Temperature adaptive fluid damping system
A temperature adaptive fluid damping system is provided. One embodiment of the temperature adaptive fluid damping system comprises two fluid chambers, a piston in fluid communication with the fluid chambers, and a fluid path between the fluid chambers. An elastomeric retaining element adjacent to the fluid path is constrained to deform substantially perpendicular to the fluid path, so that the retaining element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature.
1. A thermally adaptive damper, comprising:
a first fluid chamber;
a second fluid chamber;
a piston in fluid communication with the first fluid chamber and the second fluid chamber;
a first elastomeric seal in fluid communication with the first fluid chamber and sealingly attached to an outer surface of a first end of the piston;
a second elastomeric seal in fluid communication with the second fluid chamber and sealingly attached to an outer surface of a second end of the piston;
a fluid path extending through the piston from the first fluid chamber and the second fluid chamber;
an elastomeric retaining element adjacent to the fluid path, constrained to deform substantially perpendicular to the fluid path, so that the retaining element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature;
a non-elastomeric valve element embedded within the elastomeric retaining element, so that the valve element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature.
2. The damper according to claim 1 , wherein:
the elastomeric retaining element is constrained by a wall between the first fluid chamber and the second fluid chamber;
the wall includes a bore adapted to receive the piston; and
the fluid path comprises an orifice between the valve element and the piston.
3. The damper according to claim 1 , wherein:
the fluid path comprises a bore through the piston; and
the elastomeric retaining element is embedded in the piston.
4. The damper according to claim 1 , wherein the first and second elastomeric seals are high-capacity laminate seals.
5. The damper according to claim 1 , wherein the valve element is segmented such that at least one additional fluid path is provided between the first fluid chamber and the second fluid chamber.
6. A thermally adaptive damper, comprising:
a first elastomeric seal and a second elastomeric seal sealingly attached to an inner surface of a housing and sealingly attached to an outer surface of a piston, whereby a first fluid chamber is formed between the housing, the first elastomeric seal, and a first end of the piston, and a second fluid chamber is formed between the housing, the second elastomeric seal, and a second end of the piston;
a fluid path through the piston between the first fluid chamber and the second fluid chamber;
a elastomeric retaining element embedded in the piston and constrained by an inner surface of the piston to deform substantially perpendicular to the fluid path; and
a valve element embedded in the retaining element so that the valve element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature.
7. The damper according to claim 6 , wherein the first and second elastomeric seals are high-capacity laminate seals.
8. The damper according to claim 6 , wherein the valve element is segmented such that at least one additional fluid path is provided between the first fluid chamber and the second fluid chamber.
9. An aircraft, comprising:
a mast operably connected to a drive unit;
a central member fixed to the mast,
a blade strap hingedly connected to the central member;
a thermally adaptive fluid damper secured within the blade strap;
a blade grip secured to the blade strap; and
an elastomeric bearing secured in the blade strap operably engaged to the blade grip and to the thermally adaptive fluid damper;
wherein the thermally adaptive fluid damper comprises:
a first fluid chamber;
a second fluid chamber;
a piston in fluid communication with the first fluid chamber and the second fluid chamber;
a first elastomeric seal in fluid communication with the first fluid chamber and sealingly attached to an outer surface of a first end of the piston;
a second elastomeric seal in fluid communication with the second fluid chamber and sealingly attached to an outer surface of a second end of the piston;
a fluid path extending through the piston from the first fluid chamber and the second fluid chamber; and
an elastomeric retaining element adjacent to the fluid path, constrained to deform substantially perpendicular to the fluid path, so that the retaining element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature.
10. The aircraft according to claim 9 , wherein the damper further comprises a valve element embedded within the elastomeric retaining element, so that the valve element is operable to vary the cross-sectional area of the fluid path inversely to a change in temperature.
11. The aircraft according to claim 9 , wherein:
the fluid path comprises a bore through the piston; and
the elastomeric retaining element is embedded in the piston.
12. The aircraft according to claim 9 , wherein the first and second elastomeric seals are high-capacity laminate seals.
13. The aircraft according to claim 10 , wherein the valve element is segmented such that at least one additional fluid path is provided between the first fluid chamber and the second fluid chamber.