초록 ▼

A split fan for providing lift for an aircraft is described. In one embodiment, a main engine shaft extends to the split fan, and a portion of the split fan is located at an elevation above the main engine shaft and a portion of the split fan is located at an elevation below the main engine shaft. I

A split fan for providing lift for an aircraft is described. In one embodiment, a main engine shaft extends to the split fan, and a portion of the split fan is located at an elevation above the main engine shaft and a portion of the split fan is located at an elevation below the main engine shaft. In the one embodiment, the split fan includes an outer casing configured to be mounted to a fuselage of the aircraft, a first stage rotor including a shaft, a gear secured to the shaft, and a plurality of rotor blades radially extending from the shaft. The split fan also includes a second stage rotor including a shaft, a gear secured to the shaft, and a plurality of blades radially extending from the shaft. A drive shaft having a first end and a second end is coupled at the drive shaft first end to the main engine shaft. A drive gear is located at the second end of the drive shaft, and the first stage rotor gear and the second stage rotor gear are coupled to the drive gear so that as the drive gear rotates, the first stage rotor gear rotates in a first direction and the second stage rotor gear rotates in a second direction.

대표청구항 ▼

[ What is claimed is:] [1.] A split fan for providing lift for aircraft, said split fan comprising:an outer casing configured to be mounted to a fuselage of the aircraft;a first stage rotor comprising a shaft, a gear secured to said shaft, and a plurality of rotor blades radially extending from said

[ What is claimed is:] [1.] A split fan for providing lift for aircraft, said split fan comprising:an outer casing configured to be mounted to a fuselage of the aircraft;a first stage rotor comprising a shaft, a gear secured to said shaft, and a plurality of rotor blades radially extending from said shaft;a second stage rotor comprising a shaft, a gear secured to said shaft, and a plurality of blades radially extending from said shaft;a drive shaft comprising a first end and a second end, said drive shaft first end configured to be coupled to a main engine shaft so that when said main engine shaft rotates, said drive shaft rotates;a drive gear at said second end of said drive shaft, said first stage rotor gear and said second stage rotor gear coupled to said drive gear so that as said drive gear rotates, said first stage rotor gear rotates in a first direction and said second stage rotor gear rotates in a second direction.