In an integrated telescoping mast-payload assembly, the payload forms the top telescoping section.

Patent
   RE37559
Priority
Oct 07 1991
Filed
Mar 31 1999
Issued
Feb 26 2002
Expiry
Oct 07 2011
Assg.orig
Entity
Small
25
31
all paid
0. 1. In a telescoping mast assembly, including:
a plurality of nesting, telescoping mast sections, including a top section and at least one lower section, each of said sections having upper and lower ends, and
means for extending and retracting each of said sections relative to the next-lower section,
the improvement comprising:
a payload, located only in said top section,
said top section, including said payload, being dimensioned to be received and nest within the next-lower section,
at least a portion of said payload being received within said next-lower section when said top section is fully retracted,
such that said next-lower section provides protection for said payload when said top section is fully retracted,
said payload being a member of the group consisting of radio antennas, lights, instrumentation and telemetry packages for robotic vehicles, television cameras, antenna rotators, preamplifiers, radiation sensors and electronic and electro-mechanical instrument packages.
0. 6. A telescoping mast-payload assembly for reducing the retracted height of a mast-payload assembly and for providing protection of a payload when said mast-payload assembly is fully retracted, said mast-payload assembly comprising:
(a) a telescoping mast component extending and retracting along the mast's longitudinal axis defining a mast axis, said telescoping mast component comprising:
a telescoping mast, adapted to telescope upwardly along said mast axis to an extended position and to telescope downwardly along said mast axis to a retracted position, said telescoping mast comprising:
a fixed bottom section being shaped and dimensioned to include a hollow region for telescopically receiving a next higher mast section;
a plurality of extending and retracting intermediate mast sections, each section having upper and lower ends and being shaped and dimensioned to include a hollow region for telescopically receiving the next higher mast section; and
an extending and retracting payload section defining the top section of said telescoping mast, said payload section shaped and dimensioned to be telescopically received within the hollow region of the uppermost section of said intermediate sections;
said intermediate support sections and said payload section being constructed to telescopically retract along said mast axis within the hollow region of the next lower mast section and to telescopically extend along said mast axis above the next lower mast section, said plurality of intermediate support sections supporting said payload section when said mast is extended to said extended position and receiving and protecting said payload section when said top section is fully retracted; and
(b) a payload component of said assembly forming at least a portion of said payload section and being located only in said payload section, said payload component being shaped and dimensioned to extend along said mast axis to be supported above the next-lower support section when said mast-payload assembly is extended to said extended position and to retract along said mast axis and to be at least partially received and protected within said intermediate support sections when said mast is fully retracted.
0. 18. A vehicular mounted telescoping mast-payload assembly for reducing the retracted height of a mast-payload assembly and for providing protection of a payload when said mast-payload assembly is fully retracted, said mast-payload assembly comprising:
(a) a telescoping mast component extending and retracting along the mast's longitudinal axis defining a mast axis, said telescoping mast component comprising:
a telescoping mast, adapted to telescope upwardly along said mast axis to an extended position and to telescope downwardly along said mast axis to retracted position, said mast comprising:
a fixed bottom section being shaped and dimensioned to include a hollow region for telescopically receiving a next higher mast section;
an extending and retracting intermediate mast section, said section having an upper and lower end and being shaped and dimensioned to include a hollow region for telescopically receiving a next higher mast section; and
an extending and retracting payload section defining the top section of said telescoping mast, said payload section shaped and dimensioned to be telescopically received within the hollow region of the uppermost section;
said intermediate support sections and said payload section being constructed to telescopically retract along said mast axis within the hollow region of the next lower mast section and to telescopically extend along said mast axis above the next lower mast section, said intermediate support section supporting said payload section when said mast is extended to said extended position and receiving and protecting said payload section when said mast is fully retracted;
(b) a payload component of said assembly forming at least a portion of said payload section and being located only in said payload section, said payload component being shaped and dimensioned to extend along said mast axis to be supported above the next-lower support section when said mast-payload assembly is extended to said extended position and to retract along said mast axis and to be at least partially received and protected within said intermediate support section when said mast is fully retracted; and
(c) attachment means for attaching said bottom section to a vehicle.
0. 12. A telescoping mast-payload assembly for reducing the retracted height of a mast-payload assembly and for providing protection of a payload when said mast-payload assembly is fully retracted, said mast-payload assembly comprising:
(a) a telescoping mast component extending and retracting along the mast's longitudinal axis defining a mast axis, said telescoping mast component comprising:
a telescoping mast, adapted to telescope upwardly along said mast axis to an extended position and to telescope downwardly along said mast axis to a retracted position, said telescoping mast comprising:
a fixed bottom section being shaped and dimensioned to include a hollow region for telescopically receiving a next higher mast section;
a plurality of extending and retracting intermediate mast sections, each section having upper and lower ends and being shaped and dimensioned to include a hollow region for telescopically receiving the next higher mast section; and
an extending and retracting payload section defining the top section of said telescoping mast, said payload section shaped and dimensioned to be telescopically received within the hollow region of the uppermost section of said intermediate sections;
said intermediate support sections and said payload section being constructed to telescopically retract along said mast axis within the hollow region of the next lower mast section and to telescopically extend along said mast axis above the next lower mast section, said plurality of intermediate support sections supporting said payload section when said mast is extended to said extended position and receiving and protecting said payload section when said mast is fully retracted;
(b) a payload component of said assembly forming at least a portion of said payload section and being located only in said payload section, said payload section being shaped and dimensioned to extend along said mast axis to be supported above the next-lower support section, when said mast-payload assembly is extended to said extended position and to retract along said mast axis and to be at least partially received and protected within said intermediate support sections when said mast is fully retracted; and
(c) motor drive means for extending and retracting said payload section and said intermediate support sections relative to said bottom section.
0. 2. The assembly of claim 1 mounted on a vehicle.
0. 3. The assembly of claim 1, in which said payload is an antenna for electromagnetic energy.
0. 4. The assembly of claim 1, in which said lower section is radiopaque.
0. 5. The assembly of claim 1 which further includes:
(a) a transmission line cable for transmitting a signal to or from said payload; and
(b) a sub-assembly for stowing and dispensing said cable when said mast assembly is retracted and extended.
0. 7. The telescoping mast-payload assembly of claim 6 wherein the payload is a member of the group consisting of radio antennas, lights, television cameras, antenna rotators, preamplifiers, radiation sensors, instrumentation and telemetry packages for robotic vehicles, and electronic and electro-mechanical instrument packages.
0. 8. The telescoping mast-payload assembly of claim 6 wherein the payload is a radio antenna.
0. 9. The telescoping mast-payload assembly of claim 8 being mounted on a vehicle.
0. 10. The telescoping mast-payload assembly of claim 6 being mounted on a vehicle.
0. 11. The telescoping mast-payload assembly of claim 6, further including motor drive means for extending and retracting said payload section and said intermediate support sections relative to said bottom section.
0. 13. The telescoping mast-payload assembly of claim 12 wherein the payload is a member of the group consisting of radio antennas, lights, television cameras, antenna rotators, preamplifiers, radiation sensors, instrumentation and telemetry packages for robotic vehicles, and electronic and electro-mechanical instrument packages.
0. 14. The telescoping mast-payload assembly of claim 13 being mounted on a vehicle.
0. 15. The telescoping mast-payload assembly of claim 13 wherein the payload is a radio antenna.
0. 16. The telescoping mast-payload assembly of claim 15 being mounted on a vehicle.
0. 17. The telescoping mast-payload assembly of claim 12 further comprising:
a transmission line cable for transmitting a signal to or from said payload; and
a subassembly for stowing and dispensing said cable when said mast assembly is retracted and extended.
0. 19. The telescoping mast-payload assembly of claim 18 wherein the payload is a member of the group consisting of radio antennas, lights, television cameras, antenna rotators, preamplifiers, radiation sensors, instrumentation and telemetry packages for robotic vehicles, and electronic and electro-mechanical instrument packages.
0. 20. The telescoping mast-payload assembly of claim 19 further comprising:
a transmission line cable for transmitting a signal to or from said payload; and
a subassembly for stowing and dispensing said cable when said mast assembled is retracted and extended.
0. 21. The telescoping mast-payload assembly of claim 18 wherein the payload is a radio antennae.
0. 22. The telescoping mast-payload assembly of claim 18, further including motor drive means for extending and retracting said payload section and said intermediate support section relative to said bottom section.

This application

Briefly, in accordance with the broadest aspects of the invention, I provide an integrated telescoping mast-payload assembly comprising at least two or more nesting, telescoping mast sections, each section having an upper end and a lower end. The telescoping sections include one or more lower sections and a top section which is dimensioned to slidably nest within the next-lower section. Means are provided for extending and retracting the top section relative to the next-lower section and each of the lower sections relative to the section next below (except for the bottom section). A payload forms at least the upper end of the top section and at least a portion of the payload is received within the next-lower section when the top section is fully retracted. The lower section or sections provide protection for the payload when the top section is fully retracted.

According to a preferred embodiment, the assembly is mounted upon or in a vehicle or upon or in a transportable shelter.

In another presently preferred embodiment, the payload is an antenna for transmitting and/or receiving electro-magnetic energy such as radio signals.

In yet another preferred embodiment, one or more of the lower sections is radiopaque to shield the payload from stray electro-magnetic radiation, particularly EMP, when the assembly is retracted.

According to the best mode contemplated at present, the integrated mast-payload assembly includes means for mechanical locking the upper and lower sections together when the upper section is fully extended and when it is fully retracted, but preventing relative sequentially movement between the sections when the upper section is between the fully retracted and fully extended positions.

In another preferred embodiment of the invention, when the nature of the payload prevents forming it with a central longitudinal parameter, a plurality of axial drive screws (at least two), are employed and these drive screws are laterally spaced from the longitudinal center line of the telescoping mast sections.

The drawings are provided to further illustrate to those skilled in the art how to make and use the invention and are not intended as a limitation on the scope of the invention. In the drawings, like reference characters identify the same elements in the several views.

Referring to FIGS. 1-3, the telescoping mast-payload assembly, generally indicated by reference numeral 10 includes a bottom mast section 11, a top mast section 12 and one or more lower sections 13-19. Each of the mast sections 12-19 is dimensioned to be slidably received within the next-lower section. The top section 12 and each of the one or more lower sections 13-19 can be extended and retracted relative to the next lower section from a fully retracted position, as shown in FIGS. 1-2 to a fully extended position (not shown). A single axial drive screw 21, which is rotated by operation of an electric motor 22 which transmits rotational force through a drive train 23, engages nuts 24 carried internally at the bottom end of each of the mast sections 12-19. Rotation of the axial drive screw 21 causes upward or downward movement of the nuts 24 on the drive screw 21 and corresponding relative motion of the mast section associated with each of the nuts 24. Holddown locking mechanisms 25 are provided to cause sequential deployment and retraction of each of the mast sections 12-19, to lock adjacent sections together when the mast is fully nested and when each section is fully extended relative to its next-lower section. A cable stowage/dispensing sub-assembly 31 includes an elongate frame 32, a moveable multi-sheave pulley 33 and a spring 34 connected to the pulley 33 which urges the pulley 33 downwardly in the direction of the arrow A. The transmission line cable 35 is connected at its upper end to the connector portion 36 of a antenna element 37 which forms the hollow antenna element which forms the upper section of the telescoping assembly 10. The transmission line passes into the frame 32 forming windings 38 on the moveable pulley 33 and stationary pulley 39. A terminal portion 41 of the cable 35 is fixed by means of a hook 42 to the frame 32 and passes through an outlet aperture 43 to its point of connection with another component, e.g., radio transceiver, (not shown). Further details of the operation of the drive components 21-24, the locking devices 25 and the cable stowage/dispensing assembly 32 are disclosed in the published international application No. PCT/US92/08721 (International Publication Number WO 93/07395, published 15 Apr. 1993), which is incorporated herein by reference.

FIGS. 4a-4c depict the top section 12 of the telescoping mast of FIGS. 1-3, the major length thereof being formed as a hollow cylinder 42 having a longitudinal bore 42. At the lower end 43 the diameter of the bore 42 is increased to provide a socket 44 which receives a nut which engages threads on the axial drive screw 21. The annular shoulder 45 cooperates with the locking mechanism on the upper end of mast section 13, in the manner previously described, a key 46 is formed as a longitudinal shoulder on the outer surface of the cylindrical section 41 to prevent rotation of the upper section 12. The upper end 47 of the top section 12 is provided with a coaxial connector 48 for attaching to rf transmission cable 35 with the rf rotated/receiving components which are embedded into side walls 49 of the top section 12.

FIG. 5 depicts the integrated mast-payload assembly 10 of FIGS. 1-4, mounted externally on the rear wall 51 of an SICPS shelter 52 carried on a suitable vehicle, e.g., the HMMWV/CUCV transporter. Alternatively, as depicted in FIG. 6, the assembly 10 can be mounted within a special radio antenna enclosure, indicated by the dash lines 61 of an enclosed vehicle such as the Bradley C2V. In either case, the electrical power lines, and control cables for the drive mechanism 22 and the coaxial cable 35 are routed through the bulkheads 51 (FIG. 5) or 63 (FIG. 6) to the interior of the vehicle, which protectively houses the human operators, such that the mast and payload can be extended and retracted from within vehicles 52, 62, without requiring personnel to operate outside these shelters.

Another embodiment of the invention is depicted in FIGS. 7-11. This embodiment is useful when the character of the payload does not permit it to be formed as a hollow cylinder (as shown in FIG. 4).

As shown in FIGS. 7-11, a complex payload such as the J-STARS SCDL antenna 71 is operatively mounted on a base 72. The antenna 71 and base 72 form the upper section 73 of a multi-section telescoping mast comprising a plurality of intermediate lower sections 73 and a bottom section 74, each of the sections 72-74 are formed of aluminum frame members 75, covered and stiffened by graphite composite panels 76. Alternatively, panels 76 can be omitted, thereby reducing the wind load on the mast. The extended assembly of FIG. 7 is shown in cross-section in FIGS. 8 and 10 and in a side view in FIG. 9. In the embodiment of FIG. 7-9, the antenna cable 35 is preformed as an extensible coil 77. Power to extend and retract the assembly is provided by an electric motor 78 and associated drive mechanism 79. As shown in FIG. 11, the assembly of FIGS. 7-10 can also be mounted internally of a radio antenna well 91 formed in an appropriate vehicle such as the C2V Bradley.

Marue, Edward A., Pereira, Kenneth J.

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7989979, Apr 28 2004 The Will-Burt Company; WILL-BURT COMPANY,THE Pneumatically telescoping mast having DC operated controls
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Patent Priority Assignee Title
1426276,
2499137,
2861268,
3158865,
3347003,
3373285,
3688455,
388491,
4062156, Jan 30 1976 Dornier System GmbH Extensible rod
4180850, Jun 29 1978 The Toro Company Retractable light fixture
4254423, Oct 01 1977 Vereinigte Flugtechnische Werke-Fokker GmbH Telescopic equipment carrier including antennas
4577827, Oct 26 1979 Lois G. Langley Camera holder apparatus
4663900, Dec 16 1985 LIQUID CARBONIC CORPORATION, A DE CORP Locking mast and stop ring assembly
4725846, Dec 12 1986 HENDERSHOT, JAMES R Disguise antenna operating in the cellular band
4871138, Mar 14 1987 DORNIER GMBH, KLEEWEG 3, D-7990 FRIEDRICHSHAFEN 1, WEST GERMANY Telescopic device with unambiguous sequence of deployment and retraction
4932176, Sep 19 1988 General Dynamics Government Systems Corporation Extendible and retractible mast system
5101215, May 10 1985 Chu Associates, Inc.; CHU ASSOCIATES, INC Telescoping lightweight antenna tower assembly and the like
5117595, Feb 20 1989 Geroh GmbH Mechanische Systeme Device for erecting and aligning a tilting telescopic mast mounted on a transport vehicle
5163650, Oct 07 1991 STAINLESS, INC Telescoping mast with improved holddown-locking mechanism
5168679, Sep 10 1990 The Will-Burt Company Telescoping mast assembly
5218375, Nov 15 1991 Antenna Products Corporation Rapidly extendible and retractable antenna mast
797464,
CA671611,
DE1260800,
DE3434517,
DE3611810,
DE3636893,
FR1430168,
FR2555820,
FR2575780,
GB124268,
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Executed onAssignorAssigneeConveyanceFrameReelDoc
Mar 23 2000TRI-EX TOWER CORPORATION, A CALIFORNIA CORPORATIONWILL-BURT COMPANY, AN OHIO CORPORATION, THEASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0107850010 pdf
Aug 25 2017The Will-Burt CompanyJPMORGAN CHASE BANK, N A SECURITY INTEREST SEE DOCUMENT FOR DETAILS 0434330753 pdf
Mar 17 2022JPMORGAN CHASE BANK, N A The Will-Burt CompanyRELEASE BY SECURED PARTY SEE DOCUMENT FOR DETAILS 0592980066 pdf
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