Engine mount system and elements for reduced force transmission and reduced static motion

1. A compliant engine mount system for reacting loads from an engine of an aircraft to an aircraft structure, the system comprising:

a top mount comprising:

an upper link comprising an upper bearing surface;

a housing comprising;

a lower bearing surface disposed along the longitudinal axis of the top mount;

a center structure centrally disposed relative to the longitudinal axis of the top mount and comprising a compression stop configured to carry loads in compression and at least one tension stop configured to carry loads in tension;

wherein the upper link is configured to interlock within the center structure;

a lower mount comprising:

an upper link comprising an upper bearing surface;

a housing comprising:

a lower bearing surface disposed along the longitudinal axis of the lower mount;

a center structure centrally disposed relative to the longitudinal axis of the lower mount and comprising a compression stop configured to carry loads in compression and at least one tension stop configured to carry loads in tension;

wherein the upper link is configured to interlock within the center structure; and

a center trunnion mount comprising:

a pin configured to be received within an engine bearing structure of the engine;

a pivot element disposed on a surface of the pin, the pivot element being configured to react the loads from the engine; and

an elastomeric compliance element disposed inboard on the pin relative to the pivot element.

2. The compliant engine mount system of claim 1 , wherein the top mount comprises:

a flexing element in sealing contact with the housing;

a fluid which fills, at least partially, a cavity within the flexing element and the housing; and

an inner member located within the cavity, the cavity having a gas-filled space/bladder therein;

wherein loading of the top mount occurs along the longitudinal axis thereof.

3. The compliant engine mount system of claim 1 , wherein the lower mount comprises:

a flexing element in sealing contact with the housing;

a fluid which fills, at least partially, a cavity within the flexing element and the housing; and

an inner member located within the cavity, the cavity having a gas-filled space/bladder therein;

wherein loading of the top mount occurs along the longitudinal axis thereof.

4. The compliant engine mount system of claim 1 , wherein the upper link of the top mount is in compression or tension resulting from flexing element being biased against either the at least one compression stop or the at least one tension stop in a pre-loaded state.

5. The compliant engine mount system of claim 1 , wherein the upper link of the lower mount is in compression or tension resulting from flexing element being biased against either the at least one compression stop or the at least one tension stop in a pre-loaded state.

6. The compliant engine mount system of claim 1 , wherein the center trunnion comprises at least one stop configured to bound a movement of the pin within the housing in an inboard direction, a fore direction, vertical direction, and/or an aft direction.

7. The compliant engine mount system of claim 1 , the system further comprising:

an aft mount comprising:

an inner lug; and

an inboard elastomer package configured to move laterally with the inner lug inside of a housing;

wherein lateral movement of the inner lug and inboard elastomer package is bounded by a first position and a second position;

wherein the inboard elastomer package comprises an inner member configured to form a fluid cavity at an inboard end of the housing;

wherein the inner member is movable along a longitudinal axis of the housing to modify a volume of the fluid cavity; and

wherein lateral movement of the inner lug and inboard elastomer package pumps a fluid into or out of the fluid cavity to change a volume of a gas-filled space/bladder.

8. The compliant engine mount system of claim 7 , wherein:

the aft mount comprises a stop plate located outside of the inboard end of the housing;

the stop plate is movable laterally along with the inner lug;

the inner lug comprises an outboard stop portion located outside of an outboard end of the housing; and

a position of the inner lug is bounded by distances from the housing to the stop plate and the outboard stop portion, respectively.

9. The compliant engine mount system of claim 7 , wherein the aft mount comprises an outboard elastomer package.

10. A method for reacting loads from an engine of an aircraft to an aircraft structure, the method comprising:

providing a top mount comprising:

an upper link comprising an upper bearing surface;

a housing comprising;

a lower bearing surface disposed along the longitudinal axis of the top mount; and

a center structure centrally disposed relative to the longitudinal axis of the top mount and comprising a compression stop for carrying loads in compression and at least one tension stop for carrying loads in tension;

interlocking the upper link within the center structure;

providing a lower mount comprising:

an upper link comprising an upper bearing surface;

a housing comprising:

a lower bearing surface disposed along the longitudinal axis of the lower mount; and

a center structure centrally disposed relative to the longitudinal axis of the lower mount and comprising a compression stop for carrying loads in compression and at least one tension stop for carrying loads in tension;

interlocking the upper link within the center structure;

providing a center trunnion mount comprising:

a pin arranged within an engine bearing structure of the engine;

a pivot element disposed on a surface of the pin;

an elastomeric compliance element disposed inboard on the pin relative to the pivot element;

transmitting a load from the engine to the top mount, the lower mount, and/or the center trunnion; and

reacting the load from the engine with the top mount, the lower mount, and/or the center trunnion.

11. The method according to claim 10 , wherein:

lateral movement of the pin is bounded in an inboard direction along a longitudinal axis of the housing by a first position;

when the load acts along a longitudinal axis of the pin, the pin moves substantially freely along the longitudinal axis of the housing; and

when the load acts transverse to the longitudinal axis of the pin, the load is reacted by a pivot element and an elastomeric compliance element.

12. The method of claim 10 , wherein the top mount comprises:

a flexing element in sealing contact with the housing;

a fluid which fills, at least partially, a cavity within the flexing element and the housing; and

an inner member located within the cavity, the cavity having a gas-filled space/bladder therein;

wherein the load is transmitted to the top mount and acts along the longitudinal axis thereof.

13. The method of claim 10 , wherein the lower mount comprises:

a flexing element in sealing contact with the housing;

a fluid which fills, at least partially, a cavity within the flexing element and the housing; and

an inner member located within the cavity, the cavity having a gas-filled space/bladder therein;

wherein the load is transmitted to the lower mount and acts along the longitudinal axis thereof.

14. The method of claim 10 , wherein the upper link of the top mount is in compression or tension resulting from flexing element being biased against either the at least one compression stop or the at least one tension stop in a pre-loaded state.

15. The method of claim 10 , wherein the upper link of the lower mount is in compression or tension resulting from flexing element being biased against either the at least one compression stop or the at least one tension stop in a pre-loaded state.

16. The method of claim 10 , wherein the center trunnion mount comprises at least one stop, the method comprising using the at least one stop for bounding a movement of the pin within the housing in an inboard direction, a fore direction, vertical direction, and/or an aft direction.

17. The method of claim 10 , comprising:

providing an aft mount comprising:

an inner lug; and

an inboard elastomer package that is movable laterally with the inner lug inside of a housing;

wherein lateral movement of the inner lug and inboard elastomer package is bounded by a first position and a second position;

wherein the inboard elastomer package comprises an inner member forms a fluid cavity at an inboard end of the housing;

wherein the inner member is movable along a longitudinal axis of the housing to modify a volume of the fluid cavity; and

wherein lateral movement of the inner lug and inboard elastomer package pumps a fluid into or out of the fluid cavity to change a volume of a gas-filled space/bladder; and

transmitting a load from the engine to the aft mount; and

reacting the load from the engine with the aft mount;

wherein, when the load acts along a longitudinal axis of the housing, the inner lug and the inboard elastomer package move laterally and pump a fluid into or out of a fluid cavity within the engine mount device to change a volume of a gas-filled space/bladder; and

wherein, when the load acts transverse to the longitudinal axis of the housing, the load is reacted by the inboard elastomer package.

18. The method of claim 17 , wherein:

the aft mount comprises a stop plate located outside of the inboard end of the housing;

the stop plate is movable laterally along with the inner lug;

the inner lug comprises an outboard stop portion located outside of an outboard end of the housing; and

a position of the inner lug is bounded by distances from the housing to the stop plate and the outboard stop portion, respectively.

19. The method of claim 17 , wherein the aft mount comprises an outboard elastomer package.