초록 ▼

The subject tiltrotor aircraft has three modes of operation: airplane mode, helicopter mode, and transition mode. A tilting mast, which transitions the aircraft between airplane mode and helicopter mode, is controlled by systems that allow selective movement of the rotor blades between the flight mo

The subject tiltrotor aircraft has three modes of operation: airplane mode, helicopter mode, and transition mode. A tilting mast, which transitions the aircraft between airplane mode and helicopter mode, is controlled by systems that allow selective movement of the rotor blades between the flight modes. A hub couples the rotor blades to the tilting mast such that torque and thrust are transferred, while allowing rotor thrust vector tilting. A main swash plate controls rotor thrust vector direction. Pitch horns are coupled to the rotor blades and the main swash plate via pitch links such that swash plate inputs are communicated to the rotor blades. The pitch links are coupled at "delta-3" values that are not optimum. A feedback swash plate and feedback links receive disk tilting inputs from the rotor blades, and supply inputs to the main swash plate, which compensates for the less than optimum delta-3 coupling.

대표청구항 ▼

The subject tiltrotor aircraft has three modes of operation: airplane mode, helicopter mode, and transition mode. A tilting mast, which transitions the aircraft between airplane mode and helicopter mode, is controlled by systems that allow selective movement of the rotor blades between the flight mo

The subject tiltrotor aircraft has three modes of operation: airplane mode, helicopter mode, and transition mode. A tilting mast, which transitions the aircraft between airplane mode and helicopter mode, is controlled by systems that allow selective movement of the rotor blades between the flight modes. A hub couples the rotor blades to the tilting mast such that torque and thrust are transferred, while allowing rotor thrust vector tilting. A main swash plate controls rotor thrust vector direction. Pitch horns are coupled to the rotor blades and the main swash plate via pitch links such that swash plate inputs are communicated to the rotor blades. The pitch links are coupled at "delta-3" values that are not optimum. A feedback swash plate and feedback links receive disk tilting inputs from the rotor blades, and supply inputs to the main swash plate, which compensates for the less than optimum delta-3 coupling. im 1, further comprising a perforated stabilizing plate, through which the fuel can flow and which is made from metal and is arranged on an outflow side of the filter element. 4. Injection valve according to claim 1, wherein the ducts have a diameter of between 10 μm and 1000 μm. 5. Injection valve according to claim 1, wherein the ducts have a diameter of between 20 μm and 500 μm. 6. Injection valve according to claim 1, wherein the ducts have a diameter of between 20 μm and 200 μm. 7. Injection valve according to claim 1, further comprising a web between two adjacent ducts, wherein the web has a wall thickness between 10 μm and 200 μm. 8. Injection valve according to claim 1, further comprising a web between two adjacent ducts, wherein the web has a wall thickness between 20 μm and 100 μm. 9. Injection valve according to claim 1, wherein a length of the ducts is between 10 μm and 1000 μm. 10. Injection valve according to claim 1, wherein a length of the ducts is between 50 μm and 500 μm. 11. Injection valve according to claim 1, wherein a length of the ducts is between 100 μm and 300 μm. 12. Injection valve according to claim 1, wherein the filter element has a plurality of semiconductor boards arranged one behind the other and provided with ducts. 13. Injection valve according to claim 1, wherein the filter element is thermally insulated in relation to the housing of the injection valve. 14. Injection valve for internal combustion engines, comprising a filter element arranged inside the injection valve in fuel flow, the filter element including ducts for the fuel flow and a heating element, wherein regions of walls of the ducts are capable of being heated along longitudinal extent of the walls, and wherein the filter element has a semiconducting material at least in a vicinity of the fuel flow. 15. Injection valve according to claim 14, wherein the semiconducting material includes silicon at least in the vicinity of the fuel flow. 16. Injection valve according to claim 14, wherein the semiconducting material includes a conductive aluminium metal. 17. Injection valve according to claim 14, further comprising a perforated stabilizing plate, through which the fuel can flow and which is made from metal and is arranged on an outflow side of the filter element. 18. Injection valve according to claim 14, wherein the ducts have a diameter of between 10 μm and 1000 μm. 19. Injection valve according to claim 14, wherein the ducts have a diameter of between 20 μm and 500 μm. 20. Injection valve according to claim 14, wherein the ducts have a diameter of between 20 μm and 200 μm. 21. Injection valve according to claim 14, further comprising a web between two adjacent ducts, wherein the web has a wall thickness between 10 μm and 200 μm. 22. Injection valve according to claim 14, further comprising a web between two adjacent ducts, wherein the web has a wall thickness between 20 μm and 100 μm. 23. Injection valve according to claim 14, wherein a length of the ducts is between 10 μm and 1000 μm. 24. Injection valve according to claim 14, wherein a length of the ducts is between 50 μm and 500 μm. 25. Injection valve according to claim 14, wherein a length of the ducts is between 100 μm and 300 μm. 26. Injection valve according to claim 14, wherein the filter element has a plurality of semiconductor boards arranged one behind the other and provided with ducts. 27. Injection valve according to claim 14, wherein the filter element is thermally insulated in relation to a housing of the injection valve. air flow in an attached hose, liquid in a tank is sucked up to mix with the high speed air jet stream at the inside of a blow head to force an atomized cleaner or paint jet stream to blow out. A nozzle carrier rotates freely to allow the attached hose to hang beneath the air gun body, so as to provide for ease of operation of the gun.