Oscillating appendage for fin propulsion

Information

  • Patent Grant
  • 6835108
  • Patent Number
    6,835,108
  • Date Filed
    Monday, January 12, 2004
    21 years ago
  • Date Issued
    Tuesday, December 28, 2004
    20 years ago
Abstract
An oscillating appendage includes a vessel housing a supply of pressurized fluid with reinforced tubes selectively receiving the pressurized fluid from the vessel, an oscillating valve for controlling the supply of pressurized fluid from the vessel to the reinforced tubes, and a flexible skin encompassing the vessel, the reinforced tubes, and the valve. The flexible skin defines an outer shape of the oscillating appendage with a tail member affixed at a terminal end of the appendage to further propel the appendage by an oscillating motion of the appendage.
Description




BACKGROUND OF THE INVENTION




(1) Field of the Invention




This invention generally relates to a device for generating an oscillating motion from a flexible appendage.




(2) Description of the Prior Art




The current art for compact propulsion systems is varied. Some current concepts for unmanned undersea vehicles are very small and simple vehicles which operate in swarms. Each vehicle contains a small sensor which in itself is not particularly powerful but when combined with the sensors from many other vehicles provides a powerful sensing capability.




For a very small vehicle to be feasible, it must include space-efficient and weight-efficient energy storage, energy conversion and propulsion systems. Conventional systems utilize batteries, motors, and propellers for energy storage, energy conversion and propulsion systems, respectively. These systems can be very efficient but have limited power densities. Also, if engineered for performance, the systems can be very expensive and can involve many components which could fail under extended operation.




An alternative to the use of propellers is the use of flapping wing-like devices. It has been shown that dynamically-pitching foils can produce many times the lift compared to static foils with the same dimensions.




Triantafyllou et al. (U.S. Pat. No. 5,401,196) has shown that an optimal oscillation frequency exists which maximizes the lift produced by simple flapping wings.




In the Bandyopadhyay reference, “Maneuvering Hydrodynamics of Fish and Small Underwater Vehicles” INTEGRATIVE AND COMPARITIVE BIOLOGY, February 2002-Vol. 42, it has been further shown that the nature of vortex production from flapping foils controls the efficiency of wings as propulsive devices.




Further, in the Dickinson reference, “Wing Rotation and the Aerodynamic Basis of Insect Flight” SCIENCE, 18 Jun. 1999-Vol 284, it has been shown that the circulation of wings is critical to the enhanced lift production with a low Reynolds number for insect flight.




A number of devices have been proposed which attempt to take advantage of the hydrodynamic effects associated with the flapping foil motion commonly seen in fish propulsion and bird flight. However, it is not readily evident that any device has been proposed which is mechanically simple and can be manufactured in quantity at a very low cost.




The following patents, for example, disclose types of oscillatory wing devices, but do not disclose a device which produces an oscillatory motion in a flexible appendage, which utilizes pressurized fluid to inflate specially designed tubes within the appendage, and which includes a valve system for automatically distributing the pressurized fluid to the appropriate tubes.




Specifically, Gander (U.S. Pat. No. 4,389,196) discloses a watercraft, propelled by a swivellable propulsion fin, in which the fin extends from its swivel axle parallel to the longitudinal direction of the watercraft and which is swivellable laterally by a drive device. The swivellable propulsion fin is arranged on the stern of the watercraft in the prolongation thereof.




Moscrip (U.S. Pat. No. 4,941,627) discloses a hollow fin with a rhombical cross-section constructed of Nitinol or another memory effect alloy, mounted for oscillation about an internal shaft. The memory effect alloy has been previously stretched at a temperature below its critical transition temperature such that heating of one pair of opposite sides, in a rhombic sense, above the critical transition temperature by resistive dissipation of an electric current will cause shortening of this pair of sides and consequent change in the angle of attack.




Mostaghel et al. (U.S. Pat. No. 5,366,395) discloses a pulsating impeller system moving a body through a fluid medium. The pulsating impeller includes an enclosure mounted on a vessel or other body. The enclosure is provided with an inlet-outlet aperture for the flow of the fluid medium into and out of the enclosure. An expandable membrane is positioned in the enclosure. The volume of the membrane is inflated and deflated on a regular cycle by a compressed air or similar system in the vessel. When the enclosure is placed in a fluid such as water, and the membrane inside the enclosure is inflated and the volume of the membrane is increased, which results in the water being forced through the outlet hole in the enclosure to propel the vessel. This force generates a reactive force which thrusts the enclosure and vessel in the opposite direction.




Triantafyllou et al. (U.S. Pat. No. 5,401,196) discloses a propulsion system for use in a fluid, the system utilizing at least one foil which is both oscillated at a frequency “f” with an amplitude “a” in a direction substantially transverse to the propulsion direction and flapped or pitched about a pivot point to change the foil pitch angle to the selected direction of motion with a smooth periodic motion. Parameters of the system including Strouhal number, angle of attack, ratio of the distance to the foil pivot point from the leading edge of the foil to the chord length, the ratio of the amplitude of oscillation to the foil chord width and the phase angle between heave and pitch are all selected so as to optimize the drive efficiency of the foil system.




Yamamoto et al. (U.S. Pat. No. 6,089,178) discloses a submersible vehicle having swinging wings. The vehicle is provided with a main body and rotatable shafts arranged in series and located at front edges of the swinging wings, actuators for driving the shafts independently of one another, and a wing controller for controlling the actuators in such a manner that the wings swing in a flexible manner like the tail fin of a fish.




Sagov (U.S. Pat. No. 6,500,033) discloses a method for propulsion of water-going vessels comprising a plate, which is located in the water and extends across a desired direction of motion for the vessel, where the plate is moved from a first position to a second position and back. Under the influence of a motive force the extent of which varies sinusoidally, the plate is brought into translatory and rectilinear oscillation about a neutral position between the first and the second position, the neutral position being determined by a static equilibrium between spring forces influencing the plate. The plate is controlled in such a manner that its plane extends perpendicularly to the vessel's direction of motion, and greater resistance is exerted by the plate against the water when it is moved opposite to the vessel's desired direction of motion than when it is moved in this direction.




It should be understood that the present invention would in fact enhance the functionality of the above references by providing an oscillating motion by a flexible appendage, the flexible appendage including specially designed tubes embedded therein, and the tubes being manipulated with a supply of pressurized fluid.




SUMMARY OF THE INVENTION




Accordingly, it is a general purpose and primary object of the present invention to provide a device as an oscillating appendage for fin propulsion.




It is therefore a further object of this invention to provide an oscillating appendage with motion as the result of action by pressurized fluid.




It is therefore a still further object of the present invention to provide an oscillating appendage in which a selector valve alternates a supply of pressurized fluid to a selected portion of the appendage.




In accordance with one aspect of the present invention, there is provided an oscillating appendage including a pressure vessel housing a supply of pressurized fluid, reinforced tubes selectively receiving fluid pressure from the pressure vessel, a valve for controlling the supply of pressurized fluid from the pressure vessel to the reinforced tubes, and a flexible skin encompassing the pressure vessel, the reinforced tubes, and the valve. The flexible skin defines an outer shape of the oscillating appendage and a tail member is affixed at a terminal end of the oscillating appendage to propel the appendage when the appendage oscillates. The valve is operated to supply pressure to one or the other of the reinforced tubes, thereby selectively directing the movement of the appendage.











BRIEF DESCRIPTION OF THE DRAWINGS




The appended claims particularly point out and distinctly claim the subject matter of this invention. The various objects, advantages and novel features of this invention will be more fully apparent from a reading of the following detailed description in conjunction with the accompanying drawings in which like reference numerals refer to like parts, and in which:





FIG. 1

depicts a top cross-sectional view of a flexible appendage according to a preferred embodiment of the present invention with the appendage in a neutral position;





FIG. 2

depicts a top cross-sectional view of the flexible appendage of the present invention with the appendage in a flexed position;





FIG. 3

depicts a top cross-sectional view of the flexible appendage of the present invention with the appendage in an opposing flexed position;





FIG. 4

is a sectional view of a valve for use in the flexible appendage of the present invention; and





FIG. 5

is a sectional view of a reinforced tube for use in the present invention.











DESCRIPTION OF THE PREFERRED EMBODIMENT




In general, the present invention is directed to a propulsion device in which the propulsion is created by an oscillatory motion in a flexible appendage. Such a flexible appendage


10


is generally shown in

FIGS. 1

,


2


and


3


in neutral and opposingly flexed positions.




Specifically, the flexible appendage


10


includes a pressure vessel


12


which contains pressurized gas or fluid as a system driver for the flexible appendage. A valve


14


distributes pressurized fluid from the fluid supply in the pressure vessel


12


to reinforced tubes


16


. The valve


14


can be externally controlled to distribute fluid through a fluid system of the appendage


10


as desired, or it can be automatic, to distribute fluid in a predetermined fashion. As will be further described, an automatic mechanical system is proposed for simplicity with the detail of the valve


14


further described in connection with FIG.


4


.




A plurality of reinforced tubes


16


extend from the valve


14


to a tail


18


of the appendage


10


. The reinforced tubes


16


are shown in detail in FIG.


5


and will be further described below for their structure and operation.




A spongy and flexible skin


20


is wrapped around the reinforced tubes


16


, the pressure vessel


12


, and the valve


14


to create a body and transmit the movement of the flexible appendage


10


. The skin


20


of a type known to those skilled in the art can easily be compressed and stretched during articulation of the appendage


10


.




Referring to the reinforced tube


16


shown in

FIG. 5

, the tube includes an inner elastomeric tube


22


which holds pressure and allows axial expansion of the tube. Rigid constraint rings


24


spaced along the tube


16


prevent radial expansion of the inner tube


22


. Ideally, the constraint rings


24


are thin and closely spaced to prevent herniation of the inner elastomeric tube


22


. An end cap


26


closes the end of the inner elastomeric tube


22


and transfers internal pressure to axial tube loading. A combined supply port/end cap


28


closes an opposing end of the inner elastomeric tube


22


, transfers internal pressure to axial tube loading, and allows pressurized fluid to enter the tube structure


16


by an opening


29


in the supply port/end cap. Interconnecting members


30


connect one tube


16


to others and/or to a structure so that axial expansion of the tube is transferred into driving motions.




Turning now to the oscillating valve


14


shown in detail in

FIG. 4

, the valve generally includes a casing


32


which houses a spindle


34


. The casing


32


also attaches to pressure lines and includes chambers


48


,


52


on opposite sides of the spindle


34


.




The spindle


34


is cylindrically shaped having pass-through lines


36


,


38


, and


40


formed therein to connect pressures and vents to tubes


16


A and


16


B. Multiple circumferential seals


42


, such as O-rings, are provided to prevent fluid flow from one tube


16


A to another tube


16


B. A spring member


44


normally biases the spindle


34


to the chamber


48


. In other words, when the spindle


34


is fully seated to the chamber


48


, the spring


44


maintains a force to the chamber due to its preload.




A first stop/end-cap


46


closes the pressure chamber


48


and includes a stem


49


for terminating motion of the spindle


34


.




A second stop/end cap


50


closes the pressure chamber


52


and includes a stem


53


for terminating motion of the spindle


34


. The first stop/end cap


46


and second stop/end cap


50


may be threaded into an opening in the respective ends of the casing


32


in order to provide a secure fitting therewith.




Pressurized fluid is supplied from the pressure vessel


12


to the valve


14


through a supply port


54


.




First vent port


58


connects the tube


16


B to ambient pressure when the spindle


34


is fully to the pressure chamber


52


. A second vent port


56


connects the tube


16


A to ambient pressure when the spindle


34


is fully to the pressure chamber


48


.




A pressurization port


60


connects the pressure chamber


48


to a pressurization throttle


62


. A pressurization port


64


connects the pressure chamber


52


to a pressurization throttle


66


.




The pressurization throttle


62


restricts flow from the tube


16


B to the pressure chamber


48


. More restriction increases the time required to build sufficient pressure in the pressure chamber


48


to force the spindle


34


to the pressure chamber


52


.




The pressurization throttle


66


restricts flow from the tube


16


B to the pressure chamber


52


. More restriction decreases the time required to build sufficient pressure in the pressure chamber


48


to force the spindle


34


to the pressure chamber


52


. If insufficient restriction is provided from the throttle


66


, pressure from the pressure chamber


52


will build too quickly and insufficient pressure will be available to force the spindle


34


toward the pressure chamber


52


.




A vent port


68


allows air or fluid built up in the pressure chamber


52


to be quickly vented once motion to the chamber is initiated.




A vent passage


70


allows the flow of air or fluid for the pressure chamber


52


through the vent port


68


.




The vent pass-through line


38


acting as a vent, connects the tube


16


B to ambient pressure when the spindle


34


is toward the pressure chamber


52


. The vent pass-through line


40


, also acting as a vent, connects the tube


16


A to ambient pressure when the spindle


34


is toward the pressure chamber


48


. The pass-through line


36


acting as a fluid supply connects the tube


16


A or the tube


16


B to supply pressure when the spindle


34


is positioned toward the pressure chambers


52


and


48


, respectively.




Thus, a mechanical device is proposed for the fluid distribution control. Its design generates an oscillating motion of the spindle


34


alternately connecting the tube


16


B and tube


16


A with pressurized fluid. When the system is de-energized, all volumes, lines and chambers are filled with ambient pressure fluid. The spindle


34


is forced to the chamber


48


against the stem


49


of the end cap


46


by the preloaded spring


44


.




To start oscillation of the flexible appendage


10


, pressurized fluid is supplied to the supply port


54


and flows through the valve


14


to the tube


16


B. As the pressure builds in the tube


16


B, the tube expands axially, forcing the tail to bend as shown in FIG.


2


. The tube


16


B is connected to both ports


60


,


64


through the pressurization throttles


62


,


66


, respectively. The throttles


62


,


66


regulate the flow of fluid into the pressure chambers


48


,


52


. Fluid flow at the chamber


52


is restricted more than fluid flow at the chamber


48


so that pressure builds faster at the chamber


48


. When the net force of the spindle


34


through the pressure difference on the sides of the spindle exceeds the preload of the spring


44


, the spindle begins to move to the chamber


52


. After a very short motion, the vent port


68


is opened and the fluid within the pressure chamber


52


is free to escape. The pressure forces then grow, forcing the spindle


34


completely to the pressure chamber


52


. The tube


16


B is then connected to ambient pressure through the pass-through line


38


and the tube


16


A is connected to the pressure vessel


12


through the pass-through line


36


.




As the pressure drops in the pressure chamber


48


and pressure increases in the pressure chamber


52


, the tube


16


A expands and the tube


16


B contracts forcing the tail


18


to bend as shown in FIG.


3


. Simultaneously, the pressure of the tube


16


B drops below the pressure of the pressure chamber


48


and pressure is released back through the pressurization throttle


62


. When the pressure drops below the preload of the spring


44


forcing the spindle


34


to the pressure chamber


48


, the spindle moves back to the pressure chamber


48


. As the spindle


34


moves, the tube


16


A is connected to ambient pressure, vents and contracts while the tube


16


B connects to the pressurized fluid of the pressure vessel


12


, pressurizing and expanding. The vent passage


70


reseals and air is forced from the tube


16


B back into the sides of the spindle


34


, initiating the cycle again.




The frequency of system oscillation is controlled by the settings of the pressurization throttles


62


,


66


. Throttles remaining wide open allow the air to rapidly pressurize the sides of the spindle


34


and the device oscillates rapidly. Restricted flow slows the dynamics of the valve


14


. In addition, residence time of the spindle


34


in its positions can be controlled by adjusting the spring preload, stiffness, and the throttle settings.




Although the valve


14


can be connected to conventional linear actuators, pneumatic motors, or other devices, to support the preferred embodiment, motion of the flexible appendage


10


is generated through the use of the circumferentially reinforced elastomeric tubes


22


. The tubes are described in detail in U.S. Pat. No. 6,148,713 “Elastomeric Surface Actuation System”, incorporated herein by reference.




The thin walled elastomeric tube


22


is surrounded by the constraint rings


24


. When fluid is forced through the supply port in the end cap


28


, internal pressure forces the end caps


26


,


28


axially and the tube


22


radially. Because expansion is constrained radially by the constraint rings


24


, the tube


22


expands in an axial direction only. If the constraint rings


24


are closely spaced, the elastomeric tube


22


cannot form a hernia between the constraint rings and the system remains stable. Two of the reinforcing tubes connected together with the interconnecting members


30


can form the articulation system necessary to oscillate the tail


18


.




In view of the above detailed description, it is anticipated that the invention herein will have far reaching applications other than those of a flexible and oscillating appendage.




This invention has been disclosed in terms of certain embodiments. It will be apparent that many modifications can be made to the disclosed apparatus without departing from the invention. Therefore, it is the intent of the appended claims to cover all such variations and modifications as come within the true spirit and scope of this invention.



Claims
  • 1. A device for propulsion as an oscillating appendage, said device comprising:a vessel housing a supply of pressurized fluid; a plurality of reinforced tubes in fluid communication with said vessel; a valve for selectively controlling the supply of the pressurized fluid from said vessel to said reinforced tubes and release of the pressurized fluid from said reinforced tubes wherein the controlled supply and released flow of the pressurized fluid oscillates said oscillating appendage to propel said oscillating appendage; and a flexible skin encompassing said vessel, said reinforced tubes, and said valve wherein said flexible skin defines an outer shape of said oscillating appendage.
  • 2. The device in accordance with claim 1 wherein said device further comprises a tail member at a terminal end of said oscillating appendage, said tail member reactive to the oscillating motion for additional propulsion.
  • 3. The device in accordance with claim 2 wherein said valve comprises:a casing having a plurality of ports formed therein for enabling the supply and release of the pressurized fluid in said reinforced tubes; a spindle within said casing having passages formed therethrough, said passages aligning with selected ones of said plurality of ports; and opposing pressure chambers formed at opposite ends of said spindle, said pressure chambers controlling a position of said spindle between said pressure chambers; wherein a first positioning of said spindle enables the supply of the pressurized fluid to one of said reinforced tubes axially expanding that said reinforced tube to bend said oscillating appendage in a direction toward another of said reinforced tubes during the release of the pressurized fluid from said another of said reinforced tubes thereby oscillating said oscillating appendage, and wherein a second positioning of said spindle reverses the enablement of the first positioning.
  • 4. The device in accordance with claim 3 wherein said valve further includes an inner biased spring for normally biasing said spindle to the direction of the first positioning.
  • 5. The device in accordance with claim 4 wherein each of said reinforced tubes includes inner elastomeric tubing and a plurality of surrounding axially arranged constraint rings for constraining radial expansion of said inner elastomeric tubing.
  • 6. The device in accordance with claim 5 wherein said reinforced tubes are fluidly connected at intervals to each other.
  • 7. The device in accordance with claim 6 wherein said fluid is compressible gas.
  • 8. The device in accordance with claim 1 wherein said valve comprises:a casing having a plurality of pores formed therein for enabling the supply and release of the pressurized fluid in said reinforced tubes; a spindle within said casing having passages formed therethrough, said passages aligning with selected ones of said plurality of ports; and opposing pressure chambers formed at opposite ends of said spindle, said pressure chambers controlling a position of said spindle between said pressure chambers; wherein a first positioning of said spindle enables the supply of the pressurized fluid to one of said reinforced tubes axially expanding that said reinforced tube to bend said oscillating appendage in a direction toward another of said reinforced tubes during the release of the pressurized fluid from said another of said reinforced tubes thereby oscillating said oscillating appendage, and wherein a second positioning of said spindle reverses the enablement of the first positioning.
  • 9. The device in accordance with claim 8 wherein said valve further includes an inner biased spring for normally biasing said spindle to the direction of the first positioning.
  • 10. The device in accordance with claim 9 wherein each of said reinforced tubes includes inner elastomeric tubing and a plurality of surrounding axially arranged constraint rings for constraining radial expansion of said inner elastomeric tubing.
  • 11. The device in accordance with claim 10 wherein said reinforced tubes are fluidly connected at intervals to each other.
  • 12. The device in accordance with claim 11 wherein said fluid is compressible gas.
  • 13. A device for propulsion as an oscillating appendage, said device comprising:a supply of pressurized fluid; a plurality of reinforced tubes in fluid communication with said supply of pressurized fluid; a means for directing said supply of pressurized fluid to a separate reinforced tube of said plurality of reinforced tubes; a means for releasing in the same instant pressurized fluid from an alternate reinforced tube of said plurality of reinforced tubes thereby creating an oscillating motion by said oscillating appendage to propel said oscillating appendage; and a flexible skin encompassing said supply of pressurized fluid, said plurality of reinforced tubes, said directing means and said releasing means, said flexible skin responsive to said oscillating motion in propulsion of said device.
  • 14. The device in accordance with claim 13 wherein said device further comprises a tail member at a terminal end of said oscillating appendage, said tail member reactive to the oscillating motion for additional propulsion.
STATEMENT OF GOVERNMENT INTEREST

The invention described herein 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.

US Referenced Citations (9)
Number Name Date Kind
3385253 Mathey May 1968 A
4389196 Gander Jun 1983 A
4941627 Moscrip Jul 1990 A
5366395 Mostaghel et al. Nov 1994 A
5401196 Triantafyllou et al. Mar 1995 A
5740750 Triantafyllou et al. Apr 1998 A
6089178 Yamamoto et al. Jul 2000 A
6138604 Anderson et al. Oct 2000 A
6500033 Sagov Dec 2002 B1
Non-Patent Literature Citations (2)
Entry
Michael H. Dickinson et al, Wing Rotation and the Aerodynamic Basis of Insect Flight, SCIENCE, Jun. 18, 1999, pp. 1954-1960, vol. 284, American Association for the Advancement of Science, Washington, DC.
Promode R. Bandyopadhyay, Maneuvering Hydrodynamic of Fish and Small Underwater Vehicles, Integrative and Comparative Biology, Feb. 2002, pp. 102-117, vol. 42, No. 1, Society for Integrative and Comparative Biology, WA.