GB2182240A - Portable support; radio antenna arrangement - Google Patents

Portable support; radio antenna arrangement Download PDF

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Publication number
GB2182240A
GB2182240A GB08527026A GB8527026A GB2182240A GB 2182240 A GB2182240 A GB 2182240A GB 08527026 A GB08527026 A GB 08527026A GB 8527026 A GB8527026 A GB 8527026A GB 2182240 A GB2182240 A GB 2182240A
Authority
GB
United Kingdom
Prior art keywords
base
leg
dish
legs
antenna
Prior art date
Legal status (The legal status 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 status listed.)
Granted
Application number
GB08527026A
Other versions
GB8527026D0 (en
GB2182240B (en
Inventor
Robert John Melling
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Racal Antennas Ltd
Original Assignee
Racal Antennas Ltd
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
Application filed by Racal Antennas Ltd filed Critical Racal Antennas Ltd
Priority to GB8527026A priority Critical patent/GB2182240B/en
Publication of GB8527026D0 publication Critical patent/GB8527026D0/en
Publication of GB2182240A publication Critical patent/GB2182240A/en
Application granted granted Critical
Publication of GB2182240B publication Critical patent/GB2182240B/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/16Details concerning attachment of head-supporting legs, with or without actuation of locking members thereof
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/02Heads
    • F16M11/04Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand
    • F16M11/06Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting
    • F16M11/10Means for attachment of apparatus; Means allowing adjustment of the apparatus relatively to the stand allowing pivoting around a horizontal axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/20Undercarriages with or without wheels
    • F16M11/2007Undercarriages with or without wheels comprising means allowing pivoting adjustment
    • F16M11/2014Undercarriages with or without wheels comprising means allowing pivoting adjustment around a vertical axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/20Undercarriages with or without wheels
    • F16M11/24Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other
    • F16M11/26Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other by telescoping, with or without folding
    • F16M11/28Undercarriages for supports with one single telescoping pillar
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M11/00Stands or trestles as supports for apparatus or articles placed thereon ; Stands for scientific apparatus such as gravitational force meters
    • F16M11/20Undercarriages with or without wheels
    • F16M11/24Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other
    • F16M11/26Undercarriages with or without wheels changeable in height or length of legs, also for transport only, e.g. by means of tubes screwed into each other by telescoping, with or without folding
    • F16M11/32Undercarriages for supports with three or more telescoping legs
    • F16M11/36Members preventing slipping of the feet
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q1/00Details of, or arrangements associated with, antennas
    • H01Q1/12Supports; Mounting means
    • H01Q1/125Means for positioning
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01QANTENNAS, i.e. RADIO AERIALS
    • H01Q19/00Combinations of primary active antenna elements and units with secondary devices, e.g. with quasi-optical devices, for giving the antenna a desired directional characteristic
    • H01Q19/10Combinations 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
    • H01Q19/18Combinations 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 having two or more spaced reflecting surfaces
    • H01Q19/19Combinations 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 having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface
    • H01Q19/193Combinations 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 having two or more spaced reflecting surfaces comprising one main concave reflecting surface associated with an auxiliary reflecting surface with feed supported subreflector
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M2200/00Details of stands or supports
    • F16M2200/02Locking means
    • F16M2200/021Locking means for rotational movement
    • F16M2200/022Locking means for rotational movement by friction
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16MFRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M2200/00Details of stands or supports
    • F16M2200/02Locking means
    • F16M2200/025Locking means for translational movement
    • F16M2200/027Locking means for translational movement by friction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aerials With Secondary Devices (AREA)
  • Support Of Aerials (AREA)

Abstract

A portable support has four legs, (6, 8, 10 and 12), each in the form of upper and lower relatively slidable parts, each lower part terminating in a ground-engaging foot 6D, 8D, (10D,) 12D. The legs at their upper ends are pivotally connected to a base 14. The base 14 is rigidly secured relative to the legs by screwing down handwheels (18A,) 18B, (18C,) 18D which press respective pads (20a, 20B, 20C, 20D) into firm contact with the outer surfaces of the upper parts of the legs. A dish-shaped radio antenna 42, such as for satellite communication, is supported on an arm 40 from a column 24. The column is adjustable to swivel the antenna about a substantially vertical axis and the arm is pivotally mounted on the column 24 so as to move the dish about a substantially horizontal axis. The sub-reflector 50 for the antenna is completely enclosed within a cone-shaped support 48 made of GRP and with foam-filled reinforced ribs 54 and a GRP end plate 52. <IMAGE>

Description

SPECIFICATION Portable supports such as for radio antennas, and a radio antenna suitable for supporting by such a support The invention relates to portable supports. An embodiment of the invention to be described in more detail below isforsupportingaradio antenna. However, the portable supports of the invention are not restricted for use to supporting radio antennas.
The invention also relates to radio antennas which may, though not necessary are, supported by portable supports according to the invention.
According to the invention,there is provided a portable support, comprising a base having four adjustable-length legs pivotally depending therefrom and extending downwardly and outwardly into engagementwith the ground, and adjustable means, individually adjustable relative to each said leg in accordance with its angular position relative to the base, for rigidlysecuringthe base to the legs.
According to the invention,there its further provided a radio antenna arrangement comprising a dishshaped reflector supported within and at the closedoff large diameter end of a conically-shaped support made of radio-transparent glass reinforced plastics material.
A portable radio antenna assembly embodying the invention will now be described, byway of example only, with reference to the accompanying drawings in which Figure lisa perspective view of the support ofthe assembly; Figure2 is a side elevation ofthe assembly; and Figure3 is an enlarged view of part ofthe assembly.
The assembly to be described is intended for use in radio communications between the ground and a satellite. The assembly is designed to be portable, in disassembled form. When re-assembled, it is intended to be able to be set up on any convenient patch of ground and its antenna then directed at the satellite from which radio communication is to be received.
Therefore, the assembly has to be able to be set up so that the antenna can be given the desired orientation even when the assembly has to be placed on an uneven ground surface, and, furthermore,the assembly has to provide an extremely stable support forthe antenna once it has been set up; because of the distance involved to the satellite, even extremely minorchanges in antenna attitudewill disrupt radio communication.
As shown in Figure 1,the supportS ofthe assembly has four legs, 6,8,10 and 12. The legs are of generally square cross-section. Each leg has a lower part6A,8A, 10A, 12which is slidablewithin a respective upper part 68, 8B, lOB, 12B. The relative position of each lower part with respect to each upper part is thus easily adjustable, and when the desired relative position has been achieved,thetwo parts of each leg can be locked together by means of a respective friction clamp operated bya respective handle 6C, 8C, 100 and 12C (the latter not visible in Figure 1).Each lower leg part 6A, 8A, 10A, 12Aterminates in a respective foot 6D, 8D, 1 OD, 1 2D, the feet being in the form of respective circular discs which are pivoted to the distal ends of the lower leg parts by respective ball and socket joints.
The upper parts6B,8B,10B,12B are attached to a cruciform-shaped base 14. The base 14 has four wings 14A, 14B, 14C, 14D each of which is made up of a respective pair of side plates between which are spective one ofthe upper leg parts 6B,8B,10B,12B extends. A bolt 16 extends between the two side platesofthewing 14Aand passes through holes at the distal end (not visible) ofthe upper leg part 6B, thus pivotally supporting the leg 6 and attaching itto the base 14. The other legs 8,10 and 12 are pivotally supported to the otherth ree wings 14B, 14C and 14D ofthe base in exactly similarfashion.
The upper and outer edges of the pair of side plates forming the wing 14A are joined together by a bridg- ing piece 17Aand a bridging piece 17Dsimilarlyjoins the side plates of wing 14D; the bridging pieces four wings 14B and 14C are not visible in Figure 1. Each bridging piece supports a block having a screwthreaded bore in which is engaged a correspondinglythreaded bolt having at its upper end a knob 18A, 18B, 18C, 18D by means of which it may be screwed in and out of the respective block.At its lower end, each bolt is attached, by means of a ball and socket joint, to a pad 20A,20B,20C,20D (pads 20B and 20C not being visible), the pads thus being in alignmentwith and capable of being screwed down into contact with the outer faces of the respective upper parts 6B,8B,1 OB and 12B of the legs.
The antenna arrangement 22 is mounted on the base 14 by means of a column 24 (see Figure 2).Atits lower end, the column 24 is located in a mating part situated centrallyofthe base 14so asto befixed against rotation. The upper part ofthe column is rotatable relative to the lower part, after release of clamp 26 by means of a knob 28.
At its upper end, the column 24 supports an arm 40 carrying the main reflector 42 of the actual antenna.
The arm is attached to the upper end ofthe column 24 by a mechanism 44. The mechanism 44 is pivotally attached to column 24 and released and clamped via a knob 46. At the end of the arm 40 is mounted a hollow cone-shaped support 48 made of glassreinforced-plastics (GRP) material, more clearly shown in Figure 3. At its outer end, the sub-reflector dish 50 forthe antenna (shown dotted) is mounted and the open end ofthe support48 is closed offbya disc-shaped cover 52, such as also made ofGRP.
The support 48 is strengthened by means ofthree foam-filled GRP ribs 54 (only one shown, the others being arranged at 120 degree intervals around the outer surface ofthe cone).
Electrical connections are made to the antenna itself via the arm 40.
The coníplete assembly is set up by adjusting the effective lengths of each of the four legs 6,8,10, 12 by sliding the lower leg parts relative to the upper leg parts and then clamping them by means oftheclam- ping handles6C,8C,10C,12C.Thefeet6D,8D,10D, 1 2D adjust themselves so asto make firm contact with the ground. When the legs have been set up in this way, the knobs 18A, 18B, 18C and 18D are adju sted so as to bring the pads 20A, 20B, 20C, 20D into firm contact with the respective leg upper parts so as to secure the base 14 rigidly with respect to the legs.
The column 24 is thus rigidly supported in an approximately vertical attitude on the base 14. Thereafter, the knobs 28 and 46 areturned to release their respective clamps and the attitude of the antenna reflector42 is adjusted aboutthe horizontal and vertical axes by the means ofthe arm 40 accordingtothean- gular position ofthe satellite. The knobs 28 and 46 arethentightened to clamp the antenna.
As stated above, for effective operation it is es sentiai thatthe antenna, once adjusted, be supported art a constant attitude. Thewholestructuretherefore hasto be rigid. In particular,thestructure must be such that it remains firmly and constantly positioned on the ground. The antenna dish is of substantial size and the wind forces on the structure can therefore be quite considerable. It is found thatthe provision of four legs, in accordance with the invention, instead ofthe more usual three legs, provides considerably better support. Athree-legged support, although well able to accommodate different ground contours, provides a resistance to wind forces which varies according to the direction ofthe wind relative to the three legs.Such variation is much less pronounced with four legs. However, a problem with the use of four legs is that it is less easy to adjust them to suit variations in ground contour; not only must the lengths be adjusted but it is also necessary to provide adjustments to take account of the angle which each makes to the horizontal plane. This is achieved by arranging for the legs to be pivotally connected to the base 14 and by arranging forthe base 14to be firmly supported from the legs, afterthe legs have been set up, by means ofthe adjusting knobs 18A, 1 8B, 18C, 18D.
The assembly illustrated clearly has to be designed to copewith relatively rough handling and with frequent assembly and disassembly. It is particularly importantthatthe dish 42 and the sub-reflector 50 be held in the correct relationship with each other and that the sub-reflector be properly protected from damage. This is achieved by the GRP cone-shaped support48. It and the cover 52 enclose the subreflector 50 and rigidly support it in the correct position relative to the dish 42. At the sametime, however, the cone is effectively radio-transparent and sufficiently rigid yet light in weight.
Although the support (the part indicated generally at 5) has been described and illustrated as supporting a radio antenna, itwill be appreciated that it may instead be used for other purposes - wherever are latively rigid support is required for mounting on ground of variable contour.

Claims (18)

1. A portable support, comprising a base having fouradjustable-length legs pivotally depending therefrom and extending downwardly and outwardly into engagement with the ground, and adjustable means, individually adjustable relative to each said leg in accordance with its angular position relative to the base, for rigidly securing the base to the legs.
2. Asupportaccording to claim 1, in which each leg comprises two relatively slidable portions for adjusting its length, and means for releasably clamping the two portions of each leg together.
3. A support according to claim 1 or2, in which the distal end of each leg carries a respective groundengaging pad whose attitude relative to the distal end of the leg is adjustable.
4. A support according to any preceding claim, in which each adjusting means comprises means acting between the base and each leg and adjustable to prevent pivoting movement of that leg relative to the base in a direction tending to liftthe distal end ofthat leg from the ground.
5. A support according to claim 4, in which each adjusting means comprises screw-threaded means in screw-threaded engagement with the base so as to be capable of being screwed relative to the base into contact with an outer part of the respective leg at a point spaced down the leg from its point of pivotal attachmenttothe base.
6. Asupportaccording to any preceding claim, in which the base is of cruciform shape, comprising fourwings each of which has two side members spa- ced apart in the generally horizontal direction to provide a gap for receiving the upper end of a respective one of the legs, with the axis of pivoting of the leg passing between the two side members, and in which each screw-threaded means comprises are spective bolt screw-threadedly engaging a respective block between the respective pair of side members, the bolt having means at its upper end for rotat ingitanda leg-engaging pad at its lowerend.
7. Asupportaccording to any preceding claim, including mounting means for mounting a radio antenna arrangement on the base.
8. Asupportaccordingto claim 7, in whichthe mounting means comprises a column for mounting in a position upstanding from the base and in which the antenna comprises dish means supported from the column.
9. Asupportaccording to claim 8, in which the column is angularly movable about an up-standing axis so as to move the dish means correspondingly and in which the dish means is adjustable aboutan axis perpendicularto the upstanding axis.
10. Asupportaccordingto claim 8to 9, in which the dish means comprises a relatively large dish having its concave surface facing towards the convex surface of a coaxially positioned smaller dish.
11. Asupportaccording to claim 10, in which the smaller dish is enclosed within a support made of radio-transparent glass reinforced plastics material.
12. A support according to claim 11, in which the glass reinforced plastics material is cone-shaped with the said smaller dish mounted at its large diameter end.
13. A support according to claim 12, in which the cone-shaped glass-reinforced plastics material is strengthened by one or more foam4illed ribs.
14. A radio antenna arrangement comprising a dish-shaped reflector supported within and at the closed-offlargediameterend of a conically-shaped support made of radio4ransparent glass reinforced plastics material.
15. An antenna arrangement according to claim 15, in which the conically-shaped glass reinforced plastics material is strengthened by one or more foam-filled ribs running along its outside surface.
16. An antenna arrangementaccording to claim 14 or 15, in which the conically-shaped support supports the reflector cantilever4ashion with reference to a substantially larger antenna dish so that thesaid reflector acts as the sub-reflectorthereto.
17. A portable support, substantially as described with reference to the accompanying drawing.
18. A radio antenna arrangement, substantially as described with reference to the accompanying drawing.
GB8527026A 1985-11-01 1985-11-01 Portable supports such as for radio antennas Expired GB2182240B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8527026A GB2182240B (en) 1985-11-01 1985-11-01 Portable supports such as for radio antennas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8527026A GB2182240B (en) 1985-11-01 1985-11-01 Portable supports such as for radio antennas

Publications (3)

Publication Number Publication Date
GB8527026D0 GB8527026D0 (en) 1985-12-04
GB2182240A true GB2182240A (en) 1987-05-13
GB2182240B GB2182240B (en) 1989-10-25

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Family Applications (1)

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GB8527026A Expired GB2182240B (en) 1985-11-01 1985-11-01 Portable supports such as for radio antennas

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Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0452077A1 (en) * 1990-04-09 1991-10-16 Marconi Electronic Devices Limited Antenna arrangements
GB2432054A (en) * 2005-11-01 2007-05-09 John Cyril Watkin Portable ground mount for offset satellite dish
EP1973194A1 (en) 2007-03-23 2008-09-24 SPACE ENGINEERING S.p.A. A high efficiency antenna having compact dimensions, particularly for installation on a vehicle, such as an aircraft or a high velocity train or a motor vehicle
CN103185191A (en) * 2011-12-27 2013-07-03 富泰华工业(深圳)有限公司 Support structure
WO2021099058A1 (en) * 2019-11-22 2021-05-27 Rtl Materials Ltd Collapsible stand
US12031667B2 (en) 2019-11-22 2024-07-09 Rtl Materials Ltd Collapsible stand

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0452077A1 (en) * 1990-04-09 1991-10-16 Marconi Electronic Devices Limited Antenna arrangements
WO1991015880A1 (en) * 1990-04-09 1991-10-17 Marconi Electronic Devices Limited Antenna arrangements
GB2432054A (en) * 2005-11-01 2007-05-09 John Cyril Watkin Portable ground mount for offset satellite dish
GB2432054B (en) * 2005-11-01 2009-10-07 John Cyril Watkin Portable offset satellite antenna system
EP1973194A1 (en) 2007-03-23 2008-09-24 SPACE ENGINEERING S.p.A. A high efficiency antenna having compact dimensions, particularly for installation on a vehicle, such as an aircraft or a high velocity train or a motor vehicle
CN103185191A (en) * 2011-12-27 2013-07-03 富泰华工业(深圳)有限公司 Support structure
CN103185191B (en) * 2011-12-27 2016-08-31 富泰华工业(深圳)有限公司 Supporting construction
WO2021099058A1 (en) * 2019-11-22 2021-05-27 Rtl Materials Ltd Collapsible stand
US12031667B2 (en) 2019-11-22 2024-07-09 Rtl Materials Ltd Collapsible stand

Also Published As

Publication number Publication date
GB8527026D0 (en) 1985-12-04
GB2182240B (en) 1989-10-25

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Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 19941101