CA1048485A - Portable drilling rig compound - Google Patents

Portable drilling rig compound

Info

Publication number
CA1048485A
CA1048485A CA75232680A CA232680A CA1048485A CA 1048485 A CA1048485 A CA 1048485A CA 75232680 A CA75232680 A CA 75232680A CA 232680 A CA232680 A CA 232680A CA 1048485 A CA1048485 A CA 1048485A
Authority
CA
Canada
Prior art keywords
power
power transfer
compound
drilling rig
shafts
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.)
Expired
Application number
CA75232680A
Other languages
French (fr)
Inventor
Kenneth H. Eddy
Kenneth H. Mcgill
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.)
Dresser Industries Inc
Original Assignee
Dresser Industries 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
Application filed by Dresser Industries Inc filed Critical Dresser Industries Inc
Application granted granted Critical
Publication of CA1048485A publication Critical patent/CA1048485A/en
Expired legal-status Critical Current

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Classifications

    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B19/00Handling rods, casings, tubes or the like outside the borehole, e.g. in the derrick; Apparatus for feeding the rods or cables
    • E21B19/008Winding units, specially adapted for drilling operations
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B66HOISTING; LIFTING; HAULING
    • B66DCAPSTANS; WINCHES; TACKLES, e.g. PULLEY BLOCKS; HOISTS
    • B66D1/00Rope, cable, or chain winding mechanisms; Capstans
    • B66D1/02Driving gear
    • B66D1/14Power transmissions between power sources and drums or barrels
    • B66D1/20Chain, belt, or friction drives, e.g. incorporating sheaves of fixed or variable ratio
    • EFIXED CONSTRUCTIONS
    • E21EARTH OR ROCK DRILLING; MINING
    • E21BEARTH OR ROCK DRILLING; OBTAINING OIL, GAS, WATER, SOLUBLE OR MELTABLE MATERIALS OR A SLURRY OF MINERALS FROM WELLS
    • E21B7/00Special methods or apparatus for drilling
    • E21B7/02Drilling rigs characterised by means for land transport with their own drive, e.g. skid mounting or wheel mounting
    • E21B7/027Drills for drilling shallow holes, e.g. for taking soil samples or for drilling postholes
    • E21B7/028Drills for drilling shallow holes, e.g. for taking soil samples or for drilling postholes the drilling apparatus being detachable from the vehicle, e.g. hand portable drills

Landscapes

  • Engineering & Computer Science (AREA)
  • Geology (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mining & Mineral Resources (AREA)
  • Environmental & Geological Engineering (AREA)
  • Fluid Mechanics (AREA)
  • Physics & Mathematics (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Mechanical Engineering (AREA)
  • Devices For Conveying Motion By Means Of Endless Flexible Members (AREA)
  • Drilling And Exploitation, And Mining Machines And Methods (AREA)
  • Earth Drilling (AREA)

Abstract

PORTABLE DRILLING RIG COMPOUND

Abstract of the Disclosure. A portable drilling rig which may be disassembled into subcomponent packages small enough to be transported to the site by helicopter and quickly reassembled utilizes unique chain drive units, compound arrangement and draw-works assembly.

1a

Description

104~485 Background of the Invention. In the production of hy-drocarbons from underground formatlons located in Alaska, Canada, Peru, Indonesia, and any region where ground transportation is re-stricted or non-existent during all or part of the year, and in drilling for oil from offshore locations, and in remote ~ungle lo-cations, it often becomes necessary to transport by air the mate-rials and equipment needed to drill and explore for the oil.
Due to the cumbersome size and weight of the equipment comprising the average drilling rig, much of the rig must be tedi-ously disassembled piece-by-piece and flown in by large air trans-port. This normally requires disassembly of the heavy chain drive units, the final drive unit, and the drawworks for movement to the drilling site. This requires a timely and expensive reassembly at the site with a complicated realignment of the reassembled machin-ery. It often necessitates disassembly of each of the chain case assemblies which means draining of the oil and extensive protection to prevent contamination of the chains and sprockets with dirt, water, and other debris. Then the chain cases must be reassembled on site, often a task near impossible in subzero blizzard conditions or during heavy storms at sea.
Even though the art has progressed enough to place many individual components each on their own portable skid, these must be moved by ship to offshore locations or by large air transport to northern regions because of their extreme weight.
When weather conditions or lack of roads and airfields prevent the use of ships or airplanes, the driller must resort to helicopter transportation of the rigs which requires that each of the usual skid packages must be broken down even further due to the relatively light carrying capacity of the helicopters available.
This cancels the portability advantage of the normal skid units since reassembly of their components requires almost as much time as that of the older rigs did. ~

The present invention overcomes the limitations of the prior devices by providing a portable drilling rig engine and transmission compound, comprising: a plurality of prime movers arranged in a plurality of sets of sub-stantially parallel units; a skid unit for each of the prime movers, with the skid unit having requisite cooling, fuel, and power transmission means thereon operably con-nectable to said prime mover; the prime movers being dis-connectable from each of the associated skid units to facilitate separate movement thereof by helicopter, and the prime movers and the skid units each being easi.ly discon-nectable, transportable and reconnectable as portable sub-components; a plurality of power transfer systems each being an integral self-contained unit having power input means, power output means, and power transfer means between the input and output means, each of the power transfer systems being easily mountable components positionable between associated skid units and interconnectable for use with at least one of the power transmission means and arranged to receive power from at least one transmission means through the power input means and operable to transmit it ~hrough - the power output means; the plurality of power transfer systems being easily removable from the associated skid units, disconnectable from the drilling rig compound such that the plurality of power transfer systems can be transported as self-contained units by helicopter and easily remounted and reconnected for use; the plurality of power transfer systems being arranged to transfer power from the plurality of prime movers to a single output station for operation of a drilling rig drawworks.

-~ ~ mb/ ~ -. ~.. .

1~48485 BRIEF DESCRIPTION OF THE DRAWINGS
Figure 1 is a plan view of the drilling rig layout;
Figure 2 is a side view of the main drum assembly;
Figure 3 is an end view of the main drum assembly and a portion of the power drive assembly;
Figure 4 is an axial end view of the main brake assembly;
Figure 5 is a front view of the main brake equalizing linkage;
Figure 6 is a cross-sectional view of the main drum brake assembly;
. Figure 7 is a partially cut-away view of the align-ment mechanism on the chain case assemblies.

.... . ... ..... . ... ... . . .. . . .. . . . . .. .
DES~RIPTION OF THE PREFERRED EMBODI~ENTS
- .
The present invention comprises a drilling rig comprised of component packages each of which i6 an integral unit transportable by helicopter to the ~:.
mb/~ - 2a -drilling site and easily reassimilated into a drilling rig of al-most any capacity desirable. The number of prime movers may be in-creased or decreased without difficulty and without changing the portability of the unit.
Figure 1 illustrates the unique structure and layout of the compound 10 and the drawworks and the components making up these assemblies. In the figure, a compound is shown utilizing six internal combustion engines for power, arranged in a unique compact arrangement particularly suited for offshore rigs and mountainous areas or any place where space is at a premium.
In the compound 10, half of the engines (11, 12, and 13) are aligned adjacent to each other and the other half of the engines (14, 15, and 16) lie ad~acent to each other opposite engines 11, 12, and 13. As pictured, the engines will provide rotary power through transmissions attached thereto, with the transmissions lla, 12a, and 13a engaged in forward speeds while the transmissions 14a, 15a and 16a are engaged in reverse. Since all the engines rotate in the same direction initially, by having half of them opposed to the other half, three of the transmissions must run in reverse to ob-tain all final rotation in the same direction.
Engines 11 and 12, working through their transmissions, drive propeller shafts llb and 12b which, acting through disconnect-able couplings llc and 12c, turn sprocket shafts lld and 12d. The sprocket shafts are permanently mounted in bearings 17 which in turn are secured in the side of the chain case 18. The sprocket shafts lld and 12d extend laterally through the chain case 18 through bearings 19 securedly attached in the opposite wall of the chain case. Each of the shafts lld and 12d carry chain drive sprockets 20 and 21 thereon inside the chain case 18. The chain drive sprockets 20 on shaft lld are drivably connected to the sprockets 21 on shaft 12d by roller drive chains 22.

Sprocket shaft lld extends through a bearing 19 and has keyed thereon a multiple V-belt drive pulley or sheaves 23 for driving V-belts to mudpumps elsewhere on the rig (not shown). A
clutch 24 is located at the end of the shaft lld to engage and dis-engage the mudpumps from shaft lld.
Shaft 12d extends through a chain case bearing 19 andcarries at its end a disconnectable coupling 25 also connected to an intermediate propeller shaft 26 which in turn is attached to a disconnectable clutch 27.

The location, assembly and operation of engines 14 and 15, and chain case 28 is an identical mirror image of that of engines 11 and 12 except for the direction of rotation which is reversed in transmissions 14a and 15a to correspond to the rota-tional direction of engines 11 and 12. A similar mudpump drive assembly 29 is also driven from engine 14. Likewise, chain case 28 drives through an intermediate shaft 30 and clutch 31 to work with shaft 26 and drive a sprocket shaft 32 extending through chain case 33 in side-wall bearings 34 similar to bearings 17 and 19.
Thus, it can be seen that, other than the power take-off to the mudpumps through sheaves 23 and 29, the combined power out-put of engines 11, 12, 14, and 15 ends up driving sprocket shaft 32 in chain case 33. This in turn drives a sprocket shaft 35 in chain case 33 which shaft is also driven by engine 13 through transmission 13a and propeller shaft 36. At the opposite end of sprocket shaft 35' which shaft turns in bearings 37 secured in the side of case 33, is connected an intermediate propeller shaft 38 coupled to another sprocket shaft 39 which is held by bearings 40 in an input chain case 41. The power from engines 11 through 15 is coupled through the propeller shaft 42 with the power of engine 16 and transmitted from sprocket shaft 39 via roller chains in the input case 41 to the input drive shaft 43 passing through case 41 in sidewall bear-ings 44.

1C~4848S
The total power flow from all of the prime movers 11-16, except that which is provided through the power take-off to the mudpumps, is routed to the input shaft 43 in chain case 41 from whence it moves through a split transmission into the drum drive 5 case 45 to power the main drum assembly 46.
The split transmission comprises a high speed transmis-sion 47 driven off one end of shaft 43 and a low speed transmission 48 driven off of the opposite end of shaft 43. The two transmis-sions 47 and 48 operating through clutches 49 and 50, respectively, are connected to the drum drive shaft 51 which is connected via rol-ler chains in case 45 to main drive shaft 52, shown in phantom in figure 1.
Main drive shaft 52 is coupled through coupling 53 to auxiliary brake shaft 54 containing auxiliary brake 55. The op-15 posite end of main shaft 52 is coupled via coupling 56 to drumshaft 57. Main shaft 52 is supported in sidewall bearings in case 45 just as is drum drive shaft 51. The high speed transmission 47 also drives through auxiliary shaft 58 a catworks drive assembly 59 having a right angle gear box 60 connected by propeller shaft 61 to 20 the catworks, usually located above the drawworks.
The main drum assembly 46 has a main drawworks drum 62, a drum housing 63, a main drum brake assembly 64, (shown in phantom in figure 1) and may have an optional auxiliary brake assembly 65.
In operation, the prime-mover motive power accumulates in 25 chain case 41 and is routed either through the high speed transmis-sion 47 and clutch 49 or the low speed transmission 48 and clutch 50 to the drum drive case 45. There the power is transferred to main shaft 52 which in turn is connected to auxiliary brake assem-bly 55 and to the drum drive shaft 57 which turns the main draw-30 works drum 62. Rotation of the drum can be controlled by the var-ious clutches in the above described system as well as by the main drum brake 64 and auxiliary brakes 55 and 65.

lOg8485 The catworks is driven through the high speed transmis-sion input shaft 47a in case 47. Figures 2 and 3 illustrate ground level views of the main drum assembly and the catworks drive assem-bly, respectively.
Figure 4 illustrates an axial end view of the main brake assembly 64 inside the drum housing 63 and operating on the main drum shaft 57.
The main brake assembly comprises a central hub 66 on shaft 57 securedly attached thereto, a radial web 67 integrally formed on the outer perimeter of hub 66, and the brake drum 69 attached peripherally to web 67 by means of a radially inward pro-jecting flange 68 connected to web 67 by means of fasteners 70 or by other means such as welding. The brake shoe comprises a plural-ity of arcuate brake pads 71 of suitable material such as asbestos aligned in a double row peripherally around the drum 69 and con-tactable therewith. Arcuate brake bands 72 and 73 pass around each row of the brake pads 71 in order to clamp the pads against the drum when braking is desirable. The pads preferably are bonded or riveted to the inside surface of the brake bands. A suitable link-age 74 is attached to bands 72 and 73 to allow tightening of the bands at the operator's command.
Ad~ustable turnbolts 75, 76, and 77 and links 78 and 79 serve to equalize the amount of braking attained from the two brake pad assemblies. Also, the brake assembly is designed so that with the normal counterclockwise rotation of the drum the brakes are self-energizing, meaning that the brakes utilize the rotation of the drum to add increasing pressure to the brake pads against the drum. This cuts down greatly the amount of force required from the operator working the brake controls.
Rollers 80 and threaded rods 81 attached to the drum housing supply support and alignment to the brake pad assemblies particularly while the brakes are not in use.

1~)4~48~
Disa`sse'mb'ly of the`'Rig. When the drilling rig is to be moved to the drilling site by helicopter, the entire rig is quickly S~,~c~p-~c.,~s broken down into integral ~pon~nb~ each below the maximum weight transportable by helicopter. Reinstalling the rig on site requires i,--~
~no complicated reassembly or adjustment. The rig of this invention S~Cor~ Q~
is designed so that all the e~mF-n~=~~ are placed easily and quickly back into alignment and in operable condition almost ins~antaneously with setting them down on the rig floor.
Referring to figure 7, a detailed close-up of apparatus for alignment of the chain cases is disclosed. As previously des-cribed, each chain case is a separable, integral unit in itself and can be moved by helicopter from one site to another without disturb-ing the alignment of the chains or chain sprockets, without having to drain the lubricant therefrom, and without exposing the workings therein to contaminants or the environment.
Each chain case preferably has a plurality of "ears" 82 extending outward from several locations on the lowermost edges of the case, consisting of flat plates or angle iron.
Likewise, the skid or platform receiving or supporting each chain case has a corresponding "fence" 83 or rail attached thereto sized and located to receive the "ears" of the chain cases.
Each fence may comprise a rectangular or other shaped receptacle having vertically extending sides and enclosing all of the exposed sides of the "ears" on the chain cases. The fences are preferably f the same general shape and slightly larger than the ears of the chain cases. Different chain cases could have different sized or shaped ears with matching fences to differentiate from the other units and insure the same location for each unit respective to the others when moving from one site to the next.
Each chain case generally has two sprocket shafts passing transversely therethrough, generally in parallel alignment, each being journaled in sidewall bearings in each side of the case and 104~4~S
each carrying chain sprockets. A plurality of chains transfer power between the two sprockets carried by the shafts in each case.
The cases themselves are self-contained and fluid tight and the sidewall bearings and sprocket shafts passing therethrough are fluid tight in the case walls.
When the rig is being transported, the lift cable from the helicopter is usually hooked or tied in an eyebolt or similar attachment secured to the top of each case after the couplings or clutches at each end of the sprocket shafts have been disconnected.
Then the case can be lifted straight up and transported to the new site intact, whereupon it is set down in its proper place with the case ears sliding into the guide fences and the unit is ready to go upon reconnection o~ the various propeller shafts to the sprocket shafts. The above operation applies generally to all of the chain cases 18, 28, 33, 41, and 45 as well as to the transmissions 47 and 48.
The individual engines 11-16 are provided with eyebolts or other hook receptacle means and are helicopter transportable in-dependently of their transmissions, radiators, and skids. Each engine is unbolted from the skid and transmission and disconnected from fuel lines and coolant lines and picked up by the helicopter.
The skid, transmission, and fuel and coolant systems for each engine then travel as a single unit by helicopter.
The particular arrangement of engines is unique in that it allows the maximum number of engines with the minimum amount of space and the minimum number of power transferrance units such as chain drives and pully drives. This compact layout allows for greater use of the limited amount of room on offshore rigs and the shortest exposure time to operating and maintenance personnel in northern regions.
In addition to the compact design of the compound further novelty resides in the layout and design of drawworks drive system and of the main drum assembly.

10~4~S
In the drawworks drive system a unique split-transmission arrangement to receive the accumulated prime mover force and trans-mit it to the drawworks utilizes two compact transportable trans-missions as opposed to the old single unit two-speed transmission system. The single unit, two-speed transmission is entirely too heavy and cumbersome to be transported by helicopter, whereas each of the transmissions of this system are compact and light enough to be moved by any means, including helicopter. The split trans-mission includes a high speed unit and a low speed unit, each with its own clutch control into the drum drive case.
A power take-off from the high speed transmission also powers the catworks via a propeller shaft and right angle gear box.
Since the high speed transmission has a clutch between it and the drum drive, the catworks may be driven whether or not the drum drive is being driven by the high speed or the low speed transmission.
The main drum assembly is also novel in that it allows quick, clean dissembly of the brake system from the main drum with-out disturbing the adjustment or assembly of the individual brake parts. The entire braking system is removed from the main drum assembly intact and as a system rather than in pieces.
This is possible because of the design of the main drum which places both brake assemblies at one end of the drum rather than having one brake at each end of the drum as the prior devices have.
Also, the design of the brake system with the brake bands, pads, linkage and brake drum all remaining in one package, complete-ly assembled but separable from the main drawworks drum, means that the brake assembly can be moved by helicopter separate from the main drum and later quickly reunited therewith. This also lightens the main drum to the point that it can be similarly transported.
The auxiliary brakes preferably are both hydraulic retard-ing mechanisms used to partially brake the drum drive. Each is 1~)4t~485 separately helicopter transportable.
Although a specific preferred embodiment of the present invention has been described in the detailed description above, the description is not intended to limit the invention to the par-ticular forms of embodiments disclosed therein since they are tobe recognized as illustrative rather than restrictive and it will be obvious to those skilled in the art that the invention is not so limited. For instance, the prime movers may be of internal com-bustion type as shown or some other type such as electric powered or turbines. Also the number of such engines could be more or less than that shown. Furthermore, in some instances belt drives could be used in place of the chain drives, and vice versa. Also the cat-works could be driven by belt drive or chain drive or could be electrically operated~ rather than gear and propeller shaft driven.
Thus, the invention is declared to cover all changes and modifica-tions of the specific example of the invention herein disclosed for purposes of illustration which do not constitute departures from the spirit and scope of the invention.

Claims (12)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE PROPERTY
OR PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A portable drilling rig engine and transmission compound, comprising:
a plurality of prime movers arranged in a plurality of sets of substantially parallel units;
a skid unit for each of said prime movers, with said skid unit having requisite cooling, fuel, and power transmission means thereon operably connectable to said prime mover;
said prime movers being disconnectable from each of said associated skid units to facilitate separate movement thereof by helicopter, and said prime movers and said skid units each being easily disconnectable, trans-portable and reconnectable as portable subcomponents;
a plurality of power transfer systems each being an integral self-contained unit having power input means, power output means, and power transfer means between said input and output means, each of said power trans-fer systems being easily mountable components position-able between associated skid units and interconnectable for use with at least one of said power transmission means and arranged to receive power from at least one transmission means through said power input means and operable to transmit it through said power output means;
said plurality of power transfer systems being easily removable from the associated skid units, disconnect-able from the drilling rig compound such that said plurality of power transfer systems can be transported as self-contained units by helicopter and easily re-mounted and reconnected for use;
said plurality of power transfer systems being arranged to transfer power from said plurality of prime movers to a single output station for operation of a drilling rig drawworks.
2. The drilling rig compound of claim 1 wherein such includes six skid units and six prime movers, and four power transfer systems.
3. The drilling rig compound of claim 2 wherein said prime movers are internal combustion engines operable in two groups of three engines with the outputs thereof position in an opposed relation and connected by said plurality of power transfer systems.
4. The drilling rig compound of claim 1 wherein such additionally includes a power take-off system from at least one of said power transfer systems to power at least one of auxiliary pump.
5. The drilling rig compound of claim 1 wherein said power transfer systems each include an input shaft and an output shaft in a parallel spaced relation, said shafts passing trans-versely through the walls of a case with said shafts being rotatably and sealingly mounted in said walls, and having said power transfer means operably connected between said shafts.
6. The rig compound of claim 5 wherein said case is com-pletely sealed and fluid tight, and contains lubricant therein;
said input and output shafts each have a plurality of chain sprock-ets attached thereto; and said power transfer means comprises a plurality of closed-loop chains engaging sprockets on both of said shafts.
7. The rig compound of claim 6 wherein each said case further comprises alignment means thereon including at least one laterally projecting ear at the lower edge of said case, and at least one alignment fence matching said alignment ear and adapted to be attached to the skid unit to receive said ear in aligning engagement therein.
8. The rig compound of claim 1 further comprising at least one releasable clutch means coactably engaged between at least two of said power transfer systems.
9. A portable drilling rig compound comprised of discon-nectable subcomponents each transportable by helicopter as an inte-gral self-contained unit, said compound comprising:
six prime movers arranged in two groups, each said prime mover being transportable by helicopter as a self-contained unit;
six portable skid units each adapted to receive and mount one of said prime movers in an easily disconnectable relation, and further each having a power transmission means thereon operably connectable within associated prime mover for transmitting power from said prime mover, said portable skid units each being transportable by helicopter as a self-contained unit; and four power transfer assemblies interconnectable with said six prime mover transmission means and arranged to transfer power from all six prime movers to a final output station, each said power transfer assembly being an integral sealed, self-contained unit easily connect-able to and disconnectable from an associated power transmission means and transportable by helicopter as a self-contained unit.
10. The portable drilling rig compound of claim 9 wherein:
said prime movers comprise internal combustion engines, said two groups are positioned with outputs thereof in an opposed relation with each group containing three engines; and said power transfer assemblies each comprise a fluid tight case having two parallel rotatable shafts passing transversely through the case and sealed therewith, and including a chain and sprocket means within said case and operably connected to said shafts.
11. The portable drilling compound of claim 10 wherein said cases each have alignment means attached to the exterior thereof which are correspondingly engageable with other alignment means on said portable skid units in order to position said power transfer assemblies for operation, and said cases each have an eye means formed on the top thereof for receiving and attaching a transfer cable.
12. The portable drilling rig compound of claim 1 where-in each power transfer system comprises:
a fluid tight, chain case having parallel opposing side walls;
an input shaft passing transversely through said side walls;
bearing means sealingly mounted in said side walls, receiv-ing said input shaft in sealing, rotatable relationship;
an output shaft passing transversely through said side walls generally parallel to said input shaft;

second bearing means sealingly mounted in said side walls, receiving said output shaft in sealing, rotatable re-lationship;

sprocket means on said input and output shafts;
a plurality of looped drive chains coactably engaging sprockets on said input and output shafts; and, easily disconnectable couplings on at least one end of each of said shafts.
CA75232680A 1974-10-02 1975-08-01 Portable drilling rig compound Expired CA1048485A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US51134874A 1974-10-02 1974-10-02

Publications (1)

Publication Number Publication Date
CA1048485A true CA1048485A (en) 1979-02-13

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Family Applications (1)

Application Number Title Priority Date Filing Date
CA75232680A Expired CA1048485A (en) 1974-10-02 1975-08-01 Portable drilling rig compound

Country Status (3)

Country Link
BR (1) BR7506366A (en)
CA (1) CA1048485A (en)
GB (1) GB1522985A (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0448842A1 (en) * 1990-03-26 1991-10-02 Sietse Jelle Koopmans Displaceable, two-part winch device

Also Published As

Publication number Publication date
BR7506366A (en) 1976-08-17
GB1522985A (en) 1978-08-31

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