[go: up one dir, main page]

US1774106A - Piston - Google Patents

Piston Download PDF

Info

Publication number
US1774106A
US1774106A US300643A US30064328A US1774106A US 1774106 A US1774106 A US 1774106A US 300643 A US300643 A US 300643A US 30064328 A US30064328 A US 30064328A US 1774106 A US1774106 A US 1774106A
Authority
US
United States
Prior art keywords
expansion
skirt
rate
piston
strut
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
Application number
US300643A
Inventor
Adolph L Nelson
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.)
Bohn Aluminum and Brass Corp
Original Assignee
Bohn Aluminum and Brass Corp
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 Bohn Aluminum and Brass Corp filed Critical Bohn Aluminum and Brass Corp
Priority to US300643A priority Critical patent/US1774106A/en
Application granted granted Critical
Publication of US1774106A publication Critical patent/US1774106A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F3/00Pistons 
    • F02F3/02Pistons  having means for accommodating or controlling heat expansion
    • F02F3/04Pistons  having means for accommodating or controlling heat expansion having expansion-controlling inserts
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/02Light metals
    • F05C2201/021Aluminium
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05CINDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00Metals
    • F05C2201/04Heavy metals
    • F05C2201/0433Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0448Steel
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49229Prime mover or fluid pump making
    • Y10T29/49249Piston making

Definitions

  • This invention relates to pistons, particularly to pistons for internal combustion engines, and aims to provide means for accurately controlling the rate of expansion of the piston skirt.
  • the piston skirt expansion has generally been expressed in terms of the cyl inder and the clearance between the cylinder and the piston. This is not a reliable standard of reference since it is very generally recognized by the engineering fraternity that the cylinder expansion is a variable quantity and that the temperature range of the cylinder has no fixed relation to that of the piston skirt.
  • the rate of expansion of the piston skirt will be defined in terms of a suitable comparison that will give an exact unit of measure.
  • the rate of skirt expansion found most suitable under the circumstances may be such that it could not be obtained by combining any of the commercially available materials in a structure relying solely on the B0 expansion rate of the materials to control the The skirt expansion rate. But in the present invention any desired rate of expansion may be accurately obtained by choosing a suitable commercial material and selecting a proper arrangement of parts.
  • Fig. 1 is an elevation of a piston embodying the invention
  • Fig. 2 is a longitudinal section through the piston shown in Fig. 1;
  • Fig. 3 is a cross sectionon line 33 of Fig. 2 including a diagram representing the analysis of the expansion rate of the piston skirt;
  • Fig. 4 is a curve chart showing how the linear coeflicient of expansion of nickel-iron alloy varies with the nickel content
  • Fig. 5 is a curve chart showing how the piston skirt expansion rate varies with angle 0 of Fig. 3;
  • Fig. 6 is a modification showing how the length of the strut can be varied
  • Fig. 7 is a modification showing a single diam'etral strut
  • Fig. 8 is a further modification showing a strutted ring
  • Fig. 9 is a section on line 99 of Fig. 8.
  • Fig. 10 is a chart representing a certain phase of the invention.
  • Figs. 1 and 2 illustrate a piston of the type set forth in said copending application.
  • the piston skirt includes two slipper sections 10 and 11 which are held in spaced-apart relation by the struts 12 and 13.
  • Fig. 3 includes a diagram representing the analysis of the expansion rate of the piston skirt.
  • the points A, B, C and D represent the neutral points (regarding relative movement) in the joints between the struts and the slipper sections.
  • a diameter through point A makes an angle 0 with the diameter parallel to the struts.
  • Points E and F are opposite peripheral points in the diameter through A.
  • the material of the skirt is taken as an aluminum alloy having a coefficient of linear expansion of 000001234 per degree Fahrenheit. The examples will show the results by using strut materials having Various expansion rates.
  • a H will next resolve A H into two components, one, A I, normal to the skirt wall at E and the other, A J, parallel to the tangent at E.
  • a I represents the diametral expansion between C and A
  • a J is the expansion component parallel to the tangent and represents the peripheral movement of point A, or the distance it creeps along the cylinder wall.
  • To obtain the total resultant expansion of the skirt we must add the expansion fron A to E and from O to F, and we lay off I K to represent this expansion, taking distance A l] as 3.555 per cent of the piston diameter.
  • a K represents the total expansion from E to F on the diameter of the piston through point A.
  • the material used for the struts must have a consistent coefficient of 330 per cent per cent tual skirt expansion for the above materials for different values of angle 6, the angle 6 was varied from 20 to 40 degrees in increments of 2 degrees. (That is, five diagrams were made for each angle, one for each of the five materials.)
  • the skirt expansion found from each diagram was divided by the expansion of a cylindrical block of cast iron of equal diameter and temperature range to find the piston skirt expansion rate. These rates or ratios are plotted in Fig. 5 as ordinates against the angles of 6 as abscissus.
  • Curves I to V represent materials '1 to 5, respectively.
  • curve I gives us a rate of skirt expansion of 1.34, i. e., a skirt expansion rate 34 per cent greater than that of a cast iron cylinder of equal diameter and temperature range.
  • Curve V for the same angle gives us a rate of 0.43, i. e., 43 per cent of the expansion of cast iron.
  • the expansion rates from curves I and V are 1.74 and 1.25, i. e., we have 74 per cent greater expansion than cast iron with the struts of ordinary steel and 25 per cent greater expansion with the invar struts.
  • Fig. 6 shows a modification in which the distances A E and C F may be increased or decreased by varying the height of pedestal 14, resulting in a proportionate increase or decrease in vector I K (Fig. 3). In this case angle [3 may be varied without changing the height of pedestal 14.
  • Fig. 7 shows a strut across the central diameter of the skirt
  • Fig. 8 shows a strutted ring for controlling the skirt expansion.
  • An unsupported ring is a spring member, and while it would have a controlling influence upon the skirt expansion, it would not positively hold the skirt round and to size within the small variation permissible in a working piston.
  • a ring heavy enough to give the requisite rigidity would have prohibitive weight.
  • a strut is a bar member, and is the most eflicient type of member to space the skirt portions positively and keep the spacing constant under working conditions for long periods of time. It is therefore necessary, in order to obtain accurate results, to brace the ring by struts. It is to be understoodthat the principles herein disclosed will apply to an unbraced ring, although such a ring will not give the Ipositive results produced by rigid strut memers.
  • the same 120 is true of Fig. 9.
  • Equation (3) the values of R were calculated to plot the curves given in Fig. 10.
  • curves A, C and D, respectively are for materials 1, 2 and 5, previously mentioned.
  • Curve B is for a material (No. 6) having a coeflicient of expansion 0.4 that of ordinary steel, a material corresponding to a nickel-iron alloy containing 30.7 per cent of nickel.
  • the coefiicient of cast iron was taken as Fig. 10 gives at a glance the Various skirt expansion rates that can be elected at will by choosing suitable strut materials and Values of 'y.
  • curve A which is for material 1, having the same coeflicient of expansion as ordinary steel.
  • a skirt expansion rate of 1.79 i. e., 79 per cent greater than that of a cast iron cylinder of equal diameterand temperature range.
  • the skirt a rate of expansion the same as that of a cast iron cylinder, thereby keeping the clearance between the cylinder and the piston constant.
  • the rate of expansion of the skirt when controlled by a strut of ordinary steel is not the same as that of the cast iron cylinder, as explained above; and in the second place the temperature ranges of the piston and the cylinder are practically never the same.
  • the actual expansion for the cylinder and the piston could be equal only for the one condition of temperature ranges in which the difference in temperature ranges would exactly offset the difference in the expansion rates of the cylinder and piston skirt. It would be an extremely unusual coincidence for such a condition to occur in any engine.

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Description

Aug. 26, 1930. A. L. NELSON PISTON Filed Aug. 20, 1928 4 Sheets-Sheet Z 5 lzvzn-ron ATTORNEY Aug. 26, 1930. A. NELSON PISTON Filed Aug; 20, 1928 4 Sheets-Sheet w P. f 5 w w w W m m m M m m M w w w M m m M 0 0 0 0 0 0 0 0 x EN'OR Y 9111-0 NEY ,Aug. 26, 1930.
A. NELSON PISTON Filed Aug. 20, 1928 4 Sheets-Sheet VE TOR I ATTORNEY Au 26, 1930. A, L, QE N 1,774,106
PISTON Filed Aug. 20, 1928 4 Sheets-:Sheet '4 Valuer ofy fiiyarw 7am .9)
ATTORN EY Patented Aug. 26, 1930 UNITED STATES PATENT; OFF-ICE ADOLPH L. NELSON, OF DETROIT, MICHIGAN,- ASSIG'NOR TO BOHN ALUMINUM & BRASS CORPORATION, OF DETROIT, MICHIGAN PISTON Application filed August 20, 1928. Serial No. 300,643.
This invention relates to pistons, particularly to pistons for internal combustion engines, and aims to provide means for accurately controlling the rate of expansion of the piston skirt.
In the past the piston skirt expansion has generally been expressed in terms of the cyl inder and the clearance between the cylinder and the piston. This is not a reliable standard of reference since it is very generally recognized by the engineering fraternity that the cylinder expansion is a variable quantity and that the temperature range of the cylinder has no fixed relation to that of the piston skirt. In setting forth the present invention the rate of expansion of the piston skirt will be defined in terms of a suitable comparison that will give an exact unit of measure.
-Various types of pistons have been proposed in which auxiliary members are relied upon to control the expansion of the piston skirt. It is often assumed that the skirt will have a resultant expansion similar to that of the material of the controlling member, but 2 this assumption usually involves a very large percentage of error that should not be overlooked in accurate pistonengineering.
It is an object of this invention to provide a piston in which the arrangement of parts and materials may be changed to give any selected rate of expansion of the piston ski-rt. fact that the piston skirt must work in :1. cylinder to which it is rather closely fitted and which has a temperature range different from 55 that of the skirt makes it desirable to select and use a rate of expansion to suit the difference in temperature ranges. For the most practical results it is desirable not only to compensate the expansion rate of the skirt to suit the temperature conditions, but at the same time to select a rate by experimental determination which will also increase or decrease the working clearance between the piston skirt and the cylinder as may be found desirable. The rate of skirt expansion found most suitable under the circumstances may be such that it could not be obtained by combining any of the commercially available materials in a structure relying solely on the B0 expansion rate of the materials to control the The skirt expansion rate. But in the present invention any desired rate of expansion may be accurately obtained by choosing a suitable commercial material and selecting a proper arrangement of parts.
The scope and practicability of this invention will become apparent from a study of the diagrams and curves herein set forth repreling the resultant rate 0 expansion of the piston skirt.
In the drawings:
Fig. 1 is an elevation of a piston embodying the invention; I
Fig. 2 is a longitudinal section through the piston shown in Fig. 1;
Fig. 3 is a cross sectionon line 33 of Fig. 2 including a diagram representing the analysis of the expansion rate of the piston skirt;
Fig. 4 is a curve chart showing how the linear coeflicient of expansion of nickel-iron alloy varies with the nickel content;
Fig. 5 is a curve chart showing how the piston skirt expansion rate varies with angle 0 of Fig. 3;
Fig. 6 is a modification showing how the length of the strut can be varied;
senting the fundamental fprinciples control- Fig. 7 is a modification showing a single diam'etral strut;
Fig. 8 is a further modification showing a strutted ring;
Fig. 9 is a section on line 99 of Fig. 8.
Fig. 10 is a chart representing a certain phase of the invention.
This application is in part a continuation of my copending application Serial No. 643,499, filed June 5, 1923, and Figs. 1 and 2 illustrate a piston of the type set forth in said copending application. The piston skirt includes two slipper sections 10 and 11 which are held in spaced-apart relation by the struts 12 and 13.
Fig. 3 includes a diagram representing the analysis of the expansion rate of the piston skirt. In this figure the points A, B, C and D represent the neutral points (regarding relative movement) in the joints between the struts and the slipper sections. A diameter through point A makes an angle 0 with the diameter parallel to the struts. Points E and F are opposite peripheral points in the diameter through A. For the examples given the material of the skirt is taken as an aluminum alloy having a coefficient of linear expansion of 000001234 per degree Fahrenheit. The examples will show the results by using strut materials having Various expansion rates.
To make an analysis of the resultant expansion of the skirt we will first find the expansion between points E and F, Fig. 3, then divide this expansion by that of a solid cylindrical block of cast iron of equal diameter. That is, we will use a cylindrical block of cast iron, which has a coefficient of expansion of 000000556 per 1-F., as a standard reference or unit of measure for comparing the actual skirt expansion for equal diameters and temperature ranges. The ratio of the expansion thus defined we will call the piston skirt expansion rate. I
To lay out the diagram of expansion components as given in Fig. 3 We first calculate the expansion between points A. and B. Using A as a pole we lay off G (on line A B extended) to represent this expansion. (For convenience a piston having a diameter of 3.375 in. was used and the temperature range was taken from to 212 F. On the vectors one inch on the original drawing represents .001 inch expansion, and it will be apparent that in the printed patent this scale will be reduced Next we calculate the expansion from D to A, using ordinary steel in the struts, and represent this by G H. Drawing A H we have a line representing the combined expansive movement of point A in reference to point C. )Ve will next resolve A H into two components, one, A I, normal to the skirt wall at E and the other, A J, parallel to the tangent at E. Then A I represents the diametral expansion between C and A, while A J is the expansion component parallel to the tangent and represents the peripheral movement of point A, or the distance it creeps along the cylinder wall. To obtain the total resultant expansion of the skirt we must add the expansion fron A to E and from O to F, and we lay off I K to represent this expansion, taking distance A l] as 3.555 per cent of the piston diameter. Then A K represents the total expansion from E to F on the diameter of the piston through point A.
On this same figure we have superimposed a diagram for a strut material having acoefficient of expansion of 0000000636 per 1 F, or that of ordinary steel. Since the expansion between points A and B is the same in this case line A G remains the same, but the strut expansion between A and D will be only of G H, or G L, and line A L represents the combined expansive movement of point A in reference to point C. Resolving A L into two components we get A M and A N. Laying off M O, equal to- I K, we
get A O representing the resultant diametral expansion for the skirt when the coefficient of expansion of the strut material is that of ordinary steel. Line A N is the expansion component parallel to the tangent.
It will be apparent from these diagrams that when a strut material having a lower coefficient of expansion is used the resultant normal to the skirt wall is materially decreased, while the resultant parallel to the tangent is greatly increased.
It will further be observed from Fig. 3 that increasing angle 6 decreases the length of the strut, A D, and increases the distance A B of the skirt, thereby changing the resultant expansion of the skirt.
To illustrate how changes of strut mate'- rial and/or angle 6 affect the resultant skirt expansion, a series of diagrams similar to Fig. 3 were drawn accurately and to scale for the following examples of material:
lllaterial 1Having a coellicient of expansion of 000000030 (ordinary steel).
Material 2-Having a coel'licient of expansion of 0.0000015) 4 that of ordinary steel Material 3-Having a coeflicient of expansion of 000000109 that of ordinary steel).
Material 4Having a coeflicient of expansion of 0000000636 that of ordinary steel).
Material 5Having a coefficient of expansion of 0000000226 (invar).
Any suitable materials having the above coeflicients of expansion would produce the desired results in the illustrations given, but it is to. be noted that materials having these coefficients are available in commercial nickel-iron alloys. The curve chart of Fig. 4 shows how the coeflicient of linear expansion of' such an alloy varies with the nickel content. Plotted values of the coellieient between 31 and 36 per cent nickel as iven by different authorities agree very well and since this is the flatter part of the curve commercial pro-ducts can be kept within reasonable distance of the curve. On the other hand the change is quite rapid between 26 and 31 per cent nickel and this part of the curve is not so reliable. The material used for the struts must have a consistent coefficient of 330 per cent per cent tual skirt expansion for the above materials for different values of angle 6, the angle 6 was varied from 20 to 40 degrees in increments of 2 degrees. (That is, five diagrams were made for each angle, one for each of the five materials.) The skirt expansion found from each diagram was divided by the expansion of a cylindrical block of cast iron of equal diameter and temperature range to find the piston skirt expansion rate. These rates or ratios are plotted in Fig. 5 as ordinates against the angles of 6 as abscissus.
' The chart of Fig. 5 shows quite clearly the cooperative relation between the strut material and the value of angle 6. A few examples will demonstrate how-a proper combination of these two factors will produce any desired piston skirt expansion rate.
Curves I to V represent materials '1 to 5, respectively.
For an angle 6 of 20, curve I gives us a rate of skirt expansion of 1.34, i. e., a skirt expansion rate 34 per cent greater than that of a cast iron cylinder of equal diameter and temperature range. Curve V for the same angle gives us a rate of 0.43, i. e., 43 per cent of the expansion of cast iron. For an angle of 46 the expansion rates from curves I and V are 1.74 and 1.25, i. e., we have 74 per cent greater expansion than cast iron with the struts of ordinary steel and 25 per cent greater expansion with the invar struts.
Attention is called to the fact that for 6=20 the strut of ordinary steel gave a skirt expansion rate greater than cast iron, while invar gave far less. For 6=46 the expansion rate for struts of ordinary steel is still greater, while even the invar strut gives an expansion rate greater than that for cast iron. This illustrates clearly that the rate of expansion cannot be controlled within the desired limits by relying solely on a selection of materials, while the combination of proper strut material and the proper angle 6 will give any desired piston skirt expansion rate.
Suppose that we wanted a skirt expansion rate identical with that of cast iron, i. e., a rate of 1.00. If invar is to be used as the strut material we run from 1.00 on the ordinates across to curve V and find we must use an angle 6 of 39. This would give us a rate approximately suitable for an automobile engine piston.
Suppose we found from actual production that a slightly higherv rate of expansion would be desirable to give a minimum amount of trouble from piston slaps, and we decided to try a production run of pistons having a rate of 1.10, or a 10 per cent increase in expansion. If we are using invar, curve V shows that we must use a 6 of 42.
Suppose again that experience with the finished automobiles shows that this last rate of skirt expansion is satisfactory but we-desire to save in cost of materials by reducing the nickel content of the strut steel Curve II corresponds to a lower nickel content and shows that with material 2 an angle 6 of 38 will produce the desired skirt expansion rate of 1.10. If a new and cheaper materialsuitable for struts should be brought out we would plot a curve corresponding to its coefiicient of expansion and then obtain the angle 6 which would have to be used in order to keep the pistonskirt expansion rate identical with that already found to be desirable. In other words, having once determined the most suitable skirt expansion rate we can easily determine the angle 6 required to produce that rate with any given strut material.
The above examples illustrate the results obtainable by having an exact unit of comparison for measuring skirt expansion and by intelligently selecting a strut material and. arrangement'of parts to produce a rate of skirt expansion found to be satisfactory in actual use.
In the examples given so far it has been assumed that the distance A E remained a constant ratio to diameter E F, Fig. 6 shows a modification in which the distances A E and C F may be increased or decreased by varying the height of pedestal 14, resulting in a proportionate increase or decrease in vector I K (Fig. 3). In this case angle [3 may be varied without changing the height of pedestal 14.
Fig. 7 shows a strut across the central diameter of the skirt, while Fig. 8 shows a strutted ring for controlling the skirt expansion. An unsupported ring is a spring member, and while it would have a controlling influence upon the skirt expansion, it would not positively hold the skirt round and to size within the small variation permissible in a working piston. A ring heavy enough to give the requisite rigidity would have prohibitive weight. A strut is a bar member, and is the most eflicient type of member to space the skirt portions positively and keep the spacing constant under working conditions for long periods of time. It is therefore necessary, in order to obtain accurate results, to brace the ring by struts. It is to be understoodthat the principles herein disclosed will apply to an unbraced ring, although such a ring will not give the Ipositive results produced by rigid strut memers.
In Fig. 7 the strut length may be varied from the extreme of y=0 to y=1. The same 120 is true of Fig. 9.
In the case of Fig. 3 we gave a graphical presentation of the analysis of the expansion rate of the skirt. For Figs. 7 and 9 we will give an analytical derivation.
From Figs. 7 and 9 it will beseen that 3 is the ratio of the strut length g X to the diameter of the skirt X. Thus for g =0.5 the strut is half as long as diameter X.
Now let: =the coefficient of expansion for 130 cast iron per 1 F. T temperature range in degrees F. (e. g., 21270=14l2). Then the expansion for cast iron for diameter X would be Dividing Equation (2) by Equation (1) we get the-ratio of the resultant skirt expansion to that of cast iron for equal diameter and temperature range. Let us call this ratio R, then,
R= 2/( (3) 'Y 'Y Using Equation (3) the values of R were calculated to plot the curves given in Fig. 10. In this figure curves A, C and D, respectively, are for materials 1, 2 and 5, previously mentioned. Curve B is for a material (No. 6) having a coeflicient of expansion 0.4 that of ordinary steel, a material corresponding to a nickel-iron alloy containing 30.7 per cent of nickel. The skirt material for all curves is aluminum alloy (a=0.00001234=). The coefiicient of cast iron was taken as Fig. 10 gives at a glance the Various skirt expansion rates that can be elected at will by choosing suitable strut materials and Values of 'y. Some examples will illustrate the use of the curves and emphasize the advantages of the possible combination.
Let us first consider curve A, which is for material 1, having the same coeflicient of expansion as ordinary steel. For a value of 31 04 we get a skirt expansion rate of 1.79, i. e., 79 per cent greater than that of a cast iron cylinder of equal diameterand temperature range. Now let us take y=1.0, which is the extreme theoretical limit for the length of the strut. Then we would have an expansion rate of 1.14:, or 14 per cent more than for cast iron. Let us consider a skirt 3 inches in diameter with 0.1 in. of skirt metal between the end of the strut and the outer end of the skirt diameter which gives the greatest practicable length for the strut. In this case 3 0983. Referring this value of y to the chart we get a rate of 1.21. In other words, with a strut as shown in Figs. 8 or 9 formed of ordinary steel the closest we can come theoretically to a cast iron rate is 14 per cent above the cast iron rate, while the closest we can come in actual practice is 21 per cent above cast. iron. This example shows that it is an error to assume that a strut or rigid ring of ordinary steel will control Lhe skirt expansion in such a way as to give duced.
the skirt a rate of expansion the same as that of a cast iron cylinder, thereby keeping the clearance between the cylinder and the piston constant. In the first place the rate of expansion of the skirt when controlled by a strut of ordinary steel is not the same as that of the cast iron cylinder, as explained above; and in the second place the temperature ranges of the piston and the cylinder are practically never the same. The actual expansion for the cylinder and the piston could be equal only for the one condition of temperature ranges in which the difference in temperature ranges would exactly offset the difference in the expansion rates of the cylinder and piston skirt. It would be an extremely unusual coincidence for such a condition to occur in any engine.
Again referring to Fig. 10 let us assume that we want a piston skirt having a rate of 1.05. If we wish to use material No. 6 We find from curve B that we must use a value of g =0.66, i. e., by making the strut length 66 per cent of the piston diameter We obtain the desired expanslon rate.
It will be clear from the above that the structures of Figs. 6, 7 and 8 can be used to produce any desired skirt expansion rate just as accurately as the structure of Fig. 3. It will also be evident that the controlling members may be located at any desired point longitudinally of the skirt.
The above disclosure makes it clear that by a proper combination of commercial materials and skirt structure a piston skirt having any selected rate of expansion can be pro- The selected rate may be one that cannot possibly be obtained by relying on choice .of materials alone since the rate may not correspond to the expansion rate of any known material. Obviously the principles herein set forth can be applied to modified structures and to any materials Without departure from the true spirit and scope of the invention.
1 claim: a
The method of making a piston having a skirt with opposite bearing surfaces, and a control member connected to the bearing surfaces at the ends of a diameter passing through the centers of the bearing surfaces, the control member being of a material having a different rate of expansion from that of the material of the skirt, which comprises giving the control member a predetermined diametrical length such that the relative amounts of the strut material and skirt material along said diameter, and the coefficients of expansion of the materials of the skirt and struts cooperate to produce a predetermined rate of expansion along said diameter.
In testimony whereof I aflix my signature.
ADOLPH L. NELSON.
US300643A 1928-08-20 1928-08-20 Piston Expired - Lifetime US1774106A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US300643A US1774106A (en) 1928-08-20 1928-08-20 Piston

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US300643A US1774106A (en) 1928-08-20 1928-08-20 Piston

Publications (1)

Publication Number Publication Date
US1774106A true US1774106A (en) 1930-08-26

Family

ID=23159973

Family Applications (1)

Application Number Title Priority Date Filing Date
US300643A Expired - Lifetime US1774106A (en) 1928-08-20 1928-08-20 Piston

Country Status (1)

Country Link
US (1) US1774106A (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327594A (en) * 1964-10-08 1967-06-27 Hepworth & Grandage Ltd Pistons for internal combustion engines
US4910093A (en) * 1988-04-01 1990-03-20 Berchem & Schaberg Gmbh Piston blank for a forged piston

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3327594A (en) * 1964-10-08 1967-06-27 Hepworth & Grandage Ltd Pistons for internal combustion engines
US4910093A (en) * 1988-04-01 1990-03-20 Berchem & Schaberg Gmbh Piston blank for a forged piston

Similar Documents

Publication Publication Date Title
Almen et al. The uniform-section disk spring
US1774106A (en) Piston
US2769227A (en) Welded joint between ferritic and austenitic steel members
Ferguson et al. A variable thickness, curved beam and shell stiffening element with shear deformations
Hansen et al. Sensitivity analysis in multiple objective linear programming: The tolerance approach
JPH07107383B2 (en) Adaptive control system for internal combustion engine
Jin et al. Noether symmetries for non-conservative Lagrange systems with time delay based on fractional model
Yuan et al. On Radial Deflections of a Cylinder Subjected to Equal and Opposite Concentrated Radial Loads: Infinitely Long Cylinder and Finite-Length Cylinder With Simply Supported Ends
US1681709A (en) Piston
Sudit Additive nonhomogeneous production functions in telecommunications
Amemiya Some theorems in the linear probability model
Royle Inherent non-linear effects in hydraulic control systems with inertia loading
US1745860A (en) Piston
Kleiman et al. The relationship between two measures of total productivity
Mücke et al. A posteriori error estimates and adaptivity for finite element solutions in finite elasticity
Ponter Deformation bounds for the Bailey-Orowan theory of creep
US868264A (en) Compensation device for torsional pendulums.
GUPTA et al. Torque Roll Axis and Its Influence on Automotive Engine Mountlngs
Westlund Damage induced structural instability
Perls et al. Frequency Response of Second-Order Systems With Combined Coulomb and Viscous Damping¹
Gotoh The damping of the large wave-number disturbances in a free boundary layer flow
Bentley et al. Gas Pressure Torque of Radial Engines
Smalley et al. Liquid metal bearing technology for large, high-temperature, sodium rotating machinery. Third topical report design data handbook for externally pressurized journal bearings including turbulence and inertia effects
Bhaskar Gross modifications in structural dynamics via interpolated modes
Morley Transient Vibration by Vector Methods