Gyroscope device for creating a precession torque
The present invention is a device for generating a precession torque for transmission to an attached object. The present invention includes a motor mounted to a base and a gyroscope device. The gyroscope device includes a drive gimbal with a substantially planar drive gimbal bevel gear. A gyro gimbal is coupled to the motor to spin the gyro gimbal about a gyro gimbal axis substantially perpendicular to the plane of the drive gimbal bevel gear. A gyro simultaneously rotating about the gyro gimbal axis and spinning about a moving gyro spin axis creates a precession torque about a precession torque axis mutually orthogonal to the moving gyro spin axis and the gyro gimbal axis.
The present application is a continuation-in-part of U.S. patent application Ser. No. 10/309,734, entitled “Torque Induced Propulsion System,” filed Dec. 13, 2002 by Applicant herein, and issued Mar. 1, 2005 as U.S. Pat. No. 6,860,166.
FIELD OF THE INVENTIONThis invention relates to gyroscope devices. Specifically, the present invention is a gyroscope device in which a motor turning a gyro generates a precession torque that can be imparted to an object.
BACKGROUND OF THE INVENTIONTraditionally, machines that produce thrust or provide propulsion for aerial vehicles do so by either pushing against the air the way airplanes, jets, or helicopters do, or by expelling burned fuel the way rockets do. Many patents have been filed for propulsion systems that do not work in this conventional fashion. Many of these patents work against gyros to generate propulsion.
Patents such as U.S. Pat. No. 5,860,317 to Laithwaite (1999), U.S. Pat. No. 5,024,112 to Kidd (1991), UK patent 2,090,404 to Russell (1982), all describe gyro-based propulsion systems that have an excessive number of moving parts, U.S. Pat. No. 5,054,331 to Rogers (1991), UK patent 205,753 to Morgan (1988), U.S. Pat. No. 5,090,260 to Delroy (1992), and Japanese patent 60-56182 to Kiyunmeru (1985), also have the same problem. This adds unnecessary weight, decrease energy efficiency, and give cause for concern of mechanical breakdown. In addition, these overly complex machines seem unnecessarily expensive to build, making them impractical for manufacturing.
Propulsion system patents using principles other than gyros that claim to be able to produce the same type of propulsion (without expelling expended fuel or pushing against the medium through which they travel) suffer from the same problems of over complexity. Examples of these patents are U.S. Pat. No. 4,712,439 to North (1987), U.S. Pat. No. 4,409,856 to De Weaver (1983), U.S. Pat. No. 4,479,396 to De Weaver (1984), U.S. Pat No. 5,150,626 to Nevarro (1992), U.S. Pat. No. 5,182,958 to Black (1993), U.S. Pat. No. 5,791,188 to Howard (1998), and U.S. Pat. No. 5,966,986 to Laul (1999).
SUMMARY OF THE INVENTIONIn one embodiment, the present invention is a gyroscope device that uses the spin and precession of a gyro while revolving around an axis to generate a precession torque that is transmitted to an object. In another embodiment, the present invention is a gyroscope system that uses the spin and precession of at least two sets of two gyros each rotating on two axes while revolving around a third axis to generate pulses of torque from the resulting gyro precession to propel a machine by rotating it around two axes alternately.
In a first aspect of the present invention, a motor is mounted to a base. The base may take any form, but is optionally an object to which a precession torque is to be applied. The motor turns an axle.
A gyroscopic device is coupled to rotate about the axle. The gyroscopic device includes a drive gimbal, a gyro gimbal, and a gyro. The drive gimbal includes a substantially planar drive gimbal bevel gear. Optionally, the drive gimbal is coupled to the axle to permit rotation of the gyroscopic device about the axle by the motor.
The gyro gimbal is coupled to the motor such that the motor drives the gyro gimbal to spin continuously and completely about a gyro gimbal axis. The gyro gimbal axis is substantially perpendicular to the plane formed by the drive gimbal bevel gear.
The gyro is coupled to, and guided by, the drive gimbal bevel gear such that the gyro is caused to spin when the motor drives the gyro gimbal to spin. In this manner, the gyro simultaneously rotates about the gyro gimbal axis and spins about a moving gyro spin axis in a plane substantially parallel to the plane of the drive gimbal bevel gear. As a consequence of the gyro rotation and spin, a precession torque is generated about a precession torque axis. The precession torque axis is mutually orthogonal to the moving gyro spin axis and the gyro gimbal axis. The precession torque is transmitted to the base.
In a second aspect of the present invention, a motor drives an axle coupled to four gyroscopic devices. As above, each of a first gyroscopic device, a second gyroscopic device, a third gyroscopic device, and a fourth gyroscopic device are rotated about the axle.
A first gyroscopic device includes a first drive gimbal with a substantially planar first drive gimbal bevel gear. A first gyro gimbal is coupled to the motor and is driven by the motor to spin continuously and completely about a first gyro gimbal axis that is substantially perpendicular to the plane of the first drive gimbal bevel gear. A first gyro simultaneously rotates about the first gyro gimbal axis and spins about a first moving gyro spin axis that is in a plane substantially parallel to the plane of the first drive gimbal bevel gear. The spin of the first gyro is coupled to, and guided by the first drive gimbal bevel gear, such that the first gyro is caused to spin when the motor drives the first gyro gimbal to spin. The first gyro rotation and spin generates a first precession torque about a moving first precession torque axis that is mutually orthogonal to the first moving gyro spin axis and the first gyro gimbal axis;
A second gyroscopic device includes a second drive gimbal with a substantially planar second drive gimbal bevel gear. A second gyro gimbal driven by the motor to spin continuously and completely about a second gyro gimbal axis that is substantially perpendicular to the plane of the second drive gimbal bevel gear. The second gyro gimbal axis is substantially parallel to the first gyro gimbal axis but the spin of the second gyro gimbal is substantially opposite the spin of the first gyro gimbal. A second gyro simultaneously rotates about the second gyro gimbal axis and spins about a second moving gyro spin axis in a plane substantially parallel to the plane of the second drive gimbal bevel gear. The spin of the second gyro is coupled to, and guided by, the second drive gimbal bevel gear such that the second gyro is caused to spin when the motor drives the second gyro gimbal to spin. The second gyro rotation and spin generates a second precession torque about a moving second precession torque axis that is mutually orthogonal to the second moving gyro spin axis and the second gyro gimbal axis.
A third gyroscopic device includes a third drive gimbal having a substantially planar third drive gimbal bevel gear. A third gyro gimbal is driven by the motor to spin continuously and completely about a third gyro gimbal axis substantially perpendicular to the plane of the third drive gimbal bevel gear and is substantially perpendicular to the first gyro gimbal axis. A third gyro simultaneously rotates about the third gyro gimbal axis and spins about a third moving gyro spin axis in a plane substantially parallel to the plane of the third drive gimbal bevel gear. The spin of the third gyro is coupled to, and guided by, the third drive gimbal bevel gear such that the third gyro is caused to spin when the motor drives the third gyro gimbal to spin. The third gyro rotation and spin generates a third precession torque about a third precession torque axis mutually orthogonal to the third moving gyro spin axis and the third gyro gimbal axis.
A fourth gyroscopic device includes a fourth drive gimbal with a substantially planar fourth drive gimbal bevel gear. A fourth gyro gimbal is coupled to the motor such that the fourth gyro gimbal driven by the motor to spin continuously and completely about a fourth gyro gimbal axis substantially perpendicular to the plane of the fourth drive gimbal bevel gear. The fourth gyro gimbal axis is substantially parallel to the third gyro gimbal axis, but the spin of the fourth gyro gimbal substantially opposite the spin of the third gyro gimbal. A fourth gyro simultaneously rotates about the fourth gyro gimbal axis and spins about a fourth moving gyro spin axis in a plane substantially parallel to the plane of the fourth drive gimbal bevel gear. The spin of the fourth gyro is coupled to, and guided by, the fourth drive gimbal bevel gear such that the fourth gyro is caused to spin when the motor drives the fourth gyro gimbal to spin. The fourth gyro rotation and spin generates a fourth precession torque about a fourth precession torque axis mutually orthogonal to the fourth moving gyro spin axis and the fourth gyro gimbal axis. The first precession torque, second precession torque, third precession torque, and fourth precession torque are transmitted to the base.
BRIEF DESCRIPTION OF THE DRAWINGS
Reference is now made to the figures wherein like parts are referred to by like numerals throughout. Referring first to
It is contemplated that the action in
Turning to
The present invention is a device for creating the torque forces as the result of the precession of a gyroscope device, shown in
In such an optional embodiment, an axle 42 has a keyway 44 for a key 46 that secures a flywheel 48 to the axle 42. Washers 50 are then placed around the axle 42 on both sides of a flywheel 48 and held in place with snap rings 52 in axle slots 54, 56. In this optional embodiment, snap rings 52 are also placed in the next set of axle slots 58, 60, followed by washers 50 to support bearings 62. The bearings 62 are adjacent another set of washers 50, which are in turn adjacent additional snap rings 52 in the next set of axle slots 64, 66 to fix the position of the bearings 62. The optional embodiment illustrated includes a bevel pinion 68 and weight 70 that are then placed on the axle 42 and secured with snap rings 72 in the outermost axle grooves 74, 76.
The gyroscope device also includes a gyro gimbal 78. As described in greater detail below, the gyro gimbal 78 supports and imparts rotational motion to the gyro 40. In one optional embodiment, the gyro gimbal 78 is constructed from a single piece of material. In another optional embodiment, illustrated in
The gyro 40 and gyro gimbal 78 are assembled such that the gyro gimbal 78 may impart rotational movement to the gyro 40 and, once the drive gimbal is engaged to the gyro 40 in a manner described in greater detail below, the rotational movement of the gyro 40 may be translated to spinning movement of the gyro 40.
An optional embodiment of an assembly of the gyro 40 and the gyro gimbal 78 is shown in
More specifically, illustrated in
According to one aspect of an embodiment of the present invention, a system of gyroscope devices may be used in combination. One optional embodiment is shown in
In the optional embodiment illustrated in
In
Turning to
Thus, according to this optional embodiment, the precession torques 112, 122 alternately reinforce and cancel one another out with each one hundred-eighty degree rotation as illustrated in
Turning to
Each gyroscope device also includes a drive gimbal 134. For example,
With reference to
The drive gimbals 134 are optionally mounted to a drive assembly 144. One optional embodiment of a drive assembly 144 adapted for the optional embodiment of
Referring to
With continued reference to
It is specifically contemplated that any gear, chain, belt, or other means of transmitting motion may be used to spin and rotate the gyro 40 in the desired direction to generate a precession torque. For example, in an alternate optional embodiment, shown in
Referring to
Illustrated in
A drive assembly according to an alternate embodiment of the present invention is shown in
Illustrated in
An optional embodiment of a frame for supporting the drive assembly of
While certain embodiments of the present invention have been shown and described it is to be understood that the present invention is subject to many modifications and changes without departing from the spirit and scope of the claims presented herein.
Claims
1. A device comprising:
- a base;
- a motor mounted on said base, said motor driving an axle;
- a gyroscopic device coupled to rotate about said axle, comprising: a drive gimbal including a substantially planar drive gimbal bevel gear; a gyro gimbal coupled to said motor, said gyro gimbal driven by said motor to spin continuously and completely about a gyro gimbal axis substantially perpendicular to the plane of said drive gimbal bevel gear; and a gyro simultaneously rotating about said gyro gimbal axis and spinning about a moving gyro spin axis in a plane substantially parallel to the plane of said drive gimbal bevel gear, the spin of said gyro coupled to and guided by said drive gimbal bevel gear such that said gyro is caused to spin when said motor drives said gyro gimbal to spin, the gyro rotation and spin generating a precession torque about a precession torque axis mutually orthogonal to said moving gyro spin axis and said gyro gimbal axis that is transmitted to said base.
2. A device comprising:
- a base;
- a motor mounted to said base, said motor driving an axle;
- a gyroscopic device coupled to rotate about said axle, comprising: a drive gimbal including a substantially planar drive gimbal bevel gear, said drive gimbal rotated about said axle by said motor; a gyro gimbal coupled to said motor to spin said gyro gimbal continuously and completely about a gyro gimbal axis substantially perpendicular to the plane of said drive gimbal bevel gear; a gyro rotating about said gyro gimbal axis and spinning about a moving gyro spin axis in a plane substantially parallel to the plane of said drive gimbal bevel gear, said gyro coupled to said drive gimbal bevel gear and said gyro gimbal to cause said gyro to rotate about said gyro gimbal axis and spin about said gyro spin axis when said gyro gimbal is spun, the direction of the gyro rotation and spin generating a precession torque about a precession torque axis mutually orthogonal to said moving gyro spin axis and said gyro gimbal axis that is transmitted to said base.
3. A system comprising:
- a base;
- a motor mounted on said base, said motor driving an axle;
- a first gyroscopic device coupled to rotate about said axle, comprising: a first drive gimbal including a substantially planar first drive gimbal bevel gear; a first gyro gimbal coupled to said motor, said first gyro gimbal driven by said motor to spin continuously and completely about a first gyro gimbal axis substantially perpendicular to the plane of said first drive gimbal bevel gear; and a first gyro simultaneously rotating about said first gyro gimbal axis and spinning about a first moving gyro spin axis in a plane substantially parallel to the plane of said first drive gimbal bevel gear, the spin of said first gyro coupled to and guided by said first drive gimbal bevel gear such that said first gyro is caused to spin when said motor drives said first gyro gimbal to spin, the first gyro rotation and spin generating a first precession torque about a moving first precession torque axis mutually orthogonal to said first moving gyro spin axis and said first gyro gimbal axis;
- a second gyroscopic device coupled to rotate about said axle, comprising: a second drive gimbal including a substantially planar second drive gimbal bevel gear; a second gyro gimbal coupled to said motor, said second gyro gimbal driven by said motor to spin continuously and completely about a second gyro gimbal axis substantially perpendicular to the plane of said second drive gimbal bevel gear, said second gyro gimbal axis substantially parallel to said first gyro gimbal axis and the spin of said second gyro gimbal substantially opposite the spin of said first gyro gimbal; and a second gyro simultaneously rotating about said second gyro gimbal axis and spinning about a second moving gyro spin axis in a plane substantially parallel to the plane of said second drive gimbal bevel gear, the spin of said second gyro coupled to and guided by said second drive gimbal bevel gear such that said second gyro is caused to spin when said motor drives said second gyro gimbal to spin, the second gyro rotation and spin generating a second precession torque about a moving second precession torque axis mutually orthogonal to said second moving gyro spin axis and said second gyro gimbal axis;
- a third gyroscopic device coupled to rotate about said axle, comprising: a third drive gimbal including a substantially planar third drive gimbal bevel gear; a third gyro gimbal coupled to said motor, said third gyro gimbal driven by said motor to spin continuously and completely about a third gyro gimbal axis substantially perpendicular to the plane of said third drive gimbal bevel gear, said third gyro gimbal axis substantially perpendicular to said first gyro gimbal axis; and a third gyro simultaneously rotating about said third gyro gimbal axis and spinning about a third moving gyro spin axis in a plane substantially parallel to the plane of said third drive gimbal bevel gear, the spin of said third gyro coupled to and guided by said third drive gimbal bevel gear such that said third gyro is caused to spin when said motor drives said third gyro gimbal to spin, the third gyro rotation and spin generating a third precession torque about a moving third precession torque axis mutually orthogonal to said third moving gyro spin axis and said third gyro gimbal axis; and
- a fourth gyroscopic device coupled to rotate about said axle, comprising: a fourth drive gimbal including a substantially planar fourth drive gimbal bevel gear; a fourth gyro gimbal coupled to said motor, said fourth gyro gimbal driven by said motor to spin continuously and completely about a fourth gyro gimbal axis substantially perpendicular to the plane of said fourth drive gimbal bevel gear, said fourth gyro gimbal axis substantially parallel to said third gyro gimbal axis and the spin of said fourth gyro gimbal substantially opposite the spin of said third gyro gimbal; and a fourth gyro simultaneously rotating about said fourth gyro gimbal axis and spinning about a fourth moving gyro spin axis in a plane substantially parallel to the plane of said fourth drive gimbal bevel gear, the spin of said fourth gyro coupled to and guided by said fourth drive gimbal bevel gear such that said fourth gyro is caused to spin when said motor drives said fourth gyro gimbal to spin, the fourth gyro rotation and spin generating a fourth precession torque about a moving fourth precession torque axis mutually orthogonal to said fourth moving gyro spin axis and said fourth gyro gimbal axis, said first precession torque, second precession torque, third precession torque, and fourth precession torque transmitted to said base.
Type: Application
Filed: Feb 28, 2005
Publication Date: Aug 4, 2005
Inventor: Nathaniel Hintz (Las Vegas, NV)
Application Number: 11/068,698