WO1996018565A1 - A crane assembly - Google Patents

A crane assembly Download PDF

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Publication number
WO1996018565A1
WO1996018565A1 PCT/US1995/009243 US9509243W WO9618565A1 WO 1996018565 A1 WO1996018565 A1 WO 1996018565A1 US 9509243 W US9509243 W US 9509243W WO 9618565 A1 WO9618565 A1 WO 9618565A1
Authority
WO
WIPO (PCT)
Prior art keywords
crane
assembly
building
carriage
along
Prior art date
Application number
PCT/US1995/009243
Other languages
French (fr)
Inventor
James K. Arnold
Paul R. Shumacher
Original Assignee
Lockheed Corporation
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 Lockheed Corporation filed Critical Lockheed Corporation
Priority to KR1019970700407A priority Critical patent/KR100196982B1/en
Priority to NZ290615A priority patent/NZ290615A/en
Priority to BR9508476A priority patent/BR9508476A/en
Priority to MX9606561A priority patent/MX9606561A/en
Priority to AU31404/95A priority patent/AU685313B2/en
Priority to EP95927350A priority patent/EP0797537B1/en
Priority to RU97111797A priority patent/RU2136576C1/en
Priority to JP51351896A priority patent/JP3242113B2/en
Priority to DE69519308T priority patent/DE69519308T2/en
Publication of WO1996018565A1 publication Critical patent/WO1996018565A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66CCRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
    • B66C17/00Overhead travelling cranes comprising one or more substantially horizontal girders the ends of which are directly supported by wheels or rollers running on tracks carried by spaced supports
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64FGROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
    • B64F5/00Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
    • B64F5/10Manufacturing or assembling aircraft, e.g. jigs therefor

Definitions

  • the invention relates to the field of overhead crane assemblies for buildings and the like and, in particular, to a crane assembly useful in the manufacture of gas bags for lighter than air vehicles.
  • Non-rigid vehicles There are basically two types of Lighter-than-air vehicles; rigid or non-rigid. There are three general types of non-rigid vehicles: those comprising a single gas filled bag; several gas bags joined together in series; and, of course, those having a multiple number gas bags within a non-rigid envelope. In non-rigid designs, the flight station and cargo compartments are suspended from the bottom of the vehicle, in what is most often referred to as a gondola.
  • the gas bag is typically assembled from rolls of small strips of cloth impregnated with a resin. These strips of cloth are laid out, cut to length and joined to form larger portions of the gas bag. These portions, in turn, are joined to each other to form even larger segments of the gas bag.
  • catenary curtains, doublers, various attachment fittings, and etc. are joined thereto.
  • larger segments of the gas bag are joined together, such large items as ballonets are joined thereto.
  • the assembled segment has grown so large it covers the entire available floor space of any reasonably sized building.
  • manually handling extremely large segments for example a segment 800 feet in length and 60 feet in width on a floor is next to impossible.
  • the segments thereof must be raised above the floor to ease final assembly, which involves the seaming of these very large segments together.
  • the invention is a crane system for a building used for the assembly of a gas bag for a lighter-than-air vehicle, the building having a floor and a roof thereover with a longitudinal, vertical and lateral axis.
  • the crane assembly includes a plurality of crane carriage rail assemblies in the form of arches aligned with the lateral axis of and mounted within the building.
  • the rail assemblies are in a spaced relationship along the 3 longitudinal axis with each one incorporating a rack gear extending generally along its entire length.
  • a plurality of crane carriage assembly are movably mounted on each of the rail assemblies with each carriage assembly including a winch mounted thereon having an extendible and retractable cable.
  • a motor is mounted on each of the crane assemblies for driving it over the rail assemblies, preferably by driving a pinion gear in engagement with the rack gear on the rail assembly.
  • a position sensor on the carriage assembly determines its position along the rail assembly.
  • Each carriage assembly includes a cable position sensor.
  • a control system is provided, preferably a computer controlled for moving the carriage assemblies by rows aligned with the longitudinal axis of the building along the rail assemblies to specific locations along the lateral axis. The control system further adjusts the extended length of the cables from the winches in each of the rows as a function of the position of each of the rows of carriage assemblies along the lateral axis.
  • the winch cables of the first row of carriage assemblies are extended to a preset length and manually attached to the segment via attachment fitting located along its length.
  • the carriage assemblies are then moved to a first position, with a simultaneous adjustment in the length of the cables, lifting the first segment partially off the floor of the building.
  • a second segment is completed, it is joined to the first segment.
  • the first row of carriage assemblies are moved to a second position raising the first segment completely off the floor.
  • the winch cables of the second row of carriage assemblies are then extended and attached to the second segment, and thereafter the first and second carriage assemblies are moved further along the rails assemblies, with of course, a simultaneous adjustment of the cables. This process is continued until all the segments are joined end to end and lifted of the floor.
  • the motors of the crane carriage assemblies, as well as the motors used to adjust cable length, can be easily controlled by means of a micro-processor
  • the micro-processor need only be preprogrammed with library values for the carriage assemblies positions and cable lengths at the various stages of gas bag assembly and provide control signals via motor controllers based on inputs from the position sensors. However, more sophisticated control systems may be used.
  • Figure 1 is a simplified perspective view of a building suitable for assembling the gas bag for a lighter-than-air vehicle.
  • Figure 2 is a view of the floor of the building shown in Figure 1 illustrating segments of a gas bag for a lighter than air vehicle in various stages of assembly.
  • Figure 3 is a partial side view of one of the crane carriage rail assemblies shown in Figure 1 taken along the arrow 3.
  • Figure 4 is a partial cross-sectional view of the crane carriage rail assembly shown in Figure 3 taken along the line 4-4.
  • Figure 5 is a partial cross-sectional view of the crane carriage rail assembly shown in Figure 3 taken along the line 5-5.
  • Figure 6 is a semi-schematic representation of the subject crane assembly lifting the first completed segment off the floor of the building.
  • Figure 7 is a semi-schematic representation of the subject crane assembly shown in Figure 6 lifting the first three completed segments off the floor of the building.
  • Figure 8 is a semi-schematic representation of the subject crane assembly shown in Figure 6 lifting all the segments of the gas bag off the floor of the building.
  • Figure 9 is a semi-schematic representation of the subject crane assembly shown in Figure 6 wherein the segments of the gas bag are fully joined into the cylindrical portion of the gas bag.
  • Figure 10 is a block diagram of the control system for the crane assembly.
  • Figure 1 1 is a simplified crane position library of positions for a computer suitable for running the control system. DESCRIPTION OF THE PREFERRED EMBODIMENT
  • FIG 1 Illustrated in Figure 1 is a perspective view of the building for the assembly of the gas bag for a lighter than air vehicle, generally designated by numeral 20.
  • the building 20 includes a floor 22, arched roof 24 having a longitudinal axis 26A, vertical axis 26B and lateral axis 26C.
  • the building includes a plurality of crane rail assemblies 30 through 38 with each rail assembly having a plurality of crane carriage assemblies 40A-40I, through 48A-48I.
  • Figure 2 which is a view of the floor 22 of the building 20 shown in Figure 1
  • the gas bag is assembled from subsections 50, 52, 53, 54, and 55, which in turn are assembled from individual strips 56 of a composite cloth impregnated with a thermoplastic resin.
  • the strips of cloth 56 are butt joined together to form strips 58 of sufficient length to form the subsections 50-55.
  • the subsections 50-55 are themselves joined together to form a segment 60A which is then moved to the opposite side of the floor.
  • the ballonets 62 as well as all other fittings such as catenary curtains, vent ports etc. are added.
  • the segments 60A can range up to 700 to 800 feet in length and 60 to 100 feet in width. Thus it is readily apparent that the assembly of these segments would normally require an extremely large building. However, by use of the subject crane assembly, the size of the gas bag assembly building can be kept to a reasonable size.
  • the crane rail assembly for example rail assembly 30, includes dual rails 70A and 70B in a spaced relationship supported by a central frame 71 , having upper tracks 72A and 72B and lower tracks 74A and 74B.
  • a rack gear 76 is located on the bottom of the frame 71.
  • the crane carriage assembly, for example carriage assembly 40A on rail assembly 30, includes carriage frame 80 having twin support members 81 A and 81 B.
  • the member 81 A supports upper wheels 82A and 82B which ride on track 72A and lower wheels 83A and 83B that ride on track 74A.
  • the member 81 B supports upper wheels 84A and 84B which ride on track 72B and lower wheels 86A and 86B which ride on track 74B.
  • a motor 87 is mounted on the frame 80 that drives a pinion gear 88 via a transmission 90 and, thus drives the carriage assembly 40A along the rail assembly 30.
  • a position sensor 92 mounted to the motor 87 provides carriage assembly position indication along the carriage rail assembly 30.
  • a clevis 94 is mounted at the bottom of the frame 80 that supports a winch 96 having a cable 98.
  • a motor 100 drives the wench via a shaft 102 through a transmission 104.
  • a second position sensor 106 mounted on the motor 100 provides an indication of the position of the end of the cable 98.
  • electrical power to the carriage assembly 40A is provided by a trolley car type electrical connector 110 which is mounted to the member 81 A and has an electrical contact head 112 that rides in a groove 1 14 and makes contact with conductors 116A and 116B mounted on insulator 117. Not only can power be provided to the motors 87 and 96, but position indication from the position indicators 92 and 106 can be transmitted out.
  • the winch cables 98 of the first row of carriage assemblies 40A through 48A are extended to a preset length and manually attached to the segment via attachment fittings (not shown) located along its length (shown in dotted lines).
  • the carriage assemblies 40A-48A are then moved to a first position, with a simultaneous adjustment in the length of the cables 98, lifting the segment 60A partially off the floor 22..
  • a second segment 60B is completed, it is joined to the segment 60A.
  • the carriage assemblies 40A-48A are moved to a second position raising the first segment 60A completely off the floor 22
  • the winch cables 98 of the carriage assemblies 40B-48B are then extended and attached to the second segment. 60B and thereafter the carriage assemblies 40A-48A and 40B-48B are moved further along the carriage rails 30-38, with a simultaneous adjustment of the cables 98.
  • segments 60A-C have been completed, with segments 60A and 60B lifted completely of the floor 22 and with segment 60C lifted partially thereof by carriage assemblies 40C-48C.
  • the process is continued until all the segments 60A-60I have been completed and joined together end to end and raised off the floor 22.
  • cables 120 and 122 of floor mounted winches 124 and 126 are coupled to the segments 60A and 60I, respectively.
  • the free ends of the segments 60A and 601 are then pulled down to the center area 128 of the floor 22 by the winches 124 and 126 as the cables 98 of the winches 96 in the carriage assemblies 40A-48A through 40I-48I are readjusted to accommodate the segment movement.
  • the free ends of the segments 60A and 60I are joined together to form the cylindrical portion of the gas bag. Thereafter the completed gas bag can be raised completely off the floor 22 for subsequent manufacturing operations. While the gas bag is far from complete, (at this point, end segments have not been joined), the subject crane assembly has allowed the main section of the gas bag to be easily assembled.
  • the motors 87 of crane carriage assemblies 40A-I through 48A-I, as well as the motors 96 used to adjust cable 98 length, can be easily controlled by means of a micro-processor 130.
  • the micro-processor 130 need only be preprogrammed with library values 131 shown in Figure 11 , for the their respective positions at the various stages of gas bag assembly and provide control signals via motor controllers 132 and 134 based on inputs from the position sensors 92 and 106. However, more sophisticated control systems may be used.
  • the invention has applicability to the aircraft construction industry.

Landscapes

  • Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Mechanical Engineering (AREA)
  • Transportation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Conveying And Assembling Of Building Elements In Situ (AREA)
  • Carriers, Traveling Bodies, And Overhead Traveling Cranes (AREA)
  • Air Bags (AREA)
  • Tents Or Canopies (AREA)
  • Control And Safety Of Cranes (AREA)

Abstract

The invention is a crane system for a building (20) for the assembly of a gas bag for a lighter-than-air vehicle, the building (20) having a floor (22) and a roof (24) thereover with a longitudinal, vertical and lateral axis (26A, B, C). In detail, the crane assembly includes a plurality of crane carriage rail assemblies (30-38) in the form of arches aligned with the lateral axis (26C) of and mounted within the building (20). The carriage rail assemblies (30-38) are in a spaced relationship along the longitudinal axis (26A). A plurality of crane carriages (40A-I to 48A-I) are movably mounted on each of the crane rail assemblies (30-38) with each carriage including winch (96) mounted thereon having an extendible and retractable cable (98). A control system is provided for moving the crane carriages (40A-I to 48A-I) by rows aligned with the longitudinal axis (26A) of the building (20) along the crane carriage rail assemblies (30-38) to specific locations along the lateral axis (26C) and for adjusting the length of the cables (98) of the winches (96) in each of the rows as a function of the distance of each of the rows along the lateral axis (26C) of the building (20).

Description

A CRANE ASSEMBLY
BACKGROUND OF THE INVENTION
Field of the Invention
The invention relates to the field of overhead crane assemblies for buildings and the like and, in particular, to a crane assembly useful in the manufacture of gas bags for lighter than air vehicles.
Description of Related Art
There are basically two types of Lighter-than-air vehicles; rigid or non-rigid. There are three general types of non-rigid vehicles: those comprising a single gas filled bag; several gas bags joined together in series; and, of course, those having a multiple number gas bags within a non-rigid envelope. In non-rigid designs, the flight station and cargo compartments are suspended from the bottom of the vehicle, in what is most often referred to as a gondola.
One of the main problems in the manufacture of large single gas bag non-rigid vehicles occurs during final assembly thereof. The gas bag is typically assembled from rolls of small strips of cloth impregnated with a resin. These strips of cloth are laid out, cut to length and joined to form larger portions of the gas bag. These portions, in turn, are joined to each other to form even larger segments of the gas bag. During this build up process, catenary curtains, doublers, various attachment fittings, and etc. are joined thereto. As larger segments of the gas bag are joined together, such large items as ballonets are joined thereto. Finally one gets to a point wherein the assembled segment has grown so large it covers the entire available floor space of any reasonably sized building. Furthermore, manually handling extremely large segments, for example a segment 800 feet in length and 60 feet in width on a floor is next to impossible. Thus during final assembly, the segments thereof must be raised above the floor to ease final assembly, which involves the seaming of these very large segments together.
Thus it is a primary object of the subject invention to provide an over head crane assembly.
It is another primary object of the subject invention to provide an over head crane assembly for supporting portions of a gas bag for a lighter- than-air vehicle during assembly.
It is a further object of the subject invention to provide an over head crane assembly for supporting portions of a gas bag for a lighter-than-air vehicle during assembly that is computer controlled.
SUMMARY OF THE INVENTION
One of the methods that has been proposed for manufacturing a cylindrical portion of extremely large non-ridged cylindrical gas bags for lighter-than-air vehicles is to heat seam portions of the gas bag until a full length segment of the cylindrical portion of the gas bag is completed. Thereafter, the completed, these large segments would be heat seemed together. As previously mentioned, when the completed cylindrical segments of the gag bag are very large, final assembly becomes difficult. However, by use of the subject crane system, many of the handling problems are eliminated.
The invention is a crane system for a building used for the assembly of a gas bag for a lighter-than-air vehicle, the building having a floor and a roof thereover with a longitudinal, vertical and lateral axis. In detail, the crane assembly includes a plurality of crane carriage rail assemblies in the form of arches aligned with the lateral axis of and mounted within the building. The rail assemblies are in a spaced relationship along the 3 longitudinal axis with each one incorporating a rack gear extending generally along its entire length.
A plurality of crane carriage assembly are movably mounted on each of the rail assemblies with each carriage assembly including a winch mounted thereon having an extendible and retractable cable. A motor is mounted on each of the crane assemblies for driving it over the rail assemblies, preferably by driving a pinion gear in engagement with the rack gear on the rail assembly. A position sensor on the carriage assembly determines its position along the rail assembly. Each carriage assembly includes a cable position sensor. A control system is provided, preferably a computer controlled for moving the carriage assemblies by rows aligned with the longitudinal axis of the building along the rail assemblies to specific locations along the lateral axis. The control system further adjusts the extended length of the cables from the winches in each of the rows as a function of the position of each of the rows of carriage assemblies along the lateral axis.
When the first segment is completed, the winch cables of the first row of carriage assemblies are extended to a preset length and manually attached to the segment via attachment fitting located along its length. The carriage assemblies are then moved to a first position, with a simultaneous adjustment in the length of the cables, lifting the first segment partially off the floor of the building. After a second segment is completed, it is joined to the first segment. The first row of carriage assemblies are moved to a second position raising the first segment completely off the floor. The winch cables of the second row of carriage assemblies are then extended and attached to the second segment, and thereafter the first and second carriage assemblies are moved further along the rails assemblies, with of course, a simultaneous adjustment of the cables. This process is continued until all the segments are joined end to end and lifted of the floor. At this point, cables from two rows of floor mounted winches are coupled to the free ends of the first and last segments. The free ends of the these segments are then pulled down to the center area of the floor by floor mounted winches as the cables of the winches in the carriage assemblies are readjusted to accommodate the segment movement. Thereafter, the free ends of the first and last segments are joined together to form the cylindrical portion of the gas bag. Thereafter the completed gas bag can be raised completely off the floor for subsequent manufacturing operations. While the gas bag is far from complete, (at this point, end segments have not been joined), the subject crane assembly allows the main section of the gas bag to be easily assembled.
The motors of the crane carriage assemblies, as well as the motors used to adjust cable length, can be easily controlled by means of a micro- processor The micro-processor need only be preprogrammed with library values for the carriage assemblies positions and cable lengths at the various stages of gas bag assembly and provide control signals via motor controllers based on inputs from the position sensors. However, more sophisticated control systems may be used.
The novel features which are believed to be characteristic of the invention, both as to its organization and method of operation, together with further objects and advantages thereof, will be better understood from the following description in connection with the accompanying drawings in which the presently preferred embodiment of the invention is illustrated by way of example. It is to be expressly understood, however, that the drawings are for purposes of illustration and description only and are not intended as a definition of the limits of the invention.
BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a simplified perspective view of a building suitable for assembling the gas bag for a lighter-than-air vehicle. Figure 2 is a view of the floor of the building shown in Figure 1 illustrating segments of a gas bag for a lighter than air vehicle in various stages of assembly.
Figure 3 is a partial side view of one of the crane carriage rail assemblies shown in Figure 1 taken along the arrow 3.
Figure 4 is a partial cross-sectional view of the crane carriage rail assembly shown in Figure 3 taken along the line 4-4.
Figure 5 is a partial cross-sectional view of the crane carriage rail assembly shown in Figure 3 taken along the line 5-5.
Figure 6 is a semi-schematic representation of the subject crane assembly lifting the first completed segment off the floor of the building.
Figure 7 is a semi-schematic representation of the subject crane assembly shown in Figure 6 lifting the first three completed segments off the floor of the building.
Figure 8 is a semi-schematic representation of the subject crane assembly shown in Figure 6 lifting all the segments of the gas bag off the floor of the building. Figure 9 is a semi-schematic representation of the subject crane assembly shown in Figure 6 wherein the segments of the gas bag are fully joined into the cylindrical portion of the gas bag.
Figure 10 is a block diagram of the control system for the crane assembly.
Figure 1 1 is a simplified crane position library of positions for a computer suitable for running the control system. DESCRIPTION OF THE PREFERRED EMBODIMENT
Illustrated in Figure 1 is a perspective view of the building for the assembly of the gas bag for a lighter than air vehicle, generally designated by numeral 20. The building 20 includes a floor 22, arched roof 24 having a longitudinal axis 26A, vertical axis 26B and lateral axis 26C. The building includes a plurality of crane rail assemblies 30 through 38 with each rail assembly having a plurality of crane carriage assemblies 40A-40I, through 48A-48I. Referring to Figure 2, which is a view of the floor 22 of the building 20 shown in Figure 1 , the gas bag is assembled from subsections 50, 52, 53, 54, and 55, which in turn are assembled from individual strips 56 of a composite cloth impregnated with a thermoplastic resin. The strips of cloth 56 are butt joined together to form strips 58 of sufficient length to form the subsections 50-55. The subsections 50-55 are themselves joined together to form a segment 60A which is then moved to the opposite side of the floor. Here the ballonets 62 as well as all other fittings such as catenary curtains, vent ports etc. are added.
All the strips and subsections as well as the completed segments are joined together by a heat seaming process that involves the overlay of reinforcements on the joint and heating under pressure to fuse the resin. To aid in the movement and transfer of subsegments and subsections of the gas bag, the floor incorporates air cushion systems (not shown) such disclosed in U.S. Patent No. 2,918,183 ".Air Cushion Cargo Handling System" by T. K. Peterson, et al. U.S. Patent No. Pneumatic Conveyor" by D. H. Dennis Of course, there are numerous other systems that can be used. While the segment 60A is being completed, a second segment is being assembled in the vacated space. In large vehicles, the segments 60A can range up to 700 to 800 feet in length and 60 to 100 feet in width. Thus it is readily apparent that the assembly of these segments would normally require an extremely large building. However, by use of the subject crane assembly, the size of the gas bag assembly building can be kept to a reasonable size.
Referring to Figures 3 and 4, the crane rail assembly, for example rail assembly 30, includes dual rails 70A and 70B in a spaced relationship supported by a central frame 71 , having upper tracks 72A and 72B and lower tracks 74A and 74B. A rack gear 76 is located on the bottom of the frame 71. The crane carriage assembly, for example carriage assembly 40A on rail assembly 30, includes carriage frame 80 having twin support members 81 A and 81 B. The member 81 A supports upper wheels 82A and 82B which ride on track 72A and lower wheels 83A and 83B that ride on track 74A. The member 81 B supports upper wheels 84A and 84B which ride on track 72B and lower wheels 86A and 86B which ride on track 74B. Thus the carriage assembly 40A is supported on both sides of the rail assembly 30 and fore and aft. A motor 87 is mounted on the frame 80 that drives a pinion gear 88 via a transmission 90 and, thus drives the carriage assembly 40A along the rail assembly 30. A position sensor 92 mounted to the motor 87 provides carriage assembly position indication along the carriage rail assembly 30. A clevis 94 is mounted at the bottom of the frame 80 that supports a winch 96 having a cable 98. A motor 100 drives the wench via a shaft 102 through a transmission 104. A second position sensor 106 mounted on the motor 100 provides an indication of the position of the end of the cable 98.
Still referring to Figure 4 and additionally to Figure 5, electrical power to the carriage assembly 40A is provided by a trolley car type electrical connector 110 which is mounted to the member 81 A and has an electrical contact head 112 that rides in a groove 1 14 and makes contact with conductors 116A and 116B mounted on insulator 117. Not only can power be provided to the motors 87 and 96, but position indication from the position indicators 92 and 106 can be transmitted out. Referring now to Figures 6 and 7, when the first segment 60A is completed, the winch cables 98 of the first row of carriage assemblies 40A through 48A, are extended to a preset length and manually attached to the segment via attachment fittings (not shown) located along its length (shown in dotted lines). The carriage assemblies 40A-48A are then moved to a first position, with a simultaneous adjustment in the length of the cables 98, lifting the segment 60A partially off the floor 22.. After a second segment 60B is completed, it is joined to the segment 60A. The carriage assemblies 40A-48A are moved to a second position raising the first segment 60A completely off the floor 22 The winch cables 98 of the carriage assemblies 40B-48B are then extended and attached to the second segment. 60B and thereafter the carriage assemblies 40A-48A and 40B-48B are moved further along the carriage rails 30-38, with a simultaneous adjustment of the cables 98. As illustrated in Figure 7, segments 60A-C have been completed, with segments 60A and 60B lifted completely of the floor 22 and with segment 60C lifted partially thereof by carriage assemblies 40C-48C. Referring to Figures 8 and 9, the process is continued until all the segments 60A-60I have been completed and joined together end to end and raised off the floor 22. At this point, cables 120 and 122 of floor mounted winches 124 and 126 are coupled to the segments 60A and 60I, respectively. The free ends of the segments 60A and 601 are then pulled down to the center area 128 of the floor 22 by the winches 124 and 126 as the cables 98 of the winches 96 in the carriage assemblies 40A-48A through 40I-48I are readjusted to accommodate the segment movement. Thereafter, the free ends of the segments 60A and 60I are joined together to form the cylindrical portion of the gas bag. Thereafter the completed gas bag can be raised completely off the floor 22 for subsequent manufacturing operations. While the gas bag is far from complete, (at this point, end segments have not been joined), the subject crane assembly has allowed the main section of the gas bag to be easily assembled.
Referring to Figures 10, it can be seen that the motors 87 of crane carriage assemblies 40A-I through 48A-I, as well as the motors 96 used to adjust cable 98 length, can be easily controlled by means of a micro- processor 130. The micro-processor 130 need only be preprogrammed with library values 131 shown in Figure 11 , for the their respective positions at the various stages of gas bag assembly and provide control signals via motor controllers 132 and 134 based on inputs from the position sensors 92 and 106. However, more sophisticated control systems may be used.
While the invention has been described with reference to a particular embodiment, it should be understood that the embodiment is merely illustrative as there are numerous variations and modifications which may be made by those skilled in the art. Thus, the invention is to be construed as being limited only by the spirit and scope of the appended claims.
INDUSTRIAL APPLICABILITY
The invention has applicability to the aircraft construction industry.

Claims

1. A crane system for a building for the assembly of a gas bag for a lighter-than-air vehicle, the building having a floor and a roof thereover with a longitudinal, vertical and lateral axis, the crane assembly comprising: a plurality of crane carriage rail assemblies in the form of arches aligned with the lateral axis of and mounted within the building, said carriage rail assemblies in a spaced relationship along the longitudinal axis; a plurality of crane carriages movably mounted on each of said crane rail assemblies; a winch mounted on each crane carriage, having an extendible and retractable cable; and a control system for moving said crane carriages by rows aligned with the longitudinal axis of the building along said crane carriage rail assemblies to specific locations along the lateral axis and for adjusting the length of said cables of said winches in each of said rows as a function of the distance of each of said rows along the lateral axis of the building.
2. The crane system as set forth in Claim 1 wherein said control system further simultaneously adjusts the length of said cables of said winches as said rows of said crane carriages are moved along said crane rail assemblies.
3. The crane system as set forth in Claim 2 comprising: each of said crane carriage rail assemblies having a rack gear; and each of said crane carriage assemblies including: a motor mounted on said crane assembly, said motor having a pinion gear engaged with said rack gear; and position indication means for determining the position of said crane assembly along said crane rail assembly.
4. The crane system as set forth in Claim 3 comprising: a motor coupled to each of said winches for driving same: and position indication means coupled to each of said winches for determining the position of the end of said cable.
5. The crane assembly as set forth in Claim 4 wherein said control system is a computer.
PCT/US1995/009243 1994-12-12 1995-07-21 A crane assembly WO1996018565A1 (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
KR1019970700407A KR100196982B1 (en) 1994-12-12 1995-07-21 A crane assembly
NZ290615A NZ290615A (en) 1994-12-12 1995-07-21 Crane system for a building for assembling lighter than air vehicles with winches moved on lateral crane rails but being aligned longitudinally
BR9508476A BR9508476A (en) 1994-12-12 1995-07-21 Crane system for a construction for the assembly of a gas chamber for a vehicle lighter than air
MX9606561A MX9606561A (en) 1994-12-12 1995-07-21 A crane assembly.
AU31404/95A AU685313B2 (en) 1994-12-12 1995-07-21 A crane assembly
EP95927350A EP0797537B1 (en) 1994-12-12 1995-07-21 A crane assembly
RU97111797A RU2136576C1 (en) 1994-12-12 1995-07-21 Crane system
JP51351896A JP3242113B2 (en) 1994-12-12 1995-07-21 Crane assembly
DE69519308T DE69519308T2 (en) 1994-12-12 1995-07-21 CRANE EQUIPMENT

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/354,575 US5495956A (en) 1994-12-12 1994-12-12 Crane assembly
US354,575 1994-12-12

Publications (1)

Publication Number Publication Date
WO1996018565A1 true WO1996018565A1 (en) 1996-06-20

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PCT/US1995/009243 WO1996018565A1 (en) 1994-12-12 1995-07-21 A crane assembly

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US (1) US5495956A (en)
EP (1) EP0797537B1 (en)
JP (1) JP3242113B2 (en)
CN (1) CN1047999C (en)
AU (1) AU685313B2 (en)
BR (1) BR9508476A (en)
CA (1) CA2190133C (en)
DE (1) DE69519308T2 (en)
IL (1) IL114132A (en)
MX (1) MX9606561A (en)
NZ (1) NZ290615A (en)
RU (1) RU2136576C1 (en)
TW (1) TW264442B (en)
WO (1) WO1996018565A1 (en)

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CN100460305C (en) * 2003-08-27 2009-02-11 上海振华港口机械(集团)股份有限公司 Roil type bitrolley gantry container hoister
CN108683083B (en) * 2018-05-16 2020-12-01 许继集团有限公司 Prefabricated cabin roof and prefabricated cabin
US11767680B2 (en) * 2021-02-23 2023-09-26 Ericus Andreas van Kleef Deployable manufacturing production facility and method

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US3863771A (en) * 1972-12-08 1975-02-04 Charles Herbert Dobbie Gantry cranes
US4641757A (en) * 1983-05-06 1987-02-10 Robotic Systems, Inc. Circulating latch transport mechanism for overhead cranes
US5061148A (en) * 1990-03-23 1991-10-29 California Ammonia Co. Polar crane material handling apparatus

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GB1093288A (en) * 1964-06-20 1967-11-29 Bergbaustahl Gmbh & Co Overhead cranes
US3863771A (en) * 1972-12-08 1975-02-04 Charles Herbert Dobbie Gantry cranes
US4641757A (en) * 1983-05-06 1987-02-10 Robotic Systems, Inc. Circulating latch transport mechanism for overhead cranes
US5061148A (en) * 1990-03-23 1991-10-29 California Ammonia Co. Polar crane material handling apparatus

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See also references of EP0797537A4 *

Also Published As

Publication number Publication date
IL114132A0 (en) 1995-10-31
BR9508476A (en) 1997-12-23
CA2190133C (en) 1999-01-19
IL114132A (en) 1998-07-15
EP0797537B1 (en) 2000-11-02
EP0797537A4 (en) 1998-06-10
RU2136576C1 (en) 1999-09-10
AU3140495A (en) 1996-07-03
US5495956A (en) 1996-03-05
MX9606561A (en) 1997-03-29
JPH10509680A (en) 1998-09-22
NZ290615A (en) 1998-08-26
DE69519308T2 (en) 2001-03-01
JP3242113B2 (en) 2001-12-25
CA2190133A1 (en) 1996-06-20
EP0797537A1 (en) 1997-10-01
TW264442B (en) 1995-12-01
AU685313B2 (en) 1998-01-15
CN1047999C (en) 2000-01-05
CN1157604A (en) 1997-08-20
DE69519308D1 (en) 2000-12-07

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