Engine with hybrid crankcase

1. An engine with a hybrid crankcase, the crankcase being a composite construction having an exoskeleton formed of a non-ferrite material having no defined endurance limit as a material, the non-ferrite exoskeleton encapsulating a load bearing skeleton formed of a ferrite material, the ferrite material having a well defined endurance limit, whereby the skeleton acts to carry the highest engine loadings, the exoskeleton being formed with a plurality of intricate ribs, the ribs acting to strengthen the engine block structure while enhancing the acoustic signature.

2. The engine of claim 1 , the exoskeleton being formed of an aluminum or magnesium alloy.

3. The engine of claim 1 , all highly loaded connections, including for main bearing caps and cylinder stud locations, being terminated in the skeleton.

4. The engine of claim 1 , the exoskeleton being formed of high thermal conductivity material for dispersing local thermal loads and for being used to sink heat as a thermal battery in adverse cooling situations.

5. The engine of claim 1 , including oil drain backs being integrated in the exoskeleton, the oil drain backs providing a cooling feature by passing the oil near a external, high-surface area, of the exoskeleton, whereby the oil drain acts as a functional enhancement to oil cooling, while aiding in engine oil supply circulation.

6. The engine of claim 1 , having a coolant circuit defined within the skeleton and a lubrication circuit defined in the skeleton, thereby separating the coolant circuit and the lubrication circuit to minimize cross-leakage which could contaminate either circuit.

7. The engine of claim 1 , including integrating a coolant jacket in the skeleton, thereby stabilizing bore dimensions and reducing engine friction and incorporating a local high-pressure sealing land therein having the strength to be able to function with the highest pressure diesel combustion.

8. The engine of claim 1 , the skeleton being re-borable per usual practice, thereby allowing the engine to have a service life past the initial design point.

9. The engine of claim 1 , the duality of the non-ferrite and the ferrite structure acting to minimize structure borne noise.

10. The engine of claim 1 , employing a pre-post casting process for bonding the exoskeleton and skeleton structures on both a microscopic and macroscopic level.

11. The engine of claim 10 , the macroscopic features being placed in such a manner as to “focus” thermally induced stress, and ensure a shared load between exoskeleton and skeleton structure castings.

12. The engine of claim 1 , wherein the mismatch of thermal expansion coefficients between the exoskeleton and skeleton structures maintains the exoskeleton structure in a thermally induced compressive state during engine operation, thereby ensuring a superior fatigue performance for the exoskeleton structure, which, structure does not have a defined endurance limit.

13. The engine of claim 1 , the skeleton structure providing a load path that promotes stress distribution within the largest mass of the engine block as a function of a length dimension and a mechanical locking feature.

14. The engine of claim 1 , the thermal conductivity of the exoskeleton being used to enhance the local properties of the skeleton structure by placing less demand on cooling system accuracy by effectively having a heat load redistribution system built into the block structure, thereby minimizing the degradation of material properties with temperature to reduce engine weight.

15. A method of forming an engine with a hybrid crankcase, including forming the crankcase of a composite construction having an exoskeleton formed of a non-ferrite material having no defined endurance limit as a material, encapsulating a load bearing skeleton formed of a ferrite material, the ferrite material having a well defined endurance limit, and to carrying the highest engine loadings by means of the skeleton, defining a coolant circuit within the skeleton and defining a lubrication circuit in the skeleton, thereby separating the coolant circuit and the lubrication circuit to minimize cross-leakage which could contaminate either circuit.

16. The method of claim 15 , including forming the exoskeleton of an aluminum or magnesium alloy.

17. The method of claim 15 , including terminating all highly loaded connections, including for main bearing caps and cylinder stud locations, in the skeleton.

18. The method of claim 15 , including forming the exoskeleton of high thermal conductivity material for dispersing local thermal loads and for being used to sink heat as a thermal battery in adverse cooling situations.