WO2008141300A1 - Réglage de l'élévation et de l'azimut d'un engrenage à vis sans fin d'une antenne parabolique - Google Patents

Réglage de l'élévation et de l'azimut d'un engrenage à vis sans fin d'une antenne parabolique Download PDF

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Publication number
WO2008141300A1
WO2008141300A1 PCT/US2008/063458 US2008063458W WO2008141300A1 WO 2008141300 A1 WO2008141300 A1 WO 2008141300A1 US 2008063458 W US2008063458 W US 2008063458W WO 2008141300 A1 WO2008141300 A1 WO 2008141300A1
Authority
WO
WIPO (PCT)
Prior art keywords
worm
parabolic antenna
rotational motion
changing
gear set
Prior art date
Application number
PCT/US2008/063458
Other languages
English (en)
Inventor
E. Mitchell Blalock
Wayne Holt
Original Assignee
Viasat, Inc.
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US11/747,130 external-priority patent/US20080278404A1/en
Priority claimed from US11/747,134 external-priority patent/US20080278396A1/en
Application filed by Viasat, Inc. filed Critical Viasat, Inc.
Priority to EP08755333A priority Critical patent/EP2151015A1/fr
Publication of WO2008141300A1 publication Critical patent/WO2008141300A1/fr

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Classifications

    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q3/00—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system
    • H01Q3/02—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole
    • H01Q3/08—Arrangements for changing or varying the orientation or the shape of the directional pattern of the waves radiated from an antenna or antenna system using mechanical movement of antenna or antenna system as a whole for varying two co-ordinates of the orientation
    • H—ELECTRICITY
    • H01—ELECTRIC ELEMENTS
    • H01Q—ANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces
    • H01Q19/12—Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic using reflecting surfaces wherein the surfaces are concave

Definitions

  • Parabolic antennas are commonly used to facilitate radio communications, television communications, data communications, and other applications such as radar. In these applications, parabolic antennas are used either for transmitting and/or receiving signals. To transmit or receive signals to and from a specific remote location, a parabolic antenna may need to be at least generally pointed toward the location. This direction may be represented by an azimuth direction and an elevation angle. Systems and methods to adjust both azimuth direction and elevation angle are therefore necessary to allow a parabolic antenna to transmit and/or receive signals from different remote locations.
  • Parabolic antennas currently exist in various sizes, from diameters as small as fractions of a meter to as large as tens of meters. Regardless of size, systems for rotating the parabolic antennas will still usually be required to change the direction of the parabolic antenna so the antennas may be used to exchange or derive signals from different locations. These rotation systems must be capable of rotating the mass of the antenna precisely and consistently with as little periodic maintenance as possible. The larger the parabolic antenna, the more torque may need to be delivered by the system to move the parabolic antenna. Furthermore, precise directional alignment of the parabolic antenna may be necessary, especially in applications where weak signals are being received, or when the target of the parabolic antenna is small and/or a great distance away.
  • a system for changing the azimuth direction of a parabolic antenna may include a support member, a first gear set, and a first rotational motion source.
  • the support member may be coupled with a surface.
  • the first gear set may include a worm gear and a first worm, where the first worm may engage the worm gear, and the worm gear may have a substantially vertical axis.
  • the support member and the parabolic antenna may be operably coupled with the first gear set.
  • the first rotational motion source may be operably coupled with the first worm, and the parabolic antenna may rotate about the substantially vertical axis when the first rotational motion source is active.
  • a method for changing the azimuth direction of a parabolic antenna may include providing a first gear set operably coupled with a support member and the parabolic antenna.
  • the first gear set may include a worm gear and a first worm.
  • the first worm may engage the worm gear and the worm gear may have a substantially vertical axis.
  • the support member may be coupled with a surface, and the support member and the parabolic antenna may be operably coupled with the first gear set.
  • the method may also include providing a first rotational motion source, where the first rotational motion source may be operably coupled with the first worm.
  • the method may further include activating the first rotational motion source to generate a first rotational motion.
  • the method may moreover include receiving the first rotational motion with the first worm to rotate the parabolic antenna about the substantially vertical axis.
  • a machine-readable medium having machine executable instructions for changing the azimuth direction of a parabolic antenna may include machine-executable instructions for activating a first rotational motion source to generate a first rotational motion.
  • the first rotational motion source may be operably coupled with a first gear set which may include a first worm engaging a worm gear.
  • the first gear set may be operably coupled with a parabolic antenna, and the parabolic antenna may rotate about a substantially vertical axis when the first rotational motion source is active.
  • the machine-readable medium may also include machine- executable instructions for deactivating the first rotational motion source.
  • a system for changing the elevation angle of a parabolic antenna may include a support member, a first gear set, and a first rotational motion source.
  • the first gear set may include a worm gear and a first worm.
  • the first worm may engage the worm gear, and the worm gear may have a substantially horizontal axis.
  • the support member and the parabolic antenna may be operably coupled with the first gear set.
  • the first rotational motion source may be operably coupled with the first worm, and the parabolic antenna may rotate about the substantially horizontal axis when the first rotational motion source is active.
  • a method for changing the elevation angle of a parabolic antenna may include providing a first gear set operably coupled with a support member and the parabolic antenna.
  • the first gear set may include a worm gear and a first worm, and the first worm may engage the worm gear.
  • the worm gear may have a substantially horizontal axis, and the support member and the parabolic antenna may be operably coupled with the first gear set.
  • the method may also include providing a first rotational motion source, where the first rotational motion source may be operably coupled with the first worm.
  • the method may further include activating the first rotational motion source to generate a first rotational motion.
  • the method may moreover include receiving the first rotational motion with the first worm to rotate the parabolic antenna about the substantially horizontal axis.
  • a machine-readable medium having machine executable instructions for changing the elevation angle of a parabolic antenna may include machine-executable instructions for activating a first rotational motion source to generate a first rotational motion.
  • the first rotational motion source may be operably coupled with a first gear set which may include a first worm engaging a worm gear.
  • the first gear set may be operably coupled with a parabolic antenna, and the parabolic antenna may rotate about a substantially horizontal axis when the first rotational motion source is active.
  • the machine-readable medium may also include machine- executable instructions for deactivating the first rotational motion source.
  • Fig. IA is a front axonometric view of a system which includes a parabolic antenna and subsystems which allow for adjustment of the azimuth direction and elevation angle of the parabolic antenna;
  • Fig. IB is a rear axonometric view of the system shown in Fig. IA showing the azimuth direction adjustment assembly and elevation angle adjustment assembly;
  • Fig. 2A is an enlarged view of the portion of the system from Fig. IB which includes the azimuth direction adjustment assembly;
  • Fig. 2B is an enlarged view of the azimuth direction adjustment assembly;
  • FIG. 3 A is an enlarged view of the portion of the system from Fig. IB which includes the elevation angle adjustment assembly;
  • Fig. 3B is an enlarged view of the elevation angle adjustment assembly
  • Fig. 4 is a partially-cut-away axonometric view of an example azimuth direction adjustment assembly or elevation angle adjustment assembly;
  • Fig. 5 is a flow diagram of the mechanical process by which azimuth direction or elevation angle adjustment may occur in some embodiments of the invention.
  • Fig. 6 is a mechanical block diagram of one system of the invention for changing the azimuth direction and elevation angle adjustment of a parabolic antenna
  • Fig. 7 is a block diagram of an exemplary computer system capable of being used in at least some portions of the systems of the present invention, or implementing at least some portion of the methods of the present invention.
  • the embodiments may be described as a process which is depicted as a flowchart, a flow diagram, a data flow diagram, a structure diagram, or a block diagram. Although a flowchart may describe the operations as a sequential process, many of the operations can be performed in parallel or concurrently. In addition, the order of the operations may be re-arranged. A process is terminated when its operations are completed, but could have additional steps not included in the figure. A process may correspond to a method, a function, a procedure, a subroutine, a subprogram, etc. When a process corresponds to a function, its termination corresponds to a return of the function to the calling function or the main function.
  • machine-readable medium includes, but is not limited to portable or fixed storage devices, optical storage devices, wireless channels and various other mediums capable of storing, containing or carrying instruction(s) and/or data.
  • a code segment or machine-executable instructions may represent a procedure, a function, a subprogram, a program, a routine, a subroutine, a module, a software package, a class, or any combination of instructions, data structures, or program statements.
  • a code segment may be coupled to another code segment or a hardware circuit by passing and/or receiving information, data, arguments, parameters, or memory contents. Information, arguments, parameters, data, etc. may be passed, forwarded, or transmitted via any suitable means including memory sharing, message passing, token passing, network transmission, etc.
  • embodiments may be implemented by hardware, software, firmware, middleware, microcode, hardware description languages, or any combination thereof.
  • the program code or code segments to perform the necessary tasks may be stored in a machine readable medium.
  • a processor(s) may perform the necessary tasks.
  • a system for changing the azimuth direction of a parabolic antenna may include a support member, a first gear set and a first rotational motion source.
  • the support member may be coupled with a surface
  • the first gear set may be operably coupled with the support member
  • the parabolic antenna may be operably coupled with the first gear set.
  • Any of the aforementioned components may be coupled with each other via other unspecified components, including mechanical structural components and/or other movement enabling mechanisms.
  • the first rotational motion source may be operably coupled with a first worm in the first gear set to provide rotational motion to the system.
  • the first rotational motion source may be operably coupled with the first worm using mechanical couplings, extension shafts, and/or other components.
  • the rotational motion source may be an electric motor, a pneumatic motor, a hydraulic motor, or even a combustion engine in some applications.
  • the first gear set may include a worm gear and a worm.
  • the first worm may engage the worm gear which may have a substantially vertical axis.
  • the worm gear may be a slewing ring or a ring gear.
  • the first worm and the worm gear may be self-locking such that rotation of the worm may rotate the worm gear, but rotation of the worm gear may not rotate the worm.
  • the first gear set may also include a housing which encloses at least a portion of the worm gear and the first worm. The housing may be stationary relative to an axis of rotation of the first worm, but rotate about the substantially vertical axis relative to the worm gear.
  • first object is coupled with the housing, and a second object is coupled with the worm gear, the first object will rotate relative to the second object, and vice-versa, when the worm rotates.
  • other mechanical components may be present to allow an object to be coupled with the worm gear.
  • the housing may have one or more seals configured to at least nominally seal an interface between moving parts of the first gear set.
  • one side of the gear set may have an opening in the housing which provides a coupling point for the worm gear. This coupling point may rotate relative to the housing, and seals may be provided between the housing and the rotating point to at least nominally seal the interface.
  • Lubricants such as grease and oil may be disposed within the housing to reduce the wear at the engagement point between the worm and worm gear.
  • the interface where the seal or seals reside may be on the underside of the housing as it coupled within the system such that fluids from precipitation, condensation or other sources do not remain stagnant over the seal and infiltrate the housing, reducing the effectiveness of the lubricants therein. Though lubricants may exit the seal in such configurations, the higher viscosity of the lubricants will reduce the rate at which such leaking will occur. Furthermore, adding lubricant to gear set housings is a more typical maintenance operation than tearing down a gear set to remove foreign contaminants.
  • the support member may be operably coupled with the worm gear, while the antenna may be operably coupled with the housing.
  • the first rotational motion source may be coupled with the first worm, and when active, cause the parabolic antenna to rotate about the substantially vertical axis.
  • the worm gear may remain substantially stationary, while causing the first worm to revolve around the worm gear as the worm rotates about its own axis, hi this embodiment then, the worm, housing and the first rotational motion source revolve around the substantially vertical axis with the parabolic antenna.
  • the support member may fixedly coupled with the surface
  • some freedom of movement may be present in the coupling between the support member and the surface.
  • at least some portion of the support member may be configured to be selectively rotated around an axis perpendicular to the surface, possibly the substantially vertical axis of the worm gear, thereby adjusting a reference "starting" azimuth direction of the antenna.
  • the systems of the invention may thereafter be used to adjust the azimuth direction of the antenna from this "starting" direction.
  • a support member with such a rotatable coupling may be initially configured to point the antenna in a southwest direction, while using the systems of the invention for adjusting the position of the antenna from that "starting" southwest direction. If operational changes occur, a new "starting" direction, for example northeast, may be set, allowing the system of the invention to changing the azimuth direction of the antenna relative to the new starting direction.
  • the just described operation may be useful for restricting wear on the worm gear resultant from interacting with the first worm in one particular arc of the worm gear's circumference.
  • the worm gear may be constructed from softer material than associated worms, thereby causing the worm gear to wear at a faster rate relative to the associated worms.
  • wear could be restricted to the same general arc of the worm gear through use of the rotatable coupling. If the support member was fixedly coupled with the surface, then wear would occur in two arcs on the worm gears circumference: a first arc representing movement around the "starting" southwest direction, and a second arc representing movement around the "starting" northeast direction.
  • One possible method of the invention for changing the mesh arc of the worm and worm gear may involve disassembling the first gear set and reorienting the worm gear such that a less used arc engages the worm, and then reassembling the first gear set.
  • the support member may be rotated, and then the worm activated until the parabolic antenna is back in its mean position, thereby engaging the worm gear on a less used arc of the worm gear.
  • the parabolic antenna may be operably coupled with the worm gear, and the support member may be operably coupled with the housing (as opposed to the support member-to-worm-gear and parabolic antenna-to-housing embodiment described above).
  • the first rotational motion source may be coupled with the first worm, and when active, cause the parabolic antenna to rotate about the substantially vertical axis.
  • the rotational axis of the worm may remain substantially stationary, causing the worm gear to rotate about the substantially vertical axis as the worm rotates about its own axis.
  • the housing and the first rotational motion source remain stationary as the parabolic antenna rotates.
  • the system for changing the azimuth direction may also include a second gear set.
  • the first rotational motion source may be operably coupled with the second gear set
  • the second gear set may be operably coupled with the first worm.
  • the second gear set may be used to change the speed of the rotational motion received from the first rotational motion source before it is transferred to the first worm, depending on the gear ratio of the second gear set.
  • the second gear set may therefore be used to increase torque at the expense of rotational speed, or increase rotational speed at the expense of torque.
  • the first gear set may also include a second worm which engages the worm gear.
  • These embodiments may also include a second rotational motion source, where the second rotational motion source is operably coupled with the second worm.
  • the combined work from both rotational motion sources may be combined to rotate the antenna.
  • Increasingly more worms and rotational sources could be added to the first gear set depending on the size of the worms relative to the worm gear and other space constraints. While wear on the worm gear may occur at multiple arcs on the worm gear in these embodiments, the wear in any one arc will be less because the mechanical work required to rotate the parabolic antenna will occur over a greater number of arcs on the worm gear.
  • the system for changing the azimuth direction of a parabolic antenna may also include a sensing mechanism and a control system.
  • the sensing mechanism maybe configured to determine an approximate azimuth direction of the antenna, while the control system may be configured to selectively activate and deactivate the first rotational motion source in either rotational direction until the approximate azimuth direction is substantially equivalent to desired azimuth direction.
  • the sensing mechanism may, for example, include a vernier and an optical sensor which observes the vernier and transmits data to the control system capable of interpreting the data.
  • the control system may determine either: an absolute angular position of the parabolic antenna, possibly by first determining an angular position of the parabolic antenna relative to the support member; or a relative angular position of the parabolic antenna relative to a previous angular position.
  • Other types of sensing mechanisms could also be employed, including electromagnetic sensors and mechanical position sensors.
  • the method may include providing a first gear set operably coupled with a support member and the parabolic antenna; providing a first rotational motion source, where the first rotational motion source may be operably coupled with a first worm within the first gear set; activating the first rotational motion source to generate a first rotational motion; and receiving the first rotational motion with the first worm to rotate the parabolic antenna about the substantially vertical axis.
  • the method may also include determining an approximate azimuth direction of the parabolic antenna, and activating the first rotational motion source until the approximate azimuth direction is substantial equivalent to a desired azimuth direction.
  • the method may include providing a second gear set, and changing the speed of the first rotational motion received by the first worm with the second gear set.
  • the method may also include providing the various types of gear sets described above which employ more than one worm and a second rotational motion source.
  • Some methods of the invention may include using multiple worms to at least attempt to rotate parabolic antenna in opposite directions for a period of time in embodiments where there is backlash between the worms and the worm gear.
  • the worm gear will become substantially locked in relation to the two worms. This will prevent the worm gear from rotating in the direction of available backlash, either between the first worm and worm gear, or between the second worm and the worm gear.
  • machine-readable mediums having machine executable instructions for changing the azimuth direction of a parabolic antenna are described.
  • the machine-readable medium may include machine-executable instructions for activating a first rotational motion source in any of the systems described above to rotate a parabolic antenna, and then deactivating the first rotational motion source to achieve an adjusted azimuth direction of the parabolic antenna.
  • the machine- readable medium may include machine-executable instructions for activating a second rotational motion source, where one is available, such as in some of the systems described above.
  • the machine-readable medium may include machine- executable instructions for activating the first rotational motion source to at least attempt to rotate the parabolic antenna in a first rotational direction, and also activating the second rotational motion source to at least attempt to rotate the parabolic antenna in a second rotational direction, where the second rotational direction is opposite the first rotational direction.
  • These machine-readable mediums may also include machine-executable instructions for deactivating the first rotation motion source and the second rotational motion source when the worm gear is substantially locked in relation to the first worm and the second worm for at least the same purposes as described above.
  • the machine-readable medium may include machine- executable instructions for receiving a signal from a sensing mechanism, determining an approximate azimuth direction of the parabolic antenna based at least in part on the signal, and activating the first rotational motion source in either rotational direction until the approximate azimuth direction is substantial equivalent to a desired azimuth direction.
  • the system may include a support member, a first gear set, and a first rotational motion source.
  • the first gear set may include a worm gear and first worm, hi some embodiments, the worm gear may be a slewing ring or a ring gear.
  • the first worm may engage the worm gear and the worm gear may have a substantially horizontal axis.
  • the first worm and the worm gear may be self- locking such that rotation of the worm may rotate the worm gear, but rotation of the worm gear may not rotate the worm.
  • the first gear set may also include a housing which encloses at least a portion of the worm gear and the first worm.
  • the housing may be stationary relative to an axis of rotation of the first worm, but rotate about the substantially horizontal axis relative to the worm gear.
  • the support member may be operably coupled with the first gear set, and the parabolic antenna may be operably coupled with the first gear set.
  • Any of the aforementioned components may be coupled with each other via other unspecified components, including mechanical structural components and/or other movement enabling mechanisms.
  • the support member may be coupled with a pivot member, and the pivot member may be coupled with another gear set for adjusting the azimuth direction of the parabolic antenna, and that gear set may be coupled with the support member.
  • a bearing, or other rotational coupling may also couple with parabolic antenna with the pivot member at another point.
  • the bearing may allow the parabolic antenna to rotate relative to the pivot member depending on the movement produced by the first gear set and first rotational motion source.
  • the first rotational motion source may be operable coupled with the first worm and the parabolic antenna may rotate about the substantially horizontal axis when the first rotational motion source is active.
  • the first rotational motion source may be operably coupled with the first worm using mechanical couplings, extension shafts, and/or other components.
  • the rotational motion source may be an electric motor, a pneumatic motor, a hydraulic motor, or even a combustion engine in some applications.
  • the parabolic antenna may be coupled with the worm gear, and the housing may be coupled with the support member and/or pivot member.
  • the worm gear may be configured to rotate about the substantially horizontal axis when the first worm transfers rotational motion with the worm gear.
  • the support member and/or pivot member may be coupled with the worm gear, while the parabolic antenna may be coupled with the housing.
  • the first worm may have a rotational axis and the first worm may revolve around the substantially horizontal axis when the first worm rotates about its rotational axis.
  • the system for changing the elevation angle may also include a second gear set.
  • the second gear set may be operably coupled with the first rotational motion source and the first worm.
  • the second gear set may be used to change the speed of the rotational motion received from the first rotational motion source before it is transferred to the first worm, depending on the gear ratio of the second gear set.
  • the second gear set may therefore be used to increase torque at the expense of rotational speed, or increase rotational speed at the expense of torque.
  • the first gear set may also include a second worm which engages the worm gear.
  • These embodiments may also include a second rotational motion source, where the second rotational motion source is operably coupled with the second worm.
  • the combined work from both rotational motion sources may be combined to rotate the antenna.
  • Increasingly more worms and rotational sources could be added to the first gear set depending on the size of the worms relative to the worm gear and other space constraints. While wear on the worm gear may occur at multiple arcs on the worm gear in these embodiments, the wear in any one arc will be less because the mechanical work required to rotate the parabolic antenna will occur over a greater number of arcs on the worm gear.
  • a rotatable coupling may be used in the elevation angle adjustment gear set to couple either the pivot member and/or support member with the first gear set, or the parabolic antenna with the first gear set. This may allow a new arc on the worm gear to be engaged by the worm or worms in the first gear set without disassembling the gear set and rotating the worm gear relative to the worm and then reassembling.
  • the system for changing the elevation angle of a parabolic antenna may also include a sensing mechanism and a control system.
  • the sensing mechanism may be configured to determine an elevation angle of the antenna, while the control system may be configured to selectively activate and deactivate the first rotational motion source in either rotational direction until the approximate elevation angle is substantially equivalent to desired elevation angle.
  • the sensing mechanism may, for example, include a vernier and an optical sensor which observes the vernier and transmits data to the control system capable of interpreting the data.
  • the control system may determine either: an absolute angular position of the parabolic antenna, possibly by first determining an angular position of the parabolic antenna relative to the support member; or a relative angular position of the parabolic antenna relative to a previous angular position.
  • Other types of sensing mechanisms could also be employed, including electromagnetic sensors and mechanical position sensors.
  • the method may include providing a first gear set operably coupled with a support member and the parabolic antenna.
  • the first gear set may include a worm gear and a first worm, where the first worm may engage the worm gear, the worm gear may have a substantially horizontal axis, and the support member and the parabolic antenna may be operably coupled with the first gear set.
  • the method may further include providing a first rotational motion source, where the first rotational motion source may be operably coupled with the first worm, and activating the first rotational motion source to generate a first rotational motion.
  • the method may include receiving the first rotational motion with the first worm to rotate the parabolic antenna about the substantially horizontal axis.
  • the parabolic antenna being operably coupled with the first gear set may include the parabolic antenna coupled with the worm gear, where the worm gear may be configured to rotate about the substantially horizontal axis, and the first worm may be configured to transfer rotational motion with the worm gear.
  • the support member being operably coupled with the first gear set may include the support member coupled with the worm gear, where the first worm may have a rotational axis, and the first worm may be configured to revolve around the substantially horizontal axis when the first worm rotates about the rotational axis.
  • the methods for changing the elevation angle of a parabolic antenna may include providing a second gear set, and changing the speed of the first rotational motion received by the first worm with the second gear set.
  • the first gear set may further include a second worm which engages the worm gear
  • the method may include providing a second rotational motion source, where the second rotational motion source is operably coupled with the second worm.
  • the method may further include activating the second rotational motion source to generate a second rotational motion, and receiving the second rotational motion with the second worm to rotate the parabolic antenna about the substantially horizontal axis.
  • Some methods of the invention may include using multiple worms to at least attempt to rotate parabolic antenna in opposite directions for a period of time in embodiments where there is backlash between the worms and the worm gear.
  • the worm gear will become substantially locked in relation to the two worms. This will prevent the worm gear from rotating in the direction of available backlash, either between the first worm and worm gear, or between the second worm and the worm gear.
  • the methods for changing the elevation angle of a parabolic antenna may include determining an approximate elevation angle of the parabolic antenna, and activating the first rotational motion source until the approximate elevation angle is substantial equivalent to a desired elevation angle.
  • machine-readable mediums having machine executable instructions for changing the elevation angle of a parabolic antenna are described.
  • the machine-readable medium may include machine-executable instructions for activating a first rotational motion source to generate a first rotational motion.
  • the first rotational motion source may be operably coupled with a first gear set which includes a first worm engaging a worm gear.
  • the first gear set may be operably coupled with a parabolic antenna, and the parabolic antenna may rotate about a substantially horizontal axis when the first rotational motion source is active.
  • the machine-readable medium may also include machine-executable instructions for deactivating the first rotational motion source.
  • the first gear set being operably coupled with the parabolic antenna may include the parabolic antenna coupled with the worm gear. In other embodiments, the first gear set being operably coupled with the parabolic antenna may include a support member coupled with the worm gear.
  • the machine-readable medium may further include machine- executable instructions for activating a second rotational motion source to generate a second rotational motion.
  • the first gear set may further include a second worm engaging the worm gear, and the second rotational motion source may be operably coupled with the second worm.
  • There may also be machine-executable instructions for deactivating the second rotational motion source.
  • the machine-readable medium may also include machine- executable instructions for activating the first rotational motion source to at least attempt to rotate the parabolic antenna in a first rotational direction and activating the second rotational motion source to at least attempt to rotate the parabolic antenna in a second rotational direction, where the second rotational direction is opposite the first rotational direction.
  • these embodiments may also include machine-executable instructions for deactivating the first rotation motion source and the second rotational motion source when the worm gear may be substantially locked in relation to the first worm and the second worm.
  • machine-readable mediums having machine executable instructions for changing the elevation angle of a parabolic antenna may also include machine-readable instructions for receiving a signal from a sensing mechanism, and determining an approximate elevation angle of the parabolic antenna based at least in part on the signal. Furthermore, these embodiments may include machine-executable instructions for activating the first rotational motion source in either rotational direction until the approximate elevation angle is substantial equivalent to a desired elevation angle.
  • System 100 includes a parabolic antenna 110, a support member 120, a pivot member 130, an azimuth direction adjustment assembly (“ADA assembly”) 140, an elevation angle adjustment assembly (“EAA assembly”) 150, and a bearing 160.
  • support member 120 is fixedly coupled with a surface (not shown).
  • Support member 120 is operably coupled with ADA assembly 140.
  • ADA assembly 140 is also operably coupled with pivot member 130, which in turn is operably coupled with EAA assembly 150.
  • EAA assembly 150 is the operably coupled with parabolic antenna 110.
  • ADA assembly 140 may be activated and pivot member 130 will rotate relative to support member 120. Because pivot member is coupled with parabolic antenna 110 through EAA assembly 150, parabolic antenna 110 will rotate about a vertical axis which may be defined by ADA assembly 140.
  • EAA assembly 150 may be activated and parabolic antenna 110 will rotate relative to pivot member 130. Because pivot member is coupled to a surface through ADA assembly 140 and support member 120, parabolic antenna 110 will rotate about an axis which is horizontal relative to the surface. The horizontal axis may be defined by EAA assembly 150, and may itself rotate as ADA assembly rotates pivot member 130.
  • Fig. 2 A shows a closer view of ADA assembly 140 and surrounding components.
  • Fig. 2B shows a closer view of ADA assembly 140 and its sub-components.
  • ADA assembly 140 may include a first gear set 210 which includes a housing, a worm gear, and a worm; a second gear set 220; and a rotational motion source 230 (shown here as a motor ). When rotational motion source 230 is activated, it will transfer rotational motion to second gear set 220. Second gear set 220 may change the speed of the rotational motion and transfer the modified rotational motion to the worm in first gear set 210.
  • Support member 120 is coupled with the worm gear on the underside of first gear set 210.
  • Pivot member 130 is coupled with the housing of first gear set 210 on the topside of first gear set 210.
  • the worm in first gear set 210 has a rotational axis which is substantially stationary relative to the housing of first gear set 210. As the worm rotates when receiving the modified rotational motion from second gear set 220, the worm revolves around the worm gear, and therefore the housing of the first gear set 210 rotates about the vertical axis of the worm gear.
  • parabolic antenna rotates as the worm revolves around the worm gear, thereby changing the azimuth direction of the parabolic antenna.
  • second gear set 220 and rotational motion source 230 rotate with pivot member 130 and parabolic antenna 110. This may be advantageous because second gear set 220 and rotational motion source 230 may use the same clearance space set aside for the rotation of parabolic antenna 110.
  • Seals may exist on first gear set 210 to close interfaces between the worm gear and the housing. This assists in keeping undesirable liquids and solids, such as water and particulates, from entering the interfaces and causing accelerated wear between the teeth of the worm gear and the worm. Additionally, the seals assist in retaining lubricants, such as gear grease, within the housing, which reduces wear between the teeth of the worm gear and the worm.
  • first gear set 210 By orientating first gear set 210 in a manner which places the seals on the underside of first gear set 210, moisture, possibly from sources such as precipitation, will not collect on the seal face, therefore at least reducing the amount of undesirable ingress into the housing.
  • ADA assembly 140 may be inverted compared to its position in Fig. 2 A and Fig. 2B.
  • pivot member 130 may be coupled with the worm gear of first gear set 210
  • support member 120 may be coupled with the housing of first gear set 210.
  • the rotational axis of the worm remains stationary and therefore the housing of first gear set 210 also remains stationary.
  • the worm gear of first gear set 210 rotates about its vertical axis as it receives rotational motion from the worm, therefore rotating pivot member 130 and parabolic antenna 110 which is coupled with pivot member 130.
  • second gear set 220 and rotational motion source 230 are stationary with respect to pivot member 130 and parabolic antenna 110.
  • ADA assembly 140 may include a sensing mechanism which determines an angular position of pivot member 130, and hence parabolic antenna 110, relative to support member 120 or the surface to which support member 120 is coupled.
  • the sensing mechanism may, for example, include a vernier and an optical sensor which observes the vernier and transmits data to a control system capable of interpreting the data.
  • the control system may determine either: an absolute angular position of parabolic antenna 110, possibly by first determining an angular position of parabolic antenna 110 relative to support member 120; or a relative angular position of parabolic antenna 110 relative to a previous position.
  • FIG. 3 A shows a closer view of EAA assembly 150 and surrounding components.
  • Fig. 3B shows a closer view of EAA assembly 150 and its sub-components.
  • EAA assembly 150 may include a first gear set 310 which includes a housing, a worm gear, and a worm; a second gear set 320; and a rotational motion source 330 (shown here as a motor ). When rotational motion source 330 is activated, it will transfer rotational motion to second gear set 320. Second gear set 320 may change the speed of the rotational motion and transfer the modified rotational motion to the worm in first gear set 310.
  • Parabolic antenna 110 is coupled with the worm gear on the left side of first gear set 310.
  • Pivot member 130 is coupled with the housing of first gear set 310 on the right side of first gear set 310.
  • the worm rotates when receiving the modified rotational motion from second gear set 320, the worm transfers rotational motion with the worm gear, and therefore the worm gear rotates about the horizontal axis of the worm gear.
  • parabolic antenna 110 is coupled with the worm gear of first gear set 310, parabolic antenna rotates as the worm gear rotates, thereby changing the elevation angle of the parabolic antenna, hi this embodiment then, second gear set 320 and rotational motion source 330 are stationary as parabolic antenna 110 rotates.
  • EAA assembly 150 may be inverted compared to its position in Fig. 3A and Fig. 3B.
  • pivot member 130 may be coupled with the worm gear of first gear set 310
  • parabolic antenna 110 may be coupled with the housing of first gear set 310.
  • the worm gear remains stationary. Instead, the worm of first gear set 310 revolves around the horizontal axis as it rotates. Because the housing of first gear set 310 is stationary relative to the rotational axis of the worm, and parabolic antenna 110 is coupled with the housing, parabolic antenna 110 will rotate as the worm revolves around the substantially horizontal axis of the worm gear.
  • second gear set 320 and rotational motion source 330 rotate with parabolic antenna 110.
  • EAA assembly 150 may include a sensing mechanism which determines an angular position of parabolic antenna 110 relative to pivot member 130 or some other reference vector.
  • the sensing mechanism may, for example, include a vernier and an optical sensor which observes the vernier and transmits data to a control system capable of interpreting the data.
  • the control system may determine either an absolute angular position of parabolic antenna 110, possibly by first determining an angular position of parabolic antenna 110 relative to support member 120.
  • Fig. 4 shows partially-cut-away axonometric view of an example ADA assembly or EAA assembly 400.
  • assembly 400 includes a first rotational motion source 410 (shown here as a motor), a second rotational motion source 420 (shown here as a motor), a first worm 430, a second worm (hidden from view), a worm gear 440, a housing 450, a worm gear coupling member 460, and a seal 470.
  • both rotational motion sources 410, 420 may be activated and hence turn first worm 430 and second worm. First worm 430 and second worm may then rotate worm gear 440.
  • Worm gear coupling member 460 may be fixedly coupled with worm gear 440, thereby causing worm gear coupling member 460 to rotate whenever first rotational motion source 410 and second rotational motion source 420 are activated in concert.
  • Housing 450 may also have coupling points on its underside allowing coupling to other elements in a similar fashion to worm gear coupling member. Note that assembly 400 differs from assemblies 140, 150 previously discussed because there are no secondary gear sets (such as second gear sets 220, 230) to adjust the speed of the rotational motion provided by first rotational motion source 410 and second rotational motion source 420.
  • housing 450 may be coupled with pivot member 130 and consequently parabolic antenna 110, while worm gear coupling member 460 may be coupled with support member 120.
  • housing 450, first worm 430, second worm, first rotational motion source 410, and second rotational motion source 420 will rotate with the parabolic antenna.
  • worm gear coupling member 460 may be coupled with pivot member 130 and consequently parabolic antenna 110, while housing 450 may be coupled with support member 120.
  • housing 450, the axis of first worm 430, the axis of second worm, first rotational motion source 410, and second rotational motion source 420 will remain stationary when the parabolic antenna rotates.
  • Fig. 5 is a flow diagram of the mechanical process by which azimuth direction or elevation angle adjustment may occur in some embodiments of the invention.
  • a rotational motion source may be activated. This may occur because a new target for transmissions from the parabolic antenna has been selected, or reception from a different source is required. Other reasons for activation of the rotational motion source may include correction and/or adjustment related to movement of either the parabolic antenna or the target/source.
  • the rotational motion source generates rotational motion.
  • this motion is transmitted, possibly via shafts, clutches, couplings, and/or other mechanical elements, to another component.
  • the motion will be received by a secondary gear set.
  • the secondary gear set may adjust the speed of the rotational motion received, either reducing or increasing the speed, while increasing or reducing the torque.
  • Various gear sets known in the art may fulfill this purpose. Higher speeds may be required where faster tracking is required by the parabolic antenna, while higher torques may be required for larger parabolic antenna systems.
  • the secondary gear set transmits the modified rotational motion, possibly via shafts, clutches, coupling, and/or other mechanical elements to another component.
  • the worm of a primary gear set receives the modified rotational motion, causing the worm to rotate at block 540.
  • the parabolic antenna will transfer its rotational motion to the worm gear of the primary gear set.
  • the worm gear receives the rotational motion, causing the worm gear to rotate at block 565.
  • the parabolic antenna will rotate because it is coupled with the worm gear.
  • Fig. 6 shows a mechanical block diagram of one system of the invention for changing the azimuth direction and elevation angle adjustment of a parabolic antenna. Shown in Fig. 6 is a surface 610 to which support member 620 is coupled. As discussed above, support member 620 may be either fixedly or rotatably coupled with surface 610.
  • Support member 620 is, in turn, operably coupled with ADA assembly 630 which is also operably coupled with pivot member 640.
  • ADA assembly 630 may be various different possible arrangements, possibly dependent on how it is coupled with support member 620 and or pivot member 640.
  • Pivot member 640 is operably coupled with both an EAA assembly 650 and a bearing 660.
  • a parabolic antenna 680 is operably coupled to both EAA assembly 650 and bearing 660, possibly through coupling members 670.
  • Coupling members may include structural or fastening elements which allow the parabolic antenna to interface with the available coupling mechanisms/methods on EAA assembly 650 and bearing 660.
  • a second EAA assembly may replace bearing 660, providing for increased amount of torque to be delivered by the combined efforts of both EAA assemblies.
  • a sensing mechanism 693 may monitor at least a portion of one or more of surface 610, support member 620, ADA assembly 630, and pivot member 640, and transmits data to control system 699.
  • Control system 699 may interpret the data to determine an angular position of pivot member 640, and hence parabolic antenna 680 relative to a stationary portion of ADA assembly 630, support member 620, or surface 610.
  • This angular position equivalent to parabolic antenna's 680 azimuth direction, may be compared to a desired azimuth direction and ADA assembly 630 may be activated in either rotational direction until the determined azimuth direction is equal to, or within a certain range of, the desired azimuth direction.
  • ADA assembly 630 may be continually active during tracking of a target or source of signals transmitted or received by parabolic antenna 680.
  • Another sensing mechanism 696 may monitor at least a portion of one or more of pivot member 640, EAA assembly 650, and coupling members 670 (or possibly parabolic antenna 680 itself), and transmits data to control system 699.
  • Control system 699 may interpret the data to determine an angular position of parabolic antenna 680 relative to a standard horizon position. This angular position, equivalent to parabolic antenna's 680 elevation angle, may be compared to a desired elevation angle, and EAA assembly 650 may be activated in either rotational direction until the determined elevation angle is equal to, or within a certain range of, the desired elevation angle.
  • EAA assembly 650 may be continually active during tracking of a target or source of signals transmitted or received by parabolic antenna 680.
  • Fig. 7 is a block diagram illustrating an exemplary computer system in which at least portions of the present invention may be implemented.
  • a computer system 700 such as may be used, in whole, in part, or with various modifications, to provide the functions of the sensing mechanisms 693,696, the control system 699 and/or other components of the invention such as those discussed above.
  • various functions of the control system 699 may be controlled by the computer system, for example, accepting and storing a desired azimuth direction or elevation angle, either from a user or an another computer; determining an approximate azimuth direction or elevation angle of a parabolic antenna; activating rotational motion sources to change the approximate azimuth direction or elevation angle of a parabolic antenna; etc.
  • the computer system 700 is shown comprising hardware elements that may be electrically coupled via a bus 790.
  • the hardware elements may include one or more central processing units (CPUs) 710, one or more input devices 720 (e.g., a mouse, a keyboard, etc.), and one or more output devices 730 (e.g., a display device, a printer, etc.).
  • the computer system 700 may also include one or more storage device 740.
  • storage device(s) 740 may be disk drives, optical storage devices, solid-state storage device such as a random access memory (“RAM”) and/or a read-only memory (“ROM”), which can be programmable, flash-updateable and/or the like.
  • RAM random access memory
  • ROM read-only memory
  • the computer system 700 may additionally include a computer-readable storage media reader 750, a communications system 760 (e.g., a modem, a network card (wireless or wired), an infra-red communication device, etc.), and working memory 780, which may include RAM and ROM devices as described above.
  • the computer system 700 may also include a processing acceleration unit 770, which can include a DSP, a special-purpose processor and/or the like.
  • the computer-readable storage media reader 750 can further be connected to a computer-readable storage medium, together (and, optionally, in combination with storage device(s) 740) comprehensively representing remote, local, fixed, and/or removable storage devices plus storage media for temporarily and/or more permanently containing computer- readable information.
  • the communications system 760 may permit data to be exchanged with a network and/or any other computer described above with respect to the system 700.
  • the computer system 700 may also comprise software elements, shown as being currently located within a working memory 780, including an operating system 784 and/or other code 788. It should be appreciated that alternate embodiments of a computer system 700 may have numerous variations from that described above. For example, customized hardware might also be used and/or particular elements might be implemented in hardware, software (including portable software, such as applets), or both. Further, connection to other computing devices such as network input/output devices may be employed.
  • Software of computer system 700 may include code 788 for implementing any or all of the function of the various elements of the architecture as described herein.
  • software stored on and/or executed by a computer system such as system 700, can provide the functions of the sensing mechanisms 693,696, the control system 699 and/or other components of the invention. Methods implementable by software on some of these components have been discussed above in more detail.
  • a number of variations and modifications of the disclosed embodiments can also be used.
  • an increased number of EAA or ADA assemblies could be used when high speed and/or torque are necessary, or approximate azimuth direction and elevation angle may be determined by knowing an initial position of the parabolic antenna and calculating the present position based on how long, and in what direction the EAA and ADA assemblies have been activated.
  • other embodiments could be employed to change the orientation of devices.
  • the systems and methods described above could be used to rotate weapons systems, for example mounted firearms, lasers and/or sonic systems. Other possible uses include sports equipment such as ball throwers.
  • Optical systems could use the systems and methods described above to rotate lenses, mirrors and/or other optic components.
  • Robotic arms could also be manipulated in a similar fashion, perhaps in manufacturing environments where one robotic arm must perform work in a variety of positions.

Landscapes

  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

L'invention concerne un système permettant de changer la direction azimut ou l'élévation d'une antenne parabolique (110). Ce système comprend un élément support (120), un premier train d'engrenages et une source de mouvement rotatif. L'élément support (120) peut être couplé à une surface et le premier train d'engrenages peut comprendre un engrenage à vis sans fin et une première vis. La première vis peut être couplée à l'engrenage à vis sans fin. L'élément support et l'antenne parabolique peuvent être couplés fonctionnels au premier train d'engrenages. La première source de mouvement rotatif peut être couplée fonctionnelle à la première vis, et l'antenne parabolique peut tourner lorsque la première source de mouvement rotatif est active.
PCT/US2008/063458 2007-05-10 2008-05-12 Réglage de l'élévation et de l'azimut d'un engrenage à vis sans fin d'une antenne parabolique WO2008141300A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP08755333A EP2151015A1 (fr) 2007-05-10 2008-05-12 Réglage de l'élévation et de l'azimut d'un engrenage à vis sans fin d'une antenne parabolique

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US11/747,130 US20080278404A1 (en) 2007-05-10 2007-05-10 Worm Gear Elevation Adjustment of a Parabolic Dish
US11/747,134 2007-05-10
US11/747,130 2007-05-10
US11/747,134 US20080278396A1 (en) 2007-05-10 2007-05-10 Worm Gear Azimuth Adjustment of a Parabolic Antenna

Publications (1)

Publication Number Publication Date
WO2008141300A1 true WO2008141300A1 (fr) 2008-11-20

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Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4434345A (en) * 1982-07-29 1984-02-28 Muscatell Ralph P Microwave system for frost protection of fruit trees
US5560256A (en) * 1994-01-11 1996-10-01 Tines; John L. Base support for movable objects
US5585804A (en) * 1992-11-18 1996-12-17 Winegard Company Method for automatically positioning a satellite dish antenna to satellites in a geosynchronous belt
GB2301943A (en) * 1995-06-09 1996-12-18 Chan Ching Feng Satellite dish antenna mounting structure
US6313805B1 (en) * 1999-09-30 2001-11-06 Nec Corporation Wide range azimuth driving system for satellite communication antenna
WO2002101873A1 (fr) * 2001-06-13 2002-12-19 British Telecommunications Public Limited Company Procede et dispositif de calage d'antennes
US20030083063A1 (en) * 2001-11-01 2003-05-01 Tia Mobile, Inc. Easy set-up, vehicle mounted, in-motion tracking, satellite antenna

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4434345A (en) * 1982-07-29 1984-02-28 Muscatell Ralph P Microwave system for frost protection of fruit trees
US5585804A (en) * 1992-11-18 1996-12-17 Winegard Company Method for automatically positioning a satellite dish antenna to satellites in a geosynchronous belt
US5560256A (en) * 1994-01-11 1996-10-01 Tines; John L. Base support for movable objects
GB2301943A (en) * 1995-06-09 1996-12-18 Chan Ching Feng Satellite dish antenna mounting structure
US6313805B1 (en) * 1999-09-30 2001-11-06 Nec Corporation Wide range azimuth driving system for satellite communication antenna
WO2002101873A1 (fr) * 2001-06-13 2002-12-19 British Telecommunications Public Limited Company Procede et dispositif de calage d'antennes
US20030083063A1 (en) * 2001-11-01 2003-05-01 Tia Mobile, Inc. Easy set-up, vehicle mounted, in-motion tracking, satellite antenna

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