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A system and method for powering an air-drop device is presented. One configuration of the system includes an energy capture device, a generator and an electrical logic unit. The energy capture device converts the movement air passing by the air-drop tail device into kinetic energy. The generator co

A system and method for powering an air-drop device is presented. One configuration of the system includes an energy capture device, a generator and an electrical logic unit. The energy capture device converts the movement air passing by the air-drop tail device into kinetic energy. The generator converts that kinetic energy into electrical energy and the electrical logic unit can then be powered by the electrical energy allowing it to perform at least a portion of a mission.

대표청구항 ▼

1. A method comprising the steps of: providing an air-dropped device comprising a mission section, a rotational shaft extending outwardly from the mission section and a pinwheel mounted on the shaft entirely external to the mission section;dropping the air-dropped device through air to cause the pin

1. A method comprising the steps of: providing an air-dropped device comprising a mission section, a rotational shaft extending outwardly from the mission section and a pinwheel mounted on the shaft entirely external to the mission section;dropping the air-dropped device through air to cause the pinwheel to rotate; converting kinetic energy of the rotating pinwheel into electrical energy; andusing the electrical energy to power the mission section so that the mission section has power to perform at least part of a mission that the mission section is configured to perform;wherein the mission section has a front end and a back end; a plurality of fins are mounted to the mission section and extend rearward beyond the back end of the mission section; and the pinwheel includes a plurality of fan blades connected to the shaft rearward of the fins. 2. The method of claim 1 further comprising: using the shaft of the pinwheel to rotate a portion of an electrical generator to create the electrical energy. 3. The method of claim 1 further comprising: using electromagnetic induction to create the electrical energy. 4. The method of claim 1 further comprising: storing at least some of the electrical energy in an energy storage device. 5. The method of claim 1 wherein the mission section uses the electrical energy to perform at least one of: (a) adjusting the flight of the air-dropped device and (b) calculating a value and transmitting that value to a remote receiver expecting that value. 6. The method of claim 1 further comprising: preventing rotation of the mission section using stabilization fins. 7. The method of claim 1 wherein the pinwheel is rotatable about an axis and includes a plurality of fan blades; the mission section extends away from the axis; and the fan blades extend away from the axis further than does the mission section in a direction perpendicular to the axis. 8. An air-dropped device comprising: a mission section having a front end and a back end;a rotational shaft extending rearward from the back end of the mission section;a pinwheel which is mounted on the shaft rearward of the back end of the mission section;a plurality of fins mounted to the mission section adjacent the back end of the mission section extending between the mission section and the pinwheel; anda generator which creates electrical energy in response to rotation of the pinwheel;wherein the electrical energy powers the mission section. 9. The air-dropped device of claim 8 further comprising: an electrochemical storage device configured to store at least some of the electrical energy. 10. The air-dropped device of claim 8 wherein the pinwheel is rotatable about an axis extending from a center of the front end and a center of the back end. 11. The air-dropped device of claim 8 further comprising: a mission unit configured to execute a mission as the air-dropped device descends from a high altitude and/or reaches ground, wherein the pinwheel and generator are removably attached to the mission unit. 12. The air-dropped device of claim 8 wherein the mission unit is configured to perform at least one of: (a) adjusting the flight of the air-dropped device and (b) calculating a value and transmitting that value to a remote receiver expecting that value. 13. The air-dropped device of claim 8 wherein the pinwheel is rotatable about an axis and includes a plurality of fan blades; the mission section extends away from the axis; and the fan blades extend away from the axis further than does the mission section in a direction perpendicular to the axis. 14. The air-dropped device of claim 8 wherein the fins extend rearward beyond the back end of the mission section; and the pinwheel includes a plurality of fan blades connected to the shaft rearward of the fins. 15. The air-dropped device of claim 8 wherein the shaft is configured to rotate at least a portion of the generator. 16. The air-dropped device of claim 15 wherein the generator comprises: a field winding rotated by the shaft. 17. An air-dropped device comprising: a mission section having a front end and a back end;a rotational shaft extending from within the mission section and outwardly from the back end of the mission section so that the shaft extends beyond the back end of the mission section;a pinwheel which is mounted on the shaft, which is rotatable about an axis extending from the front end to the back end of the mission section, and which is entirely rearward of the back end of the mission section;a generator which creates electrical energy in response to rotation of the pinwheel;wherein a plurality of fins are mounted to the mission section and extend rearward beyond the back end of the mission section; and the pinwheel includes a plurality of fan blades connected to the shaft rearward of the fins. 18. The air-dropped device of claim 17 wherein the pinwheel is rotatable about an axis and includes a plurality of fan blades; the mission section extends away from the axis; and the fan blades extend away from the axis further than does the mission section in a direction perpendicular to the axis.