1. Field of the Invention
The present invention generally relates to an exercise device and methods for use. More particularly, a first aspect of the present invention relates to an exercise device, which has loads applied by both a vacuum cylinder and a flywheel. This first aspect of the present invention is useful in zero or micro gravity for simulating lifting weights under normal gravity conditions and also has terrestrial application advantages. A second aspect of the present invention relates to an exercise device, which has a vacuum cylinder and a load adjusting armbase assembly.
2. Description of the Related Art
Numerous exercise devices have been designed and are on the market. The vast majority of these devices are designed for normal gravity conditions. For example, many devices have been developed of the “weight type” wherein weights are employed in the resistance to the exertion of muscular force. Perhaps the simplest of these are barbells, but a host of machines of this type have been developed which employ weight stacks of a variety of types against which muscular force is exerted in exercising to achieve or maintain muscular development. Machines of the “weight type” suffer from several common deficiencies, which detract from their desirability.
Such machines are normally rather cumbersome and expensive. They do not possess the fidelity of adjustability (i.e., they are limited to the weight stack increments). Perhaps the most obvious aspect of these types of devices is that they are very heavy due to the inherent nature of the use of weight stacks.
The following patents disclose prior art efforts related to the above-described and/or other problems and studies:
U.S. Pat. No. 4,257,593, issued May 24, 1981, to Keiser discloses an exercising device that employs pneumatics in creating resistance to the muscular force exerted during the exercising operation. Keiser's pneumatic system includes an external source of compressed gas, such as compressed air, a reservoir having an internal chamber of adjustable capacity connecting in receiving relation to the gas from the external source, and a means for selecting the volume of the gas in the reservoir.
U.S. patent application Ser. No. 09/945,026, filed Aug. 31, 2001, to Keiser discloses an exercising device that employs pneumatics in creating resistance to the muscular force exerted during an exercising operation that permits upper and lower body musculature to be exercised simultaneously. Keiser's pneumatic system includes a major and minor pneumatic cylinder assembly, an air compressor, an air compressor accumulator, and pneumatic circuit for interconnectivity purposes. As with '593 to Keiser, this design relies on an external source of compressed gas and a gas reservoir.
U.S. patent application Ser. No. 09/931,142, filed Aug. 16, 2001, to Colosky Jr., et al. discloses a gravity-independent exercise unit designed for use in micro gravity, or on the ground, as a means by which to counter muscle atrophy and bone degradation due to disuse or misuse. Colosky's exercise device utilizes at least one modular resistive “pack,” each pack containing at least one constant force torque spring. Each torque spring is “wound up” upon a separate storage drum within the pack and each spring is attached to a single output drum. Each output drum is attached to an output shaft and each output shaft is mechanically connected to a cable drum. There is also a series of mechanical selection devices to select the amount of resistance. The unit is compact and of low mass. However, the complexity and number of internal mechanisms necessary for Colosky's design is less than optimal. Hence, maintenance issues arise, particularly in a micro gravity environment wherein it is undesirable to have a large number of internal parts with the potential of these parts “floating” around in an unmanageable manner.
U.S. Pat. No. 5,226,867, issued Jul. 13, 1993, to Beal discloses a user-manipulated modular exercise machine with two reel assemblies, each including a spirally-wound spring with applies to the real a reactive torque of changing magnitude as the reel rotates in response to pulling input forces applied to a pull-cord by the user. A cam-operated spring compensating mechanism provides for essentially a constant force during operations in various exercise modes.
There are a number of shortcomings with the prior art exercise devices, and particularly those designed for use in zero or micro gravity. Exercise devices for use in space should be compact with minimal mass and mechanical parts, provide for a large number of different exercises, be adjustable for different loads, be adjustable for different sized individuals, operate for long periods with minimal maintenance, and produce a measurable constant force during exercise. Also, it is preferred that the exercise device simulates exercising under normal gravity conditions wherein all of the aforementioned characteristics are applicable. Prior art exercise devices have failed to meet these criteria.
Accordingly, a need has arisen for an exercise device for zero or micro gravity conditions which, for example, simulates the lifting of free weights in a 1-g environment and which is compact with relatively low mass, provides for numerous different exercises, is adjustable for different loads, is adjustable for different sized individuals and will operate for long periods with minimal maintenance.
In accordance with the present invention, an exercise device is provided which has loads applied by both a vacuum cylinder and a flywheel. When used in a space application, this device simulates the lifting of free weights in a 1-g environment.
Also in accordance with the present invention, an exercise device is provided which comprises a vacuum cylinder and a load adjusting armbase assembly.
Accordingly, an object of the present invention is to provide an exercise device for space application, which simulates the lifting of free weights in a 1-g environment.
Accordingly, a second object of the present invention is to provide an exercise device having a vacuum cylinder and a unique load-adjusting feature, which varies the otherwise constant load provided by a vacuum cylinder.
A third object of the present invention is to provide an improved exercising apparatus for terrestrial applications such as, for examples: a home gym for personal use; rehabilitation and physical therapy purposes; and an exercise device for a health club, hotel, or cruise ship.
Further objects and advantages are to provide improved elements and arrangements thereof in an exercise apparatus for the purpose described which is dependable, economical, durable, and fully effective in accomplishing the intended purpose.
A better understanding of the invention can be obtained when the detailed description of exemplary embodiments set forth below is considered in conjunction with the attached drawings in which:
The present invention relates to an exercise device 10, which has loads applied by both a vacuum cylinder 30 and a flywheel 40. As shown in
In an embodiment, the exercise device's 10 main load is a pair of 8-inch internal diameter vacuum cylinders 30. However, any size vacuum cylinder can be used such that the size is commensurate with the overall design of an exercise device consistent with the elements described herein. The vacuum cylinders 30 provide the necessary resistance for exercise. The vacuum cylinders 30 operatively connect to the frame 20 and to the armbase assembly 50. The flywheel's 40 purpose is to provide the user 11 with the inertial component of free weight exercise, which is currently absent from other exercise devices designed for use in a micro gravity environment. The armbase assembly 50 services as the load adjustment mechanism for the exercise device 10 and is part of the overall load path. The wishbone arm 62 and lift bar 60 serve as an exercise interface for the user 11 of the exercise device 10 and allows the user 11 to perform exercises such as the squat, dead lift, heal raise, and many others. Besides being able to perform bar exercises, the user 11 can also perform pulley exercises such as arm flys and hip abductions with the cable/pulley mechanism 61. Thus, the present invention provides for numerous different exercises.
With reference to
With continued reference to
While the vacuum cylinders 30 provide the constant load component, the flywheels 40 simulate the inertial component of 1-g exercises that occurs during the motion of free weights. As is discussed further below, this is done using a simple gearing mechanism and a rotating mass, i.e., the flywheels 40. A gear rack 32 is attached to the cylinder shaft 31 and it interfaces with the flywheel gear train 41. The gear rack 32 causes the flywheel 40 to rotate with the movement of the lift bar 60. At the top and bottom of each exercise stroke, the flywheel 40 rotation should be stopped. This adds an additional load into the system, which is felt by the user 11 at the lift bar 60. This approximates the loading felt by a user 11 in a 1-g environment.
With continued reference to
With reference to
With reference to
With continued reference to
With reference to
Relative to use on the International Space Station or similar space vehicle, the device allows the entire physiological range (i.e., height, weight, proportion, etc.) of a Space Station crew to perform the required resistive exercises to maintain crew health in terms of maintaining muscle and bone density in a microgravity environment. The device of the present invention has a long operational life with high reliability and low maintenance.
With reference to
The present device 10 is useful where a number of people are required to stay fit and where there is a large usage of the machine. With the present device 10, users 11 exercise with one machine instead of a multiplicity of machines. The present device 10 provides for upper and lower body exercises for a user 11.
As shown in
The theory behind the flywheel 40 is as follows: the linear velocity of the piston 33/gear rack 32 is determined by the exercise frequency at the lift bar 60; the piston's 33/gear rack's 32 linear velocity causes a rotational velocity of the spur gear 44 that meshes with the gear rack 32; the rotational velocity causes a rotational velocity and rotational acceleration on the flywheel 40 that depends on the gear ratios of the flywheel gear train 41; the angular acceleration of the flywheel 40 introduces a torque on the flywheel gear train 41 that depends on the moment of inertia of the flywheel 40; and the torque is transferred back through the flywheel gear train 41 and adds an additional force to the cylinder shaft 31/gear rack 32, which is felt by the user 11 at the lift bar 60.
As shown in
The cable/pulley mechanism 61 is shown in
While the present invention is particularly well suited for use in space, it can be used under normal gravity conditions (i.e., terrestrial applications). As in space applications, under normal gravity conditions, the vacuum cylinder 30 provides a constant force without an inertial component. The lifting of free weights has an inertial component of the load. As the flywheel provides an inertial component to the load, even under normal gravity conditions, the exercise device 10 simulates lifting free weights under normal gravity conditions.
In the second aspect of the present invention, the cylinder shaft 31 is directly connected to the armbase assembly 50 without the flywheel gear train 41 being present. The armbase assembly 50 functions in the same manner as in the first aspect of the present invention to vary the load from the vacuum cylinder. With this second aspect, there is no inertial component to the load. In fact, the exercise device 10 is designed such that the flywheel gear train 41 may be disconnected or swung away from the gear track 32 such that the exercise device 10 operates such as described in this second aspect.
The present inventive product is advantageous over known exercise devices for use in space as the present exercise device 10 is compact, provides for a large number of different exercises, is adjustable for different loads, is adjustable for different sized individuals, and can operate for long periods with minimal maintenance. Also, the present exercise device 10, by providing an inertial component to the load, simulates exercising under normal gravity conditions.
Multiple methods exist for using the various embodiments described above. For example, with reference to
As another method of use example, in the case of a cable/pulley exercise, the user 11 would first affix the appropriate attachment to the end of the cable 63 for the desired exercise. Next, the user 11 selects the amount of desired resistance using the crank 57 to adjust the location of the slider mechanism 55 on the arm base assembly 50. The user 11 will then perform the desired exercise such as an arm fly or hip abduction.
Having described the invention above, various modifications of the techniques, procedures, materials, and equipment will be apparent to those skilled in the art. It is intended that all such variations within the scope and spirit of the invention be included within the scope of the appended claims.
The invention described herein was made by employees of the United States Government and may be manufactured and used by or for the Government of the United States of America for governmental purposes without the payment of any royalties thereon or therefor.
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