US444077A - Piston-travel indicator - Google Patents
Piston-travel indicator Download PDFInfo
- Publication number
- US444077A US444077A US444077DA US444077A US 444077 A US444077 A US 444077A US 444077D A US444077D A US 444077DA US 444077 A US444077 A US 444077A
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- US
- United States
- Prior art keywords
- piston
- bar
- travel
- cylinder
- barrel
- 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
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- 238000010276 construction Methods 0.000 description 4
- 230000003247 decreasing Effects 0.000 description 4
- CVRALZAYCYJELZ-UHFFFAOYSA-N (±)-Leptophos Chemical compound C=1C=CC=CC=1P(=S)(OC)OC1=CC(Cl)=C(Br)C=C1Cl CVRALZAYCYJELZ-UHFFFAOYSA-N 0.000 description 2
- 101700078529 ADRB1 Proteins 0.000 description 2
- 241000229754 Iva xanthiifolia Species 0.000 description 2
- 230000004075 alteration Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 230000036633 rest Effects 0.000 description 2
Images
Classifications
-
- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63C—SKATES; SKIS; ROLLER SKATES; DESIGN OR LAYOUT OF COURTS, RINKS OR THE LIKE
- A63C9/00—Ski bindings
- A63C9/005—Ski bindings with means for adjusting the position of a shoe holder or of the complete binding relative to the ski
-
- G—PHYSICS
- G08—SIGNALLING
- G08B—SIGNALLING OR CALLING SYSTEMS; ORDER TELEGRAPHS; ALARM SYSTEMS
- G08B5/00—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied
- G08B5/02—Visible signalling systems, e.g. personal calling systems, remote indication of seats occupied using only mechanical transmission
Definitions
- Figure l is a vertical central section of an air-brake cylinder with our improvement attached thereto;
- Fig. 2 a side elevation, partly in section, of the indicating device;
- Fig. 3 a plan View of the same, also partly in section;
- Fig. 4 a section online y-LL fl of Fig. 3, looking in the direction of the arrows.
- the last three figures are on an enlarged scale.
- A is the air-brake cylinder; B, the piston; IJ, the piston-rod; C, a barrel or stuffing-box attached to the cylinder; D, a graduated bar sliding in such barrel; d d, lugs on such bar, and E a spring bearing against the bar D.
- the cylinder to which our device is attached is constructed in the usual way, as are also the piston, piston-rod, &c., and being well known require no further description.
- the barrel or stuffing-box C is made of any suitable material and screwed into the rearward cylinder-head, projecting outward, as shown in Fig. l, and serves as a guide and snpport for the bar D. IVe then make the bar D.
- This bar is made preferably of metal and slides back and forth in the barrel C. To keepit from being drawn or forced entirely out of the barrel, we prefer to provide it with lugs d d, as shown, which strike against the inner end of the barrel.
- the barD is graduated along one or both sides. In the drawings an inch scale is represented; but any other may be used as desired.
- a spring E is placed in the barrel, which preferably has a recess e to receive it. This spring bears against the bar D, and is intended to insure the steady motion of the bar to prevent its being thrown forward farther than the piston travels and to hold the bar in the place to which it moved, so as to preserve the record made.
- a piston-travel indicator comprising a barrel or stufiing-boX attached to the end of the cylinder, a bar sliding iu such barrel and entering the cylinder, and means for retaining such bar in the position to which it is IOO moved bcv the travel ol the piston, substanl i. lIn a pislon'travcl indicator, abar entertially as described. ing the cylinder and adapted to be pushed 2.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Actuator (AREA)
Description
(Nor/mel.) l
E B. THOMPSON 85 A. SHROYER. PISTON TRAVEL INDICATOR.
No. 444,077. Patented Jan. 6, 1891.
UNITED STATES PATENT CFFICE.
EDGAR BTI-IOMPSO AND CHARLES A. SCHROYER, OF CHICAGC, ILLINOIS.
PlSTON-TRAVEL INDICATOR.
SPECIFICATION forming part of Letters Patent No. 444,677, dated January 6, 1891.
Application iled November 21, 1889. Serial No. 331.086. (No model.)
To @ZZ whom, it may concern:
Be it known that We, EDGAR B. THOMPSON and CHARLEs A. ScHRoYER, citizens of the United States, residing at Chicago, Cook county, Iliinois, have invented a new and useful Improvement in Piston-Travel Indicators, of which the following is a specification.
For brevity and convenience we shall describe our device as applied to an air-brake cylinder, althou gh it is obvious that it is capable of being used to indicate the travel of any piston,the necessary alterations as to dimensions, &c., being made. It is a well-known fact that if the travel of the piston in the airbrake cylinder is too short the air-pressure will be increased and the dangerof skidding7 the wheels or wearing them unevenly will be increased correspondingly. On the other hand, if the piston-travel be too great the pressure will be decreased, thereby decreasing the efiiciency of the braking service. To get at the amount of this travel it has heretofore been customary to make an application of the brakes and then measure the travel with a rule-a very laborious and troublesome method.A
It is our object to provide a simple and effective apparatus for obtaining the indication desired, which is operated by the movement of the piston; and our invention consists in the features and details of construction hereinafter described and claimed.
In the drawings, Figure l is a vertical central section of an air-brake cylinder with our improvement attached thereto; Fig. 2, a side elevation, partly in section, of the indicating device; Fig. 3, a plan View of the same, also partly in section; and Fig. 4, a section online y-LL fl of Fig. 3, looking in the direction of the arrows. The last three figures are on an enlarged scale.
A is the air-brake cylinder; B, the piston; IJ, the piston-rod; C, a barrel or stuffing-box attached to the cylinder; D, a graduated bar sliding in such barrel; d d, lugs on such bar, and E a spring bearing against the bar D.
The cylinder to which our device is attached is constructed in the usual way, as are also the piston, piston-rod, &c., and being well known require no further description.
The barrel or stuffing-box C is made of any suitable material and screwed into the rearward cylinder-head, projecting outward, as shown in Fig. l, and serves as a guide and snpport for the bar D. IVe then make the bar D.
This bar is made preferably of metal and slides back and forth in the barrel C. To keepit from being drawn or forced entirely out of the barrel, we prefer to provide it with lugs d d, as shown, which strike against the inner end of the barrel. The barD is graduated along one or both sides. In the drawings an inch scale is represented; but any other may be used as desired. A spring E is placed in the barrel, which preferably has a recess e to receive it. This spring bears against the bar D, and is intended to insure the steady motion of the bar to prevent its being thrown forward farther than the piston travels and to hold the bar in the place to which it moved, so as to preserve the record made.
The operation is as follows: Then the piston is in the position shown in Fig. l, the graduated bar should be pushed inward until its end rests against the piston. When the brakes are applied, the pistou will be driven toward the right, Fig. l, carrying the bar along. The lat-ter will be brought into the position shown by dotted lines in Fig. 1, and will indicate the travel of the piston, the distance the bar is forced out of the barrel being equal to the distance traveled by the piston. As above stated, the springE holds the bar so firmly that it can only move through the application of positive force. It will move only while pushed by the piston and will travel no farther than the latter. lVhen the piston returns to its original position, Fig. 1, the spring will hold the bar in the position indicated by dotted lines until again pushed back against the piston.
XVhile we have shown and prefera flattened bar, it willbe obvious that a differently-shaped one may be used with equal advantage, and that similar changesin form and construction may be made without departing from the spirit of our invention.
l. A piston-travel indicator comprising a barrel or stufiing-boX attached to the end of the cylinder, a bar sliding iu such barrel and entering the cylinder, and means for retaining such bar in the position to which it is IOO moved bcv the travel ol the piston, substanl i. lIn a pislon'travcl indicator, abar entertially as described. ing the cylinder and adapted to be pushed 2. The combination ol a cylinder, a piston, i out therefrom bythe movement o l` the piston i5 a `barrel attached to the head of the cylinder, and remaining in the position into which it 5 and a graduated bar passing through the bar- 1 is brought, whereby the travel of thc piston rel into the cylinder and adapted to be forced l is indicated, substantially as described. out ot the cyhndei by the movement of thc EDGAR n THOMPSON piston whereby the travel of Snell piston is Y, 1 l f indicated, substantially as described. UIARMLS A' SCURO) ER' 1o 3. The combination of the cylinder A, pisl Witnesses:
t0n B, barrel c, ,graduated bar D, having lugs l GEORGE S. PAYSON, d d, and spring E, substantially as described.
SAMUEL E. HIBBEN.
Publications (1)
Publication Number | Publication Date |
---|---|
US444077A true US444077A (en) | 1891-01-06 |
Family
ID=2512971
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US444077D Expired - Lifetime US444077A (en) | Piston-travel indicator |
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US (1) | US444077A (en) |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2718868A (en) * | 1951-12-29 | 1955-09-27 | Chicago Pneumatic Tool Co | Stroke indicating mechanism for riveting machines |
US3997887A (en) * | 1975-06-27 | 1976-12-14 | Midland-Ross Corporation | Piston overtravel indicator |
US4550675A (en) * | 1983-03-31 | 1985-11-05 | Chrysler Corporation | Self-adjusting shift indicator for automatic transmission |
US6073979A (en) * | 1997-10-28 | 2000-06-13 | Rotex, Inc. | Adjustable clamp and force level indicator for screening machine cover |
US20040205977A1 (en) * | 2003-04-18 | 2004-10-21 | Halliar William R | Apparatus for measuring piston travel |
US20070034420A1 (en) * | 2003-03-28 | 2007-02-15 | Stanford Frantz D | Mechanical lift measurement system |
US20130272851A1 (en) * | 2012-04-12 | 2013-10-17 | General Electric Company | Turbine shell displacement monitoring system |
US20170008645A1 (en) * | 2015-07-06 | 2017-01-12 | The Boeing Company | Body Fuel Tank Critical Gap Measurement and Validation Template |
-
0
- US US444077D patent/US444077A/en not_active Expired - Lifetime
Cited By (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2718868A (en) * | 1951-12-29 | 1955-09-27 | Chicago Pneumatic Tool Co | Stroke indicating mechanism for riveting machines |
US3997887A (en) * | 1975-06-27 | 1976-12-14 | Midland-Ross Corporation | Piston overtravel indicator |
US4550675A (en) * | 1983-03-31 | 1985-11-05 | Chrysler Corporation | Self-adjusting shift indicator for automatic transmission |
US6073979A (en) * | 1997-10-28 | 2000-06-13 | Rotex, Inc. | Adjustable clamp and force level indicator for screening machine cover |
US20070034420A1 (en) * | 2003-03-28 | 2007-02-15 | Stanford Frantz D | Mechanical lift measurement system |
US7544902B2 (en) * | 2003-03-28 | 2009-06-09 | Actuant Corporation | Mechanical lift measurement system |
US20040205977A1 (en) * | 2003-04-18 | 2004-10-21 | Halliar William R | Apparatus for measuring piston travel |
US6904698B2 (en) * | 2003-04-18 | 2005-06-14 | Ttx Company | Apparatus for measuring piston travel |
US20130272851A1 (en) * | 2012-04-12 | 2013-10-17 | General Electric Company | Turbine shell displacement monitoring system |
CN103376082A (en) * | 2012-04-12 | 2013-10-30 | 通用电气公司 | Turbine shell displacement monitoring system |
US20170008645A1 (en) * | 2015-07-06 | 2017-01-12 | The Boeing Company | Body Fuel Tank Critical Gap Measurement and Validation Template |
US9815542B2 (en) * | 2015-07-06 | 2017-11-14 | The Boeing Company | Body fuel tank critical gap measurement and validation template |
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