초록 ▼

A method of generating energy from a discharge of an aircraft comprising the steps of: a) providing an air recovery generator assembly having a bladed wheel; and, b) positioning the air recovery generator behind the aircraft. The discharged air from the aircraft then turns the wheel thereby generati

A method of generating energy from a discharge of an aircraft comprising the steps of: a) providing an air recovery generator assembly having a bladed wheel; and, b) positioning the air recovery generator behind the aircraft. The discharged air from the aircraft then turns the wheel thereby generating energy. In a preferred aspect of this invention the bladed wheel comprises a bladed cylinder wheel and the bladed cylindrical wheel additionally rotates a flywheel to store rotational energy therein. A mechanism is provided to move the bladed cylindrical wheel from a below ground storage position to an elevated operational position.

대표청구항 ▼

What is claimed is: 1. A method of generating electrical energy on the ground from a discharge of an aircraft comprising the steps of: a) providing an air recovery generator assembly having a bladed wheel; and, b) positioning the air recovery generator behind the aircraft on the ground; so that di

What is claimed is: 1. A method of generating electrical energy on the ground from a discharge of an aircraft comprising the steps of: a) providing an air recovery generator assembly having a bladed wheel; and, b) positioning the air recovery generator behind the aircraft on the ground; so that discharged air from the aircraft turns the wheel thereby generates electrical energy on the ground. 2. A method as in claim 1 wherein the bladed wheel comprises a bladed cylinder wheel. 3. A method as in claim 2 wherein the bladed cylindrical wheel additionally rotates a flywheel to store rotational energy therein. 4. A method as in claim 2 further comprising a mechanism to move the bladed cylindrical wheel from a below ground storage position to an elevated operational position. 5. A method as in claim 4 wherein the mechanism is covered by a grate so that a flat supporting surface is presented above the bladed cylindrical wheel when it is in a retracted position and so that discharged air can pass through the grate when it is in an elevated position. 6. A method as in claim 5 wherein the grate is hinged on a rear side portion so that if the grate was inadvertently left open it would close when an aircraft rolled forwardly thereover. 7. A method as in claim 6 wherein the bladed cylindrical wheel is carried by a lower front side portion of the grate and wherein the generator and flywheel are carried attached to a lower rear side portion of the grate so that when the grate is lifted the bladed wheel is also lifted. 8. A method as in claim 7 wherein the grate is hinged along a rear side portion so that the front side portion of the grate can be swung upwardly lifting the upper side portion of the bladed cylindrical wheel above ground to the elevated operational position. 9. A method as in claim 8 wherein the grate is provided with a remotely controlled lift mechanism. 10. A method as in claim 8 further comprising a grate counterweight so that the lift required to elevate the grate to the operational position is minimized. 11. A method as in claim 10 further comprising a wind catching blade attached along a front side portion of the grate so that discharged air from the aircraft will automatically elevate the grate to an operational position. 12. A method as in claim 8 further comprising a governor/clutch assembly mechanically attached to a shaft of the bladed cylindrical wheel on one end and a secondary flywheel on the other end to limit the speed of the bladed cylindrical wheel when required. 13. A method as in claim 8 further comprising additional jet air recovery generator assemblies spaced along the runway.