Dual series damper system
A dual series damper includes a fluid damper portion and a elastomeric damper portion. The fluid damper portion includes a first housing, a first connection member, and a piston coupled to the first connection member. The piston divides an interior of the first housing into a first fluid chamber and a second fluid chamber. The piston has a fluid passage in the piston, the fluid passage being configured to provide fluid communication between the first fluid chamber and the second fluid chamber. The elastomeric damper portion includes a second housing, a second connection member coupled to the second housing, and an elastomer between the first housing and the second housing. When a lead/lag force is introduced to the dual series damper, the fluid damper portion behaves rigidly so that the elastomeric damper portion dampens the lead/lag oscillation.
1. A dual series damper for a rotorcraft, the dual series damper comprising:
a fluid damper portion comprising:
a first housing;
a first connection member;
a piston coupled to the first connection member, the piston dividing an interior of the first housing into a first fluid chamber and a second fluid chamber;
a fluid passage in the piston, the fluid passage being configured to provide fluid communication between the first fluid chamber and the second fluid chamber;
an elastomeric damper portion comprising:
a second housing;
a second connection member coupled to the second housing;
an elastomer between the first housing and the second housing;
wherein the elastomeric damper portion moves independently of the fluid damper portion; and
wherein the fluid damper portion is configured such that the fluid passage allows a fluid to travel between the first fluid chamber and the second fluid chamber when the dual series damper is subjected to a steady force thereby changing a length of the fluid damper portion.
2. The dual series damper according to claim 1 , wherein the fluid damper portion is configured to behave rigidly when the dual series damper is subjected to a lead/lag oscillatory force.
3. The dual series damper according to claim 1 , wherein the elastomeric damper portion is configured to dampen an oscillatory lead/lag motion and also provide a spring force that adjusts a lead/lag mode frequency to a desired value.
4. The dual series damper according to claim 1 , wherein the fluid damper portion is configured to behave rigidly when the dual series damper is subjected to a force occurring at a lead/lag mode frequency.
5. The dual series damper according to claim 1 , wherein the dual series damper is configured for attachment between a rotor blade and a rotor yoke.
6. The dual series damper according to claim 1 , wherein the dual series damper is configured for attachment between adjacent rotor blades.
7. The dual series damper according to claim 1 , wherein the elastomeric damper portion is configured to dampen a lead/lag oscillatory motion and provide spring force to adjust a lead/lag mode frequency, through deflection of the elastomer.
8. A dual series damper for a rotorcraft, the dual series damper comprising:
a fluid damper portion comprising:
a first housing having a cylinder portion and a central portion;
a first connection member;
a piston coupled to the first connection member, the piston dividing an interior of the cylinder portion of the first housing into a first fluid chamber and a second fluid chamber;
a fluid passage configured to provide fluid communication between the first fluid chamber and the second fluid chamber;
an elastomeric damper portion comprising:
a second housing;
a second connection member coupled to the second housing;
an elastomer between the central portion of the first housing and the second housing;
wherein the elastomeric damper portion is configured to a dampen an oscillatory motion, while the fluid damper portion is configured to eliminate a steady force; the elastomeric damper portion moving independently of the fluid damper portion; and
wherein the fluid damper portion is configured to passively change the length of the dual series damper when subjected to the steady force.
9. The dual series damper according to claim 8 , wherein the oscillatory motion occurs at a lead/lag mode frequency and higher.
10. The dual series damper according to claim 8 , wherein the elastomer of the elastomeric damper portion has a stiffness sufficient to treat the oscillatory motion.
11. The dual series damper according to claim 8 , the fluid damper portion further comprising:
a sliding seal between the piston and the cylinder portion of the first housing.
12. The dual series damper according to claim 8 , the fluid damper portion further comprising:
an elastomer seal between the piston and the cylinder portion of the first housing.
13. The dual series damper according to claim 8 , wherein the fluid damper portion is configured to passively change the length of the dual series damper when subjected to the steady force through a translation of the piston relative to the cylinder portion of the first housing.
14. A rotor hub for an aircraft, the rotor hub comprising:
a rotor yoke;
a plurality of blade grips coupled to the rotor yoke;
a rotor blade coupled to each blade grip;
a dual series damper coupled between each blade grip and the rotor yoke, the dual series damper comprising:
a fluid damper portion comprising:
a first housing;
a first connection member;
a piston coupled to the first connection member, the piston dividing an interior of the first housing into a first fluid chamber and a second fluid chamber;
a fluid passage in the piston, the fluid passage being configured to provide fluid communication between the first fluid chamber and the second fluid chamber;
an elastomeric damper portion comprising:
a second housing;
a second connection member coupled to the second housing;
an elastomer between first housing and the second housing;
wherein the elastomeric damper portion moves independently of the fluid damper portion; and
wherein the fluid damper portion of the dual series damper is configured such that the fluid passage allows a fluid to travel between the first fluid chamber and the second fluid chamber when the dual series damper is subjected to a steady force thereby changing a length of the fluid damper portion.
15. The rotor hub according to claim 14 , wherein the fluid damper portion of the dual series damper is configured to behave rigidly when the dual series damper is subjected to a lead/lag oscillatory force at a lead/lag frequency mode and higher.
16. The rotor hub according to claim 14 , wherein the elastomeric damper portion of the dual series damper is configured to dampen a lead/lag oscillation and provide a spring force to a lead/lag frequency mode.
17. The rotor hub according to claim 14 , wherein the fluid damper portion behaves rigidly when a lead/lag oscillatory force is introduced to the dual series damper, so that the elastomeric damper portion treats the lead/lag oscillatory force.