical structure of claim 1 , wherein the VEM has an anisotropic response, exhibiting greater damping for vibrations applied in a given direction than for vibrations applied in other directions.
14 . A passively damped mechanical structure configured to mount to a structural element, the passively damped mechanical structure, comprising:
a bracket configured to hold a payload;
one or more legs each having a length extending between and connecting the structural element to the bracket, each leg having a wall and a hollow interior, a leg of the one or more legs comprising:
a lattice structure provided within the hollow interior along at least a portion of the leg; and
a viscoelastic material (VEM) provided within the hollow interior along at least a portion of the lattice structure, the VEM adhering to at least the lattice structure, an amount of VEM material provided within the hollow interior selected to optimally tune at least one of damping and response to shock loads.
15 . The passively damped mechanical structure of claim 14 , wherein the VEM further adheres to the wall of the leg.
16 . The passively damped mechanical structure of claim 14 , wherein the bracket comprise one or more planar surfaces, each planar surface of the one or more planar surfaces configured to receive the payload in the form of a shock-sensitive momentum wheel.
17 . The passively damped mechanical structure of claim 14 , wherein the bracket comprise one or more planar surfaces, each planar surface of the one or more planar surfaces configured to receive the payload in the form of shock sensitive instrumentation.
18 . The passively damped mechanical structure of claim 14 , wherein the VEM dissipates vibrational energy and prevents at least a portion of the vibrational energy from reaching the bracket.
19 . A passively damped mechanical structure configured to mount to a structural element, the passively damped mechanical structure, comprising:
a bracket comprising one or more planar surfaces, each planar surface of the one or more planar surfaces configured to hold a payload;
a plurality of legs each having a length extending between and connecting the structural element to the bracket, each leg having a wall and a hollow interior, a leg of the plurality of legs comprising:
a lattice structure provided within the hollow interior along at least a portion of the leg; and
a viscoelastic material (VEM) provided within the hollow interior along at least a portion of the lattice structure, the VEM adhering to the wall and the lattice structure;
wherein the VEM dissipates vibrational energy and prevents at least a portion of the vibrational energy from reaching the bracket.
20 . The passively damped mechanical structure of claim 14 , wherein the payload comprises one of a shock-sensitive momentum wheel and shock-sensitive instrumentation.