A personal air propulsion device of sophisticated design is needed to power an individual over a chosen surface. The surface might be ice, snow, water, land, pavement, or any surface chosen. The device should provide lightweight air propulsion from an internal combustion engine powering a fan. The fan drive should be stepped up from the speed of the engine's crankshaft such that increased fan speed provides greater thrust than would direct drive. Air should be guided into the device in a laminar fashion. Air should be expelled from the device in a way that further increases thrust. The fan drive of the device should be housed to avoid potential injury and to provide greater thrust. Air inlets and outlets should be screened to prevent the intrusion of foreign objects. The device should offer lighting for night use, with battery backup for the lights. The device should offer hand controls.
Further, the device should offer safety features whereby it can either be manually turned off in an instant or turned off automatically should a user fall. The present invention fulfills these needs.
The invention relates to propulsion devices, and more specifically to a personal air propulsion device for use by an individual in snow skiing, skating, bicycling, or the like.
The general purpose of the personal air propulsion device, described subsequently in greater detail, is to provide a personal air propulsion device with many novel features that result in a personal air propulsion device which is not anticipated, rendered obvious, suggested, or even implied by prior art, either alone or in combination thereof.
To accomplish this, the improved personal air propulsion device comprises a backpack frame, the exemplary frame of plastic or aluminum. The front of the frame is padded for the comfortable receipt of a user's back. A padded shoulder harness with a single buckle is attached to the front of the frame.
In one example, the invention offers arm rests that extend forward from the frame and are disposed below a user's arms. Armrests are adjustable to fit a wide range of user sizes. Handles are disposed toward the forward and upward end of each armrest. Controls for motor on/off and motor speed are fitted within one handle. A light switch is disposed within the opposite handle. Optional lights are mounted to either side and on top of the propeller drive housing. Lights are mounted atop light stalks. Lights provide for forward facing headlights and rearward facing red tail lights.
The propeller drive housing is mounted to the back of the back pack frame. The housing contains a drive pulley mounted to the motor output, a slave pulley, and the belt that rotatably connects the two. The drive belt partially encircles the drive pulley and extends downward to partially encircle the slave pulley. The slave pulley is removably attached to a propeller axle. In one example, the pulleys are sized to drive the propeller axle at twice the speed of the engine's crankshaft. Pulley sizes are varied in other examples. The propeller drive housing is accessible through the front of the backpack frame for adjustment of the pulley system. The propeller axle is supported at the backpack frame by an axle front bearing. Extending back into the propeller surround, the propeller axle is supported by a propeller axle stabilizer bearing mounted within the center of the propeller stabilizer. The propeller stabilizer is mounted within the propeller surround and thereby provides stability for the propeller axle and the propeller.
The propeller is mounted at the rear of the axle. One example of the invention uses a two-blade propeller. In yet a further example, the fan is of typical turbine fan design. Air intake shrouds are to the front of and on either side of the propeller surround. Intake shrouds further comprise a protective screening to prevent clothing and other foreign objects from being drawn into the propeller. Air is drawn into the intake shrouds via air intake cones which provide for greater and more laminar air intake. Air is pulled through the propeller surround by the propeller and exits via the air outlet cone. The air outlet cone is provided for greater directional air flow and thrust.
The gasoline engine is mounted above the propeller surround. One example utilizes a 2-cycle gasoline engine. Alloys such as aluminum are exemplified, to insure light weight of the invention. The fuel tank is of non-leak design. The drive belt is a V-belt in one example. A further example of the personal air propulsion device utilizes a toothed belt.
In yet a further example, the user handles are affixed atop ski poles. Controls for the motor and lights remain in the handles. Flexible wires connect the handles to the back pack motor and lights. In an additional example, the motor control is via unplugable wire such that excessive movement of the handle away from the backpack affects motor kill. In this way, accidents affect the kill switch to the motor. In yet a further example, the motor and light controls are sent and received via airwave signal to the back pack from the handles.
A further optional safety feature of the personal air propulsion device utilizes a pendulum emergency stop device that is housed in a small encasement mounted against the fuel tank. Other examples mount the pendulum device in various locations. The location is not critical. The orientation of the pendulum requires that the pivot be uppermost oriented, at the 12:00 position. If a user falls, a pendulum needle makes contact with a right or left contact post within the housing. Pendulum contact stops the engine.
The personal air propulsion device utilizes aluminum, plastics, composites, and a combination thereof to best achieve light weight and inexpensive production.
Thus has been broadly outlined the more important features of the personal air propulsion device so that the detailed description thereof that follows may be better understood and in order that the present contribution to the art may be better appreciated.
Numerous objects, features and advantages of the personal air propulsion device will be readily apparent to those of ordinary skill in the art upon reading the following detailed description of presently preferred, but nonetheless illustrative, embodiments of the personal air propulsion device when taken in conjunction with the accompanying drawings.
In this respect, before explaining the current embodiments of the personal air propulsion device in detail, it is to be understood that the invention is not limited in its application to the details of construction and arrangements of the components set forth in the following description or illustration. The invention is capable of other embodiments and of being practiced and carried out in various ways. It is also to be understood that the phraseology and terminology employed herein are for purposes of description and should not be regarded as limiting.
Those skilled in the art will appreciate that the conception upon which this disclosure is based may readily be utilized as a basis for the design of other structures, methods and systems for carrying out the several purposes of the personal air propulsion device. It is therefore important that the claims be regarded as including such equivalent constructions insofar as they do not depart from the spirit and scope of the present invention.
Objects of the personal air propulsion device, along with various novel features that characterize the invention are particularly pointed out in the claims forming a part of this disclosure. For better understanding of the personal air propulsion device, its operating advantages and specific objects attained by its uses, refer to the accompanying drawings and description.
With reference now to the drawings, and in particular
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With respect to the above description then, it is to be realized that the optimum dimensional relationships for the parts of the personal air propulsion device, to include variations in size, materials, shape, form, function and the manner of operation, assembly and use, are deemed readily apparent and obvious to one skilled in the art, and all equivalent relationships to those illustrated in the drawings and described in the specification are intended to be encompassed by the present invention.
Therefore, the foregoing is considered as illustrative only of the principles of the invention. Further, since numerous modifications and changes will readily occur to those skilled in the art, it is not desired to limit the invention to the exact construction and operation shown and described, and accordingly, all suitable modifications and equivalents may be resorted to, falling within the scope of the invention.
Number | Name | Date | Kind |
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1792031 | Price | Feb 1931 | A |
2509603 | Marin | May 1950 | A |
3570785 | Croft | Mar 1971 | A |
3576376 | Steeg | Apr 1971 | A |
5222569 | Martel | Jun 1993 | A |
6305048 | Salisian | Oct 2001 | B1 |