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SE406995B - KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES - Google Patents

KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES

Info

Publication number
SE406995B
SE406995B SE7713018A SE7713018A SE406995B SE 406995 B SE406995 B SE 406995B SE 7713018 A SE7713018 A SE 7713018A SE 7713018 A SE7713018 A SE 7713018A SE 406995 B SE406995 B SE 406995B
Authority
SE
Sweden
Prior art keywords
aircraft
rope
posts
line
ropes
Prior art date
Application number
SE7713018A
Other languages
Swedish (sv)
Inventor
R Granberg
Original Assignee
Skogsflyg Cassel Aero
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 Skogsflyg Cassel Aero filed Critical Skogsflyg Cassel Aero
Priority to SE7713018A priority Critical patent/SE406995B/en
Priority to FI783378A priority patent/FI783378A7/en
Priority to NO783894A priority patent/NO783894L/en
Priority to FR7832654A priority patent/FR2409617A1/en
Priority to CA316,500A priority patent/CA1090322A/en
Publication of SE406995B publication Critical patent/SE406995B/en

Links

Classifications

    • HELECTRICITY
    • H02GENERATION; CONVERSION OR DISTRIBUTION OF ELECTRIC POWER
    • H02GINSTALLATION OF ELECTRIC CABLES OR LINES, OR OF COMBINED OPTICAL AND ELECTRIC CABLES OR LINES
    • H02G1/00Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines
    • H02G1/02Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables
    • H02G1/04Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines for overhead lines or cables for mounting or stretching

Landscapes

  • Electric Cable Installation (AREA)
  • Vehicle Body Suspensions (AREA)
  • Joining Of Building Structures In Genera (AREA)
  • Revetment (AREA)
  • Suspension Of Electric Lines Or Cables (AREA)

Description

1113018-sï 2 sedd och av en luftfarkost, exempelvis en helikopter; upplyftbar bygel för en spolstomme med en på spolstommen upplindad lina, och fig. 4 visar den löstagbara axeln för spolstommen. 1113018-sï 2 seen and by an aircraft, for example a helicopter; lifting bracket for a spool body with a line wound on the spool body, and Fig. 4 shows the detachable shaft for the spool body.

Den lina l, i detta fall en ledningslina, som skall utdragas och upphängas, är upplindad på enflspolstomme 2 av vanligt slag. Före li- nans utdragning monteras spolstommen i en med en lyftögla 3 försedd bygel h genom att en i fig. A visad med en vev 5 försedd axel 6 skjuts genom ej visade hål i bygelns båda nedre ändar samt spolstommens cent- rala genomgående hål,“varefter axelns gängade ena ände 7 skruvas in i ett centralt hål 8 i'en på bygelns utsida anordnad skiva 9 till en skivbroms. Skivan är kopplad till en mot spolstommen verkande med- i bringare 10, så att spolstommen kan vrida skivan 9. ll.är skivbromsens ek. 12 är en elektrisk aemkrefc, sem är kepfiied 1-.111 den hydrauliska skivbromsens bromscylinder 13. Den elektriska domkraften kan fjärr- manövreras viáfett kopplingsdon lh.The line 1, in this case a line, which is to be pulled out and hung, is wound on a coil frame 2 of the usual kind. Before pulling out the line, the spool body is mounted in a bracket h provided with a lifting loop 3 by sliding a shaft 6 provided with a crank 5 shown in Fig. 5 through holes (not shown) in both lower ends of the bracket and the central through hole of the spool body, “ after which the threaded one end 7 of the shaft is screwed into a central hole 8 in the disc 9 arranged on the outside of the yoke for a disc brake. The disc is coupled to a member 10 acting against the spool body, so that the spool body can turn the disc 9. 11 is the disc brake oak. 12 is an electric aemkrefc, which is kep fi ied 1-.111 the hydraulic disc brake brake cylinder 13. The electric jack can be remotely operated by a fat connector lh.

En helikopter 15 eller annan luftfarkost användes enligt uppfinning- en för utdragningen och upphängningsn av linan l. För detta ändamål är helikopyern försedd med en ej visad vinsch, vars lyftlina 16 i än- den har en lyftkrok 17. Man drager ut lyftlinan ett stycke och fäster lyftkroken i bygelns A lyftögla 3. Kopplingsdonet lh anslutes till ett för helikopterns pilot åtkomligt manöverdon i förarplatsen. Led- ningslinans l drages ut ett stycke från spolstommen 2 och dess fria ände fästes markfast på lämpligt sätt.A helicopter 15 or other aircraft is used according to the invention for pulling out and suspending the rope 1. For this purpose, the helicopter is provided with a winch (not shown), the lifting rope 16 of which has a lifting hook 17. The lifting rope is pulled out a bit and attaches the lifting hook in the lifting eye of the jumper A 3. The connector lh is connected to an actuator accessible to the helicopter pilot in the driver's seat. The cable line 1 is pulled out a distance from the spool body 2 and its free end is fixed to the ground in a suitable manner.

Helikoptern får nu stiga och lyfta bygeln med spolstommen samt sak- ta flyga framåt, varvid ledningslinan lindas av från spolstommen. Pi- loten håller härvid emot med lämplig brómsverkan i skivbromsen, så att ledningslinan sträckes med önskad kraft. Han styr helikoptern så, att ledningslinan lägges i den skära 18, som finnes i toppen på de stöd- isolatorer 19, som åro.monterade i de utmed den avsedda sträckningen av ledningslinan rosta stolparna 20. Med hjälp av en på helikopterns 'nos monterad backspegel 21 kan piloten med stor precision placera led- nimgslinan i nämnda skära. Denna manöver underlättas, om stödisolatorn har försetts med ett parsnett uppstående horn 22, som för ledningsli- nan mot skåran 18. Markpersonal kan med signaler dirigera piloten och underlätta nämnda precisionsarbete.' ' På grund av att ledningslinans 1 fria ände har fästs markfast,före~ kokmer knappast någon glidning av ledningslinan l i skåran 18. Pilo- ten flyger nu helikoptern från den ena stolpen till den andra och “hänger upp ledningslinan. Då hela eller nästan hela ledningslinan har '7713018-5 ' avlindats från spolstommen 2, sätter piloten ner helikoptern eller vinschar ner bygeln'h, varefter markpersonal fäster ledningslinans andra ände på lämpligt sätt. Markpersonal kan nu gå upp i stolparna och naja fast ledningslinan vid isolatorerna 19. Skall flera, i regel tre,ledningslinor hängas upp, får piloten göra tre resor längs stolp- raden, varvid det med fastnajningen av ledningslinorna kan anstå,ti1ls alla ledningslinorna ha dragits ut och hängts upp. Endast en äntring av varje stolpe blir härigenom erforderlig trots att exempelvis tre ledníngslinor ha hängtslupp. Z För att inte dragningen från ledningslinan l skall vrida bygelnzh med spolstommen 2 snett, kan bygeln vara styrd av från dess båda ned- re ändar* bakåfiriktade Sfiyrarmar 23, i vars yttre mQt varandra fjädran- de anliggande ändar styrtrissor 24 äro roterbart lagrade och anligga med spårade periferier från var sitt håll mot den från spolstommen ut- löpande ledningslinan l. Styrtrissorna kunna ersättas av släpskor el- ler av ett styröga, genom vilket ledningslinan 1 får löpa.The helicopter must now rise and lift the jumper with the spool body and slowly fly forward, whereby the cable line is unwound from the spool body. In this case, the pilot resists with a suitable braking action in the disc brake, so that the line is stretched with the desired force. He controls the helicopter so that the cable is laid in the cutter 18, which is located at the top of the support insulators 19, which are mounted in the towers 20 along the intended stretch of the cable line, by means of a rear-view mirror mounted on the helicopter's nose 21, the pilot can with great precision place the guide line in said insert. This maneuver is facilitated if the support insulator has been provided with a pair of nets arising 22, which guide the line towards the groove 18. Ground personnel can direct the pilot with signals and facilitate said precision work. ' Due to the fact that the free end of the line 1 has been fixed to the ground, there is hardly any slippage of the line 1 in the groove 18. The pilot now flies the helicopter from one pole to the other and “hangs up the line. When the entire or almost the entire line has been '7713018-5' unwound from the spool body 2, the pilot puts down the helicopter or winches the jumper'h, after which ground personnel attach the other end of the line in a suitable manner. Ground personnel can now go up to the poles and fasten the cable to the insulators 19. If several, usually three, cable lines are to be hung up, the pilot may make three trips along the pole line, whereby with the sewing of the cable lines it may take until all the cable lines have been drawn out and hung up. Only one entry of each post is thereby required, despite the fact that, for example, three cable lines have a hanging slip. Z In order to prevent the pull from the cable line 1 from turning the stirrup with the spool body 2 obliquely, the stirrup can be guided by from its two lower ends * rear fi directed arms 2, in the outer of which resiliently abutting abutment ends guide pulleys 24 are rotatably mounted and abutting with grooved peripheries from each direction towards the guide line 1 extending from the coil body. The guide pulleys can be replaced by trailing shoes or by a guide eye, through which the guide line 1 may run.

Genom att man med hjälp av helikopter kan transportera den tunga spolstommen utmed stolpraden, blir man çberoendefav hur terrängen ser ute, Uppfinningen kan modifieras inom ramen för efterföljande patentkrav._By being able to transport the heavy spool body along the pole row by means of a helicopter, it becomes independent of what the terrain looks like. The invention can be modified within the scope of the following patent claims.

Claims (6)

nu. . mštnsëšlll S" PATENTKRAV.now. . mštnsëšlll S "PATENTKRAV. 1. Sätt för utdragning i terrängen av på spolstommar (2) upplindade (linor (1), särskilt ledningslinor, vilka spolstommar upphänges roter- bart kring en horisontell axel (6) i en bygel (h)_i en farkost, vil- ken framförea längs en rad med stolpar (20) under avlindning av linan _från spolstommen ochfeuccessiv upphängning av linan i hållare (19), exempelvis stödisolatorer, i stolparna, k ä n n e t e clk n a t därav) att bygeln (h) anslnteš till en vinsch eller annan lyftanordning i en luftfarkost (15), Sbm därefter flyges utmed raden av stolpar (ZÖ) på så sätt, au; linan (1) successivt anläggas 1 hanarna (19).Method for pulling out in the terrain of ropes (1) wound on spool bodies (2), in particular conductor ropes, which spool bodies are rotatably suspended about a horizontal axis (6) in a stirrup (h) in a vessel which along a row of posts (20) during unwinding of the line from the bobbin case and overeccessive suspension of the line in holders (19), for example support insulators, in the posts, known as the bracket (h) being connected to a winch or other lifting device in an aircraft (15), Sbm then flown along the row of poles (ZÖ) in this way, au; the line (1) is successively laid in 1 the males (19). 2. Sätt enligt patentkravet 1, k ä n n e t'e c k n a t därav, att luftfarkosten (15) flyges så, att linan (1) ovanifrân ilägges mellan från hâllarna (19) uppstående par av horn (22).2. A method according to claim 1, characterized in that the aircraft (15) is flown so that the rope (1) is inserted from above between pairs of horns (22) arising from the holders (19). 3. Sätt enligt patentkravet l eller 2, k ä n n e t e c k n a t därav, att luftfarkostens (15) pilot kontrollerar utdragningen och upphäng- ningen av linan (1) medelst en i luftfarkosten anordnad backspegel (213. A method according to claim 1 or 2, characterized in that the pilot of the aircraft (15) controls the pull-out and suspension of the rope (1) by means of a rear-view mirror (21) arranged in the aircraft. 4. IL. Sätt enligt något av patentkraven 1 - 3, k ä n n e t e c k n a t därav, att markpersonal medverkar till luftfarkostens (15) dirigering _ genom eignaler till piloten.4. IL. A method according to any one of claims 1 - 3, characterized in that ground personnel participate in the routing of the aircraft (15) through signals to the pilot. 5. Sätt enligt något av patentkraven l - h; k ä n n e t e c k n a t därav, att den utdragna linans (1) slutände fästes, varefter mark- personal äntrar stolparna (20) och najar eller på annat sätt fäster linan (1) i hållarna (19).A method according to any one of claims 1 - h; characterized in that the end of the extended rope (1) is fastened, after which ground personnel enter the posts (20) and fasten or otherwise fasten the rope (1) to the holders (19). 6. Sätt enligt patentkravet 5, k ä n n e t e c k n a t Idärav, att det med en linas (1) fästande i stolparna (20) får anstå, tills samtliga linor ha upphängts i stolparna. S i _ ÅNFURDA PUBLIKATIONER: Sverige 317 731 (HOZG 1/04) \ Storbritannien 1 119 942 (HOZG 1/Ö2), 1 217 843 (HOZG 1/02)6. A method according to claim 5, characterized in that with a rope (1) fastening to the posts (20), it must wait until all the ropes have been suspended in the posts. S i _ ANNOUNCED PUBLICATIONS: Sweden 317 731 (HOZG 1/04) \ Great Britain 1 119 942 (HOZG 1 / Ö2), 1 217 843 (HOZG 1/02)
SE7713018A 1977-11-18 1977-11-18 KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES SE406995B (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
SE7713018A SE406995B (en) 1977-11-18 1977-11-18 KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES
FI783378A FI783378A7 (en) 1977-11-18 1978-11-07 SAETT FOER UTDRAGNING AV LINOR OCH UPPHAENGNING I STOLPAR
NO783894A NO783894L (en) 1977-11-18 1978-11-17 PROCEDURE FOR DRAWING LINES AND SUSPENSION IN POSTS
FR7832654A FR2409617A1 (en) 1977-11-18 1978-11-20 Installation of overhead power cable using aircraft - from which cable spool is rotatably suspended, to pay out cable as aircraft files along line of poles
CA316,500A CA1090322A (en) 1977-11-18 1978-11-20 Method to draw out wires and their hanging up in poles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
SE7713018A SE406995B (en) 1977-11-18 1977-11-18 KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES

Publications (1)

Publication Number Publication Date
SE406995B true SE406995B (en) 1979-03-05

Family

ID=20332904

Family Applications (1)

Application Number Title Priority Date Filing Date
SE7713018A SE406995B (en) 1977-11-18 1977-11-18 KIT FOR EXTRACTION IN THE TERRAIN OF WINDED ROPES ON SPOOL FRAMES

Country Status (5)

Country Link
CA (1) CA1090322A (en)
FI (1) FI783378A7 (en)
FR (1) FR2409617A1 (en)
NO (1) NO783894L (en)
SE (1) SE406995B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4993665A (en) * 1989-02-17 1991-02-19 Fred Sparling Device for attachment to a helicopter
US20240150150A1 (en) * 2022-11-04 2024-05-09 Pacific Gas And Electric Company Helicopter conductor reel payout dolly

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2651930B1 (en) * 1989-09-12 1991-10-25 Cnmh HELIPORTED CABLE ROLLER.
RU2147389C1 (en) * 1999-12-15 2000-04-10 Государственное унитарное предприятие Октябрьская железная дорога Method for laying cable on supports of contact-lines, and of automatic block lines of railways
DE10216059A1 (en) * 2002-04-11 2003-10-23 Norddeutsche Seekabelwerk Gmbh Method and device for laying strand-like winding material
JP5348674B2 (en) * 2009-06-30 2013-11-20 株式会社永木精機 Stringer
CN103594962B (en) * 2013-11-05 2016-02-24 国家电网公司 Transmission line flight wire-binding device
CN103594963B (en) * 2013-11-05 2016-01-13 国家电网公司 Flight stringing pay off rack
US10277023B2 (en) * 2017-07-21 2019-04-30 Discovery International Geophysics Inc. Aerial cable laying device
CN111470056B (en) * 2020-04-14 2021-07-09 国网江苏省电力有限公司扬州供电分公司 An intelligent pulley and its working method
FR3116390B1 (en) * 2020-11-19 2022-09-30 Rte Reseau De Transp Delectricite Cable unwinding pulley and adaptation device for such a pulley
CN113889910B (en) * 2021-11-08 2023-02-24 国网山东省电力公司寿光市供电公司 A rapid obstacle-surpassing wire flying car

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3211394A (en) * 1962-09-26 1965-10-12 Petersen Gerald A Winding device for twisted cable
US3586256A (en) * 1970-01-19 1971-06-22 Bertie William Wellman High-tension-wire-laying device for use with helicopters

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4993665A (en) * 1989-02-17 1991-02-19 Fred Sparling Device for attachment to a helicopter
US20240150150A1 (en) * 2022-11-04 2024-05-09 Pacific Gas And Electric Company Helicopter conductor reel payout dolly

Also Published As

Publication number Publication date
FI783378A7 (en) 1979-05-19
CA1090322A (en) 1980-11-25
FR2409617A1 (en) 1979-06-15
NO783894L (en) 1979-05-21

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