US106335A - Improvement in sheaves - Google Patents
Improvement in sheaves Download PDFInfo
- Publication number
- US106335A US106335A US106335DA US106335A US 106335 A US106335 A US 106335A US 106335D A US106335D A US 106335DA US 106335 A US106335 A US 106335A
- Authority
- US
- United States
- Prior art keywords
- sheaves
- improvement
- bushing
- heddles
- sheave
- 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 - Lifetime
Links
- 229910001018 Cast iron Inorganic materials 0.000 description 4
- 239000002184 metal Substances 0.000 description 4
- 229910052751 metal Inorganic materials 0.000 description 4
- 230000000875 corresponding Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910000679 solder Inorganic materials 0.000 description 2
- 238000005476 soldering Methods 0.000 description 2
- 229910052718 tin Inorganic materials 0.000 description 2
- 239000005028 tinplate Substances 0.000 description 2
Images
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H55/00—Elements with teeth or friction surfaces for conveying motion; Worms, pulleys or sheaves for gearing mechanisms
- F16H55/32—Friction members
- F16H55/36—Pulleys
- F16H55/44—Sheet-metal pulleys
Definitions
- My invention relates to the method'of constructing the sheaves which are used in mountingheddles in looms, so thatthey may he n'rade. of sufficient strength, and yet much lighter and also cheaper than those in common use.
- the sheaves usually employed in mounting heddles are made of cast-iron, and are, necessarily, when made as light as practicable, of considerable weight; and in mounting a looin with, say, twenty leaves of heddles with six sheaves (three above and three bclow)to each leaf, there would" be required one hundred and twenty sheaves in all, and as 'these have to bepartially, rotated with a reciprocating motion at each movement of the warps, their united inertia and momentum in stopping and starting at each pick, ofl'ers considerable resistance to the easy working of the loom, and consuniesa considerable amount of the power without any corresponding useful result, and especially in operating the loom rapidly.
- Bl1ii by constructing the sheaves of 'tin, or other sheet-metal, in the manner herein described, they can bemade of a better form, and of much less weight and cost, and less liable to be broken,-than when made of cast-iron.
- Figure 2 is a section of the saine,-showing one form of inserting the bushing orhub to receive the hole at the center.
- Figures 3 and 4 are an elevation and section, showing another mode of applying the central bushing 01' hub, so that it maybe removed. 7
- the sheave is formed of two pieces of tin plate, A, which are struckJup to form in a die by the wellknown process of making raised work, which pieces are placed together face to face, and united by a bushing or hub, B, which is insertedin the central hole and secured therein by soldering, as is shown in figs;
- the plates may also be, united by a line of solder at H, around the circumference, if desired.
- F F are holes in the flange 1),'t-0 receive a wrench or spanner to screw it up.
- asheave can be made of a less thickness than in any other practicable way known to me, and yet give a suflicient depth and breadth to the groove G for the cord, without liability of its being broken, which is a matter of great importance in using a large number of heddles, where it is very desirable to make them as thin as possible.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Looms (AREA)
Description
dished grates patent dtjiliire.
Letters Patent N 106,335, dated August 16, 1870.
IMPROVEMENT IN SHEAVES.
The Schedule referred to in these Lettera Patent and making part of the same I, HILAS D. DAVIS, of North Audover, in the county of Essex andState of Massachusetts, have invented an improved Sheave, of which the following is a specification.
Nature and Object of the Invention.
My invention relates to the method'of constructing the sheaves which are used in mountingheddles in looms, so thatthey may he n'rade. of sufficient strength, and yet much lighter and also cheaper than those in common use.
The sheaves usually employed in mounting heddles are made of cast-iron, and are, necessarily, when made as light as practicable, of considerable weight; and in mounting a looin with, say, twenty leaves of heddles with six sheaves (three above and three bclow)to each leaf, there would" be required one hundred and twenty sheaves in all, and as 'these have to bepartially, rotated with a reciprocating motion at each movement of the warps, their united inertia and momentum in stopping and starting at each pick, ofl'ers considerable resistance to the easy working of the loom, and consuniesa considerable amount of the power without any corresponding useful result, and especially in operating the loom rapidly. Bl1ii" by constructing the sheaves of 'tin, or other sheet-metal, in the manner herein described, they can bemade of a better form, and of much less weight and cost, and less liable to be broken,-than when made of cast-iron.
Although this mode of making sheaves was especially designed for mounting heddles, it is equally applicable to any other purpose to which its qualities adapt it.
Description.-
In the drawing- Figure 1 is a side elevation ot'.a sheave, full size; and
Figure 2 is a section of the saine,-showing one form of inserting the bushing orhub to receive the hole at the center.
Figures 3 and 4 are an elevation and section, showing another mode of applying the central bushing 01' hub, so that it maybe removed. 7
The sheave is formed of two pieces of tin plate, A, which are struckJup to form in a die by the wellknown process of making raised work, which pieces are placed together face to face, and united bya bushing or hub, B, which is insertedin the central hole and secured therein by soldering, as is shown in figs;
1 and 2, or by flanges upon the bushing, as is shown in figs. 3 and 4, the flangeG being formed upon the bushing, and the flange I) screwed upon the same, so as to clamp the plates between them. I
In this last case, the plates would not bebent out at a right angleat the central hole, as is shown at E, fig. 2.
The plates may also be, united by a line of solder at H, around the circumference, if desired.
F F are holes in the flange 1),'t-0 receive a wrench or spanner to screw it up.
By this means asheave can be made of a less thickness than in any other practicable way known to me, and yet give a suflicient depth and breadth to the groove G for the cord, without liability of its being broken, which is a matter of great importance in using a large number of heddles, where it is very desirable to make them as thin as possible.
\Vhat I claim as my invention, is-
A sheave formed of two thin plates of metal, enibossed to form, and placed together face to face, and combined with a central bushing or hub, substantially as described.
Executed March 23, 1870. v
HILAS I). DAVIS.
Witnesses G. E. WHITNEY, WM. 0. HIBBARD.
Publications (1)
Publication Number | Publication Date |
---|---|
US106335A true US106335A (en) | 1870-08-16 |
Family
ID=2175811
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US106335D Expired - Lifetime US106335A (en) | Improvement in sheaves |
Country Status (1)
Country | Link |
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US (1) | US106335A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2639119A (en) * | 1947-11-14 | 1953-05-19 | Lockheed Aircraft Corp | Rotor blade attachment means and method |
-
0
- US US106335D patent/US106335A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2639119A (en) * | 1947-11-14 | 1953-05-19 | Lockheed Aircraft Corp | Rotor blade attachment means and method |
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