GB2074981A - Telescopic variable length device - Google Patents

Telescopic variable length device Download PDF

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Publication number
GB2074981A
GB2074981A GB8110762A GB8110762A GB2074981A GB 2074981 A GB2074981 A GB 2074981A GB 8110762 A GB8110762 A GB 8110762A GB 8110762 A GB8110762 A GB 8110762A GB 2074981 A GB2074981 A GB 2074981A
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GB
United Kingdom
Prior art keywords
variable length
flexible element
length device
tubular
telescopic variable
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
GB8110762A
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GB2074981B (en
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BAE Systems PLC
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British Aerospace PLC
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Filing date
Publication date
Application filed by British Aerospace PLC filed Critical British Aerospace PLC
Priority to GB8110762A priority Critical patent/GB2074981B/en
Publication of GB2074981A publication Critical patent/GB2074981A/en
Application granted granted Critical
Publication of GB2074981B publication Critical patent/GB2074981B/en
Expired legal-status Critical Current

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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles

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  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)

Abstract

A telescopic boom especially for deploying a solar array on a spacecraft comprises a flexible member extending in the longitudinal direction of the boom and movable in that direction to pick up and extend tubular boom sections 3, 2 one after another in sequence. As shown the member may be an endless sprocket chain 23 driven by an electric motor and entrained around a wheel 14 mounted at the forward end of a pillar 9 which extends inside the boom to a position near the outer end of the unextended boom, the chain having regularly spaced increased thickness link-plates for engaging matching abutment surfaces 46 of the tubular sections 3, 2 to extend them. As the section 3 comes to its fully extended position, it shifts the next section 2 to a position in which it too will be engaged by the increased thickness link plates of the chain 23 so as to be extended in turn thereby. <IMAGE>

Description

SPECIFICATION Telescopic variable length device This invention relates to a telescopic variablelength device comprising a plurality of tubular sections nested one within another. By way of example, the device may be a carrier boom for deploying apparatus such as a solar cell array in a spacecraft.
It is known to extend such a carrier boom by admitting compressed gas to the interior of the boom so as to push the sections out one from within another. Also it has been proposed in patent specification No. 1512912 to provide, within such a boom, a rotatable partly screwthreaded rod upon which there are engaged a plurality of nuts secured to respective ones of the tubular sections. In the stowed position of the boom, only the first nut secured to the innermost tubular section is engaged with the threaded part so that the rod can rotate freely within them. As the rod is rotated, the first nut is screwed along it so that the innermost tubular section moves to its extended position.Shortly before it reaches this position it becomes so engaged with the next larger section that this next larger section is carried along with it and the nut secured thereto becomes engaged with the threaded part of the rod. Thereupon, this next larger section is moved to its extended position and so on.
According to the present invention, there is provided a telescopic variable length device comprising a plurality of tubular sections and a mechanism including an elongate flexible member, for example, a sprocket chain, which extends in the longitudinal direction of the boom and is movable in the direction of its length, and which is operable while being so moved for engaging the tubular sections one after another in sequence to move them along with it.
For a better understanding of the invention reference will now be made, by way of example, to the accompanying drawings in which: figure 1 is a plan view of a telescopic boom, which view, below and to the right of the line AA, is sectioned on the line BB of figure 2, figure 2 is a partly sectioned elevation of part of the boom of figure 1, and figure 3 is a side view of part of a sprocket chain, figure 4 is a view on the line CC in figure 3, and figure 5 is a view on the line DD in figure 2.
The telescopic boom comprises a plurality of tubular sections which are nested one within another when the boom is retracted or "stowed" and of which, for clarity, only the outermost one, 1, and the innermost two, 2 and 3, are shown in figures 1 and 2. Each tubular section comprises a light metal tube to the forward end of which, "forward" here referring to the direction in which the sections move while being extended, i.e. the right-hand side in figure 1, there is attached a forward end flange 4. Each flange 4 is made up of a shallow cup-shaped ring 5 and an annulus 6 which fits into the ring 5. The forward end of each tube is flared slightly and this flared end is clamped between the ring 5 and annulus 6 which are secured together by screws (not shown).The rear end of the outermost tubular section 1 is fixed into a flanged collar 7 which is attached, for example by screws (not shown) to one wall of a girder-shaped mounting member 8. The mounting member is in turn mounted in or upon a spacecraft (not shown). Affixed to the same wall of the member 8 so that it extends into and along the axis of the tubular sections of the boom, there is a pillar 9 which may be made up of a plurality of screwed together sections as shown so as to ease manufacture and enable the length of the pillar to be adjusted but which could also be made in one piece. Also, the pillar could be hollow to save weight. The forward end of the pillar comes to a rounded point 10 which is able to engage within a boss 11 affixed to the annulus 6 of the innermost tubular section.The boss 11 has a low friction plastics material insert 12 fitted therein to receive and guide the end of the pillar. A short distance behind its forward end, the pillar 9 is formed with a slot 1 3 wherein there is rotatably mounted a sprocket wheel 1 4. Near the rear end of the pillar there is a further slot 1 5 which extends back and merges with a hole 1 6 formed in the relatively wider diameter base part 1 7 of the pillar. Attached by screws 18 to the base wall 19 of the mounting member 8 there is an electric motor/gearbox unit to the output shaft of which is coupled a large sprocket wheel 20 so that it is in alignment with the sprocket wheel 14 near the forward end of the pillar 9.Within the slot 15 there are two further sprocket wheels 21 and 22 these being mounted one (22) behind the other (21) in the lengthwise direction of the pillar and such that one side of each just emerges from the slot 1 5. A continuous sprocket chain loop 23 is entrained around the sprocket wheel 14 and, from there, extends back along opposite sides of the pillar 9. On that side of the pillar, at which the slot 1 5 opens, i.e. the lower side in figure 1, the chain is entrained around the outer side of the sprocket 21 and then around the inner side of sprocket 22. On both sides, the chain then extends back through the hole 1 6 and then via a series of tensioning sprocket wheels to the large wheel 20.For clarity, in figures 1 and 2, all the sprocket wheels are shown diagrammatically as smooth discs while the sprocket chain is drawn as a single line. The actual shape of the chain and wheels may be inferred from figure 3 which will be referred to later.
As shown in figures 1 and 2, the aforementioned series of tensioning sprocket wheels consists of three such wheels 24, 25 and 26 for each side of the loop 23. The three wheels are positioned one behind the other having regard to the longitudinal direction of the boom and the outer two 24 and 26 in each case are mounted for rotation about respective fixed axes on a plate 27 which is supported above the wall 1 9 of the mounting member 8 upon columns 28 of the length such as to bring the sprocket wheels 24 and 26 into correct alignment with the wheels 14, 20,21 and 22.Each side of the chain passes around the inner side, i.e. the side nearest the longitudinal axis of the boom, of the respective foremost tensioning wheel 24, then around the outer side of the respective central tensioning wheel 25 and then around the inner side of the respective rear tensioning wheel 26 before extending on to the sprocket wheel 20. Each wheel 25 is mounted at one corner of a respective triangular plate 29. The plates 29 are mounted for pivoting movement about a common axis on the plate 27 so as to form a caliper with a tension spring 30 extending between the plates 29 which spring acts so as to bias those corners of the plates 29 at which the respective sprockets 25 are mounted, and hence the sprockets 25 themselves, outwards away from each other and hence to tension the sprocket chain 23.
Each tubular section of the boom, apart from the outermost one 1, is provided with an inwardly extending flange 32 at its rear end, the flanges being such that all of them have the same inner diameter. Around the outside of the rear end of each of the tubular sections apart from the outermost one are arranged a plurality of bearing pads 33 which slidably engage the inner surface of the next larger tubular section in each case.
Spaced forwardly from the pads 33, but still in the rear regions of the tubular sections, each of the inner sections is fitted with a sleeve 34 which has two forwardly extending lugs (not visible in the figures). The flanges 4 of each tubular section, apart from the innermost one, contain inwardly biassed spring latches 35 which, while the boom is stowed, engage in respective apertures formed in the next smaller tubular section in each case so as to lock the entire boom in the stowed position.
When the boom is to be extended, the latches holding the innermost section 3 may be disengaged by any suitable means (not shown).
Alternatively, the innermost section can be without the apertures in which the latches of the next iarger section engage and can instead be held stowed by some other controllable means which is then released. Then, in the manner described later with reference to figure 3, the inner section is moved to its extended position. When the inner section 3 reaches its extended position, the spring latches mounted within the flange of the next larger section 2 become engaged in apertures in the lugs of the sleeve 34 of the innermost section 3 which thereby becomes interlocked with the section 2. At the same time, the sleeve 34 of section 3 engages the spring latches which are mounted in the flange of the tubular section which is next larger than the section 2 and which were previously holding the section 2 in its stowed position.As a result, the section is able to move to its extended position, become interlocked with the next larger section and, at the same time, release that next larger section for movement to its extended position. This sequence continues until the boom is fully deployed. The operation of the latches and the construction of the sleeves 34 and such are described more fully in our patent application No. 8006751 to which attention is directed.
The sprocket chain 23 has the usual series of links each comprising a pair of side-by-side figure eight-shaped plates and connected to each adjacent link by way of a respective hinge pin and a pair of side-plates which are also figure eightshaped. At spaced intervals, however, the normal side-plates are replaced by modified ones 40 which are somewhat thicker, as shown in figures 3 and 4, the corresponding hinge pins 41 being of extended length. Each modified side-plate has a generally triangular extension portion 42 which carries an outwardly extending guide pin 43.
As shown in figure 5, the central portion of the pillar, i.e. between the slot 1 5 and the pillar part which carries the wheel 14, is circular in crosssection but with two flat-bottomed recesses 31 on opposite sides of the pillar and extending along its length. As mentioned earlier, the pillar may be hollow and it is shown like this in figure 5. At the sides of at least that one of the recesses which is at the lower side of the pillar in figure 1, there are fitted respective guide strips 44 which have portions 45 overhanging the floor of the recess to retain the guide pins 43 and hence to guide the sprocket chain and retain it close to the pillar 9.
The guide strips 44 could be discarded if the recesses 31 are machined so as to form the overhanging portions 45 integral with the recess walls.
Each of the inwardly extending flanges 32 at the rear of the respective tubular section is provided with two radially inwardly extending projections 46 which as seen best in figure 5, lie adjacent respective sides of the sprocket chain (beneath the pillar 9 in figure 1). They are sufficiently spaced from the chain to enable the normal links and side plates to pass between them but the thicker side plates 40 are able to engage them so as to move them and the tubular section to which they are attached along to the extended position.
As seen best in figure 1, the sprocket chain is so guided by the wheels 21 and 22 that initially only the projections 46 of the innermost tubular section 3 are positioned so as to be come engaged by the chain. Thus, when the boom is to be extended, the electric motor is operated so as to move the lower side of the chain loop forwardly in the direction towards the right-hand side of figure 1. Then the first link having the modified side plates 40 to reach the projections 46 of the tubular section 3 engages these projections and moves this section to its extended position. Just before this link reaches the sprocket wheel 14, the section 3 becomes interlocked with the next larger section 2 as described earlier and, as a result, the section 2 is moved forwardly so that the projections 46 of its flange 32 move into a position where they can be engaged by the nextto-arrive chain-link having the modified sideplates 40. At the same time, the projections 46 of the section 3 reach the wheel 14 and become disengaged from the chain. The chain now moves the section 2 to its extended position and so on until the boom is fully extended. The number and spacing of the links having the modified side plates are made such as to give as smooth a progression of the extension as possible.Ideally, one link will pick-up a particular tubular section just as the next preceding one comes to the position of disengagement, but clearly this is not essential and the number of links may be modified, e.g. to give even spacing thereof.
The inner surface of each flange 32 is provided with a series of bearing pads 47, made of Nylatron (trade name) or P.T.F.E., for example, which extend to a short distance from the surface of the pillar 9 and assist in counteracting tendency of the pillar and the structure as a whole to bend in the face of the various forces to which they are subjected both normally and while the boom is being extended.
It will be realised that the boom could be modified so that the mechanism which extends it can equally well retract it if it should be desired to make a recoverable spacecraft. For this no particular modification of the sprocket chain and such is needed. However, there does have to be provided some means (not shown) for disengaging the spring latches 35 which hold the tubular sections interlocked one with another when the boom is extended. By way of example, a series of cams could be arranged to push the spring latches 35 out of engagement with each section as that section is retracted. Alternatively, the illustrated interlocking system using the spring latches 35 could be replaced by some disengageable interlocking means.

Claims (11)

1. A telescopic variable length device comprising a plurality of tubular sections and a drive mechanism including an elongate flexible element which extends in the longitudinal direction of the device and is movable in the direction of its length, and which is operable while being so moved for engaging the tubular sections one after another in sequence to move them along with it.
2. A telescopic variable length device according to claim 1, wherein the flexible element is constrained to move along an endless path.
3. A telescopic variable length device according to claim 2, wherein the endless path includes a take up region and a set down region adjacent which the flexible element engages and disengages a particular tubular element respectively.
4. A telescopic variable length device according to any of the preceding claims, wherein the flexible element includes engaging means adapted to be co-operable with engaging means associated with the tubular sections.
5. A telescopic variable length device according to claim 4, wherein the engaging means associated with each tubular section comprise an abutment region extending radially inwardly of the tubular section, the abutment surfaces of all the tubular sections being of substantially the same radial extent.
6. A telescopic variable length device according to claim 3, wherein coupling means are provided which couple a given tubular section which is engaged with the flexible element to the successive tubular section as that given tubular section approaches the set-down region so that the successive tubular element is moved by the given member to the take-up region subsequently to be engaged by the flexible element.
7. A telescopic variable length device according to claim 4, wherein the engaging means included on the flexible element comprise an abutment surface projecting from the flexible element.
8. A telescopic variable length device according to claim 4, wherein the flexible element includes a plurality of engaging means spaced along the element.
9. A telescopic variable length device according to any of the preceding claims, wherein the flexible element is supported by rod means extending along the longitudinal axis of the tubular sections, at least some of said tubular sections including bearing means adapted to bear on a part of the rod means.
10. A telescopic variable length device according to any of the preceding claims, wherein the flexible element is in the form of a sprocket chain.
11. A telescopic variable length device substantially as hereinbefore described with reference to, and as illustrated in, any of the accompanying drawings.
GB8110762A 1980-04-11 1981-04-06 Telescopic variable length device Expired GB2074981B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8110762A GB2074981B (en) 1980-04-11 1981-04-06 Telescopic variable length device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8011952 1980-04-11
GB8110762A GB2074981B (en) 1980-04-11 1981-04-06 Telescopic variable length device

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GB2074981A true GB2074981A (en) 1981-11-11
GB2074981B GB2074981B (en) 1984-01-04

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3125603A1 (en) * 1980-07-02 1982-05-13 JLG Industries Inc., 17233 McConnellsburg, Pa. TELESCOPIC BOOM
US4480415A (en) * 1981-06-19 1984-11-06 British Aerospace Public Limited Company Extendable structures
US4524552A (en) * 1981-10-09 1985-06-25 General Dynamics Corporation/Convair Div. Mechanism for deploying a deployable truss beam
DE19641191A1 (en) * 1996-09-24 1998-03-26 Mannesmann Ag Telescopic jib for stationary or mobile cranes
DE19641193A1 (en) * 1996-09-24 1998-03-26 Mannesmann Ag Telescopic jib for stationary or mobile cranes
US6904722B2 (en) * 2001-02-21 2005-06-14 The United States Of America As Represented By The Secretary Of The Navy Elongated truss boom structures for space applications
US7581360B2 (en) * 2000-09-22 2009-09-01 Tower Solutions, Llc Retractable column and method of forming
US8366066B2 (en) 2003-04-17 2013-02-05 Tower Solutions, Llc Extendable/retractable support column
US10030379B2 (en) 2010-10-29 2018-07-24 Tower Solutions, Llc Extendable/retractable support column
US11661761B2 (en) 2018-03-22 2023-05-30 Tower Solutions, Llc Mobile tower for transportation and remote deployment

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3125603A1 (en) * 1980-07-02 1982-05-13 JLG Industries Inc., 17233 McConnellsburg, Pa. TELESCOPIC BOOM
US4480415A (en) * 1981-06-19 1984-11-06 British Aerospace Public Limited Company Extendable structures
US4524552A (en) * 1981-10-09 1985-06-25 General Dynamics Corporation/Convair Div. Mechanism for deploying a deployable truss beam
DE19641191A1 (en) * 1996-09-24 1998-03-26 Mannesmann Ag Telescopic jib for stationary or mobile cranes
DE19641193A1 (en) * 1996-09-24 1998-03-26 Mannesmann Ag Telescopic jib for stationary or mobile cranes
DE19641193C2 (en) * 1996-09-24 2002-04-25 Mannesmann Ag Telescopic boom, especially for stationary or mobile cranes
US8225559B2 (en) 2000-09-22 2012-07-24 Tower Solutions, Llc Retractable column and method of forming
US9546499B2 (en) 2000-09-22 2017-01-17 Tower Solutions, Llc Retractable column and method of forming
US7581360B2 (en) * 2000-09-22 2009-09-01 Tower Solutions, Llc Retractable column and method of forming
US7921611B2 (en) 2000-09-22 2011-04-12 Tower Solutions, Llc Retractable column and method of forming
US10094135B2 (en) 2000-09-22 2018-10-09 Tower Solutions, Llc Retractable column and method of forming
US8720127B2 (en) 2000-09-22 2014-05-13 Tower Solutions, Llc Retractable column and method of forming
US6904722B2 (en) * 2001-02-21 2005-06-14 The United States Of America As Represented By The Secretary Of The Navy Elongated truss boom structures for space applications
US6920722B2 (en) 2001-02-21 2005-07-26 The United States Of America As Represented By The Secretary Of The Navy Elongated truss boom structures for space applications
US8955811B2 (en) 2003-04-17 2015-02-17 Tower Solutions, Llc Extendable/retractable support column
US10012344B2 (en) 2003-04-17 2018-07-03 Tower Solutions, Llc Extendable/retractable support column
US8366066B2 (en) 2003-04-17 2013-02-05 Tower Solutions, Llc Extendable/retractable support column
US10030379B2 (en) 2010-10-29 2018-07-24 Tower Solutions, Llc Extendable/retractable support column
US10604928B2 (en) 2010-10-29 2020-03-31 Tower Solutions, Llc Extendable/retractable support column
US11661761B2 (en) 2018-03-22 2023-05-30 Tower Solutions, Llc Mobile tower for transportation and remote deployment

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Publication number Publication date
GB2074981B (en) 1984-01-04

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PCNP Patent ceased through non-payment of renewal fee