Wingtip and sponson interaction on an amphibious aircraft
A system for enhanced lateral stability of an amphibious aircraft includes a buoyancy system laterally displaced from opposite sides of the fuselage of the aircraft and wingtip system having a hydrodynamic planing surface associated with each wingtip. The hydrodynamic planing surface on each wingtip prevents the submersion of an associated buoyancy structure. By supplementing the lateral stability of the buoyancy structures using hydrodynamic planing surfaces, the combined lateral width of the fuselage and buoyancy structures can be reduced without detrimentally impacting operational performance. This reduced lateral width enables the amphibious aircraft to be configured for storage and transportation on a trailer or shipping container.
1. A method for enhancing lateral stability of an amphibious aircraft on a body of water, the method comprising;
displacing a buoyancy system laterally from a fuselage of the amphibious aircraft sufficient to maintain static lateral stability wherein the buoyancy system includes a hydrodynamic step; and
responsive to a wingtip of the amphibious aircraft engaging the body of water while the amphibious aircraft is in motion, producing a dynamically increasing righting force augmenting lateral stability of the amphibious aircraft.
2. The method for enhancing lateral stability according to claim 1 wherein the dynamically increasing righting force opposes a submersion force associated with the buoyancy system when at least a portion of the buoyancy system is submerged.
3. The method for enhancing lateral stability according to claim 1 wherein the wingtip possesses a tip dihedral orientation and a positive angle of incidence such that upon contact with the body of water at least one hydrodynamic planing surface of the wingtip is substantially parallel with the body of water.
4. The method for enhancing lateral stability according to claim 1 wherein the wingtip is an anhedral wingtip possessing a tip dihedral orientation with a hydrodynamic planing surface such that upon interaction with the body of water the hydrodynamic planing surface is substantially parallel with a water surface of the body of water.
5. The method for enhancing lateral stability according to claim 1 wherein the dynamically increasing righting force is substantially perpendicular to the body of water.
6. The method for enhancing lateral stability according to claim 1 wherein interaction between the buoyancy system and the wingtip provides dynamic lateral stability.
7. The method for enhancing lateral stability according to claim 1 wherein the wingtip is located at each of opposite ends of a polyhedral wing.
8. A method for dynamic lateral stability of an amphibious aircraft, comprising;
providing by a buoyancy system having a hydrodynamic step laterally displaced from a fuselage of the amphibious aircraft static lateral stability; and
responsive to a wingtip located at each end of a polyhedral wing of the amphibious aircraft interacting with a surface of a body of water while the amphibious aircraft is in motion, creating a dynamically increasing righting force substantially perpendicular to the surface of the body of water sufficient to provide dynamic lateral stability.
9. The method for dynamic lateral stability of claim 8 wherein the wingtip is an anhedral wingtip possessing a tip dihedral orientation.
10. The method for dynamic lateral stability of claim 9 wherein the wingtip includes a hydrodynamic planing surface with a positive angle of incidence.
11. The method for dynamic lateral stability of claim 10 wherein the dynamically increasing righting force is proportional to displacement of the hydrodynamic planing surface and speed of the amphibious aircraft.
12. A method for dynamically stabilizing an amphibious aircraft by augmenting lateral stability of a buoyancy system laterally displaced from a fuselage of the amphibious aircraft wherein augmenting includes forming a righting force substantially perpendicular to a surface of a body of water at a wingtip of the amphibious aircraft, the righting force being proportional to speed of the amphibious aircraft and displacement of the wingtip in the body of water.
13. The method for dynamically stabilizing an amphibious aircraft of claim 12 wherein interaction between the buoyancy system and wingtip makes the amphibious aircraft laterally stable while the amphibious aircraft is in motion.
14. The method for dynamically stabilizing an amphibious aircraft of claim 12 wherein the wingtip has an anhedral configuration and is associated with a polyhedral wing, the wingtip further possessing a positive angle of incidence with at least one hydrodynamic planing surface.
15. The method for dynamically stabilizing an amphibious aircraft of claim 14 wherein the at least one hydrodynamic planing surface includes a tip dihedral orientation such that upon rolling of the amphibious aircraft sufficient for the wingtip to make contact with the body of water the at least one hydrodynamic planing surface is substantially parallel with body of water.
16. A stability system for an amphibious, the system comprising:
a sponson laterally displaced from a fuselage of the amphibious aircraft wherein the sponson includes a hydrodynamic step; and
a planning surface on each wingtip of a polyhedral wing wherein interaction between the sponson and the planning surface is operable to provide static and dynamic waterborne stability.
17. The stability system of claim 16 wherein the sponson is operable to provide static stability.
18. The stability system of claim 16 wherein the planning surface augments dynamic stability.
19. The stability system of claim 16 wherein upon the planning surface contacting a water surface the planning surface is substantially parallel with the water surface.
20. The stability system of claim 19 wherein the planning surface includes a hydrodynamic step.
21. The stability system of claim 19 wherein increased dynamic submersion downward force of the planning surface results in a proportional opposite increase in an righting force.
22. The stability system of claim 19 wherein the planning surface includes a positive angle of inclination upon interaction with the water surface.
23. The stability system of claim 19 wherein interaction of the planning surface with a water surface prevents submersion of the sponson.
24. A dynamic lateral stability system for an amphibious aircraft, comprising:
a planning surface positioned at each wingtip of a polyhedral wing wherein interaction of the planning surface with a water surface while the amphibious aircraft is in motion supplements lateral stability of a laterally displaced sponson, the laterally displaced sponson being associated with a fuselage of the amphibious aircraft and having a hydrodynamic step.
25. The dynamic lateral stability system of claim 24 wherein the planning surface and the laterally displaced sponson interact to provide dynamic and static stability for the amphibious aircraft during substantially all waterborne operations.
26. The dynamic lateral stability system of claim 24 wherein the planning surface includes a hydrodynamic step.
27. The dynamic lateral stability system of claim 24 wherein responsive to a lateral displacement of the amphibious aircraft resulting in contact of one of the wingtips with the water surface, the planning surface interface with the water surface is substantially laterally parallel with a positive longitudinal inclination.
28. The dynamic lateral stability system of claim 24 wherein interaction of the planning surface with the water surface creates a righting force substantially perpendicular to the water surface.
29. The dynamic lateral stability system of claim 24 wherein a leading edge of the planning surface possesses a positive inclination with respect to the trailing edge of the planning surface.