Airspring and sleeve

Claim 2

In an airspring of the type with a sleeve having (1) a chamber portion connected at an end to a closure member and (2) a rolling lobe portion connected at an end to a piston, the sleeve of the elastomeric type reinforced with successive layers of embedded cords disposed at opposite helical angles, the improvement comprising: cords in each of the successive layers wound at inconstant helical angles in an annular band portion of one of the sleeve portions from first opposite helical angles to second opposite helical angles.

Claim 3

The airspring as claimed in claim 1 wherein the band portion defines a means for establishing an inflated contour of the sleeve.

Claim 4

The airspring as claimed in claim 1 wherein the band portion is in the rolling lobe portion.

Claim 5

The airspring as claimed in claim 1 wherein the band portion is in the chamber portion.

Claim 6

The airspring as claimed in claim 1 and further including a strut member extending from the end closure member and slidably through a center portion of the piston.

Claim 7

In an airspring of the type with with a sleeve having (1) a chamber portion connected to an end to an closure member and (2) a rolling lobe portion connected at an end end to a piston, the sleeve of the elastomeric type reinforced with embedded fibrous members, the improvement comprising: means for contouring a band portion of the rolling lobe portion to an effective diameter that decreases as part of the rolling lobe portion is rolled into the chamber portion by means of the piston to thereby decrease the effective spring rate of the airspring wherein the contouring means comprises an embedded fibrous reinforcement of successive layers of cord wound at opposite helical angles in successive layers, the cords wound at inconstant helical angles in an annular band portion of the rolling lobe portion from first opposite helical angles to second opposite helical angles.

Claim 8

In an airspring of the type with with a sleeve having (1) a chamber portion connected to an end to an closure member and (2) a rolling lobe portion connected at an end end to a piston, the sleeve of the elastomeric type reinforced with embedded fibrous members, the improvement comprising: means for contouring a band portion of the rolling lobe portion to an effective diameter that decreases as part of the rolling lobe portion is rolled into the chamber portion by means of the piston to thereby decrease the effective spring rate of the airspring wherein the contouring means comprises an embedded fibrous reinforcement of successive layers of cord wound at opposite helical angles in successive layers, the cords wound at inconstant helical angles in an annular band portion of the rolling lobe portion from first opposite helical angles to second opposite helical angles.

Claim 9

The airspring as claimed in claim 6 wherein the cords in the rolling lobe portion are at constant and first opposite helical angles in a range from about 30 to about 45 degrees and at a second larger angle from about 40 to about 55 degrees.

Claim 10

In an airspring of the type with a sleeve having (1) a chamber portion connected at an end to a closure member and (2) a rolling lobe portion connected at an end to a piston, the sleeve of the elastomeric type reinforced with embedded fibrous members, the improvement comprising: means for contouring a band portion of the sleeve to increase an inflated volume of the chamber portion wherein the contouring means comprises an embedded fibrous reinforcement of successive layers of cords wound at opposite helical angles in successive layers, the cords would at inconstant helical angles in an annular band portion of the chamber portion from first opposite helical angles to second opposite helical angles.

Claim 11

In an airspring of the type with a sleeve having (1) a chamber portion connected at an end to a closure member and (2) a rolling lobe portion connected at an end to a piston, the sleeve of the elastomeric type reinforced with embedded fibrous members, the improvement comprising: means for contouring a band portion of the sleeve to increase an inflated volume of the chamber portion wherein the contouring means comprises an embedded fibrous reinforcement of successive layers of cords wound at opposite helical angles in successive layers, the cords would at inconstant helical angles in an annular band portion of the chamber portion from first opposite helical angles to second opposite helical angles.

Claim 12

The airspring as claimed in claim 8 wherein the cords of the chamber portion are from a first opposite helical angle in a range from about 40 to 55 degrees to lesser second helical angle in a range from about 45 to 30 degrees.

Claim 13

In an airspring sleeve having a chamber portion interconnecting a rolling lobe portion and of the elastomeric type reinforced with successive layers of embedded cords wound at opposite helical angles, the improvement comprising: cords of successive layers wound at inconstant helical angles in an annular band portion of one of the sleeve portions from first opposite helical angles to second opposite helical angles.

Claim 14

In an airspring sleeve having a chamber portion interconnecting a rolling lobe portion and of the elastomeric type reinforced with successive layers of embedded cords wound at opposite helical angles, the improvement comprising: cords of successive layers wound at inconstant helical angles in an annular band portion of one of the sleeve portions from first opposite helical angles to second opposite helical angles.

Claim 15

The airspring sleeve as claimed in claim 10 wherein the band portion defines a means for establishing an inflated contour of the sleeve.

Claim 16

The airspring sleeve as claimed in claim 10 wherein the band portion is in the chamber portion of the sleeve.

Claim 17

The airspring sleeve as claimed in claim 10 wherein the band portion is in the rolling lobe portion.

Claim 18

The airspring sleeve as claimed in claim 13 wherein the band portion is in the rolling lobe portion and juxtaposed the chamber portion.

Claim 19

The airspring sleeve as claimed in claim 10 wherein the band portion has a width measured axially of the sleeve that is at least about 0.5 in.

Claim 20

The airspring sleeve as claimed in claim 10 wherein the sleeve is substantially cylindrical.

Claim 21

The airspring sleeve as claimed in claim 10 wherein the sleeve is substantially frustoconical.

Claim 22

The airspring sleeve as claimed in claim 10 wherein the absolute difference between the first and second opposite helical angles is at least about five degrees.

Claim 23

The airspring sleeve as claimed in claim 10 wherein the inconstant helical angles of the band are substantially in the rolling lobe portion and are followed by a second and opposite inconstant helical angles in a second annular band portion substantially in the chamber portion, the opposite helical angles of the second band portion from the second opposite helical angles to third opposite helical angles.

Claim 24

The airspring sleeve as claimed in claim 19 wherein the first opposite helical angle is from about 30 to about 45 degrees, the second opposite helical angle is from about 40 to 55 degrees, and the third opposite helical angle is from about 30 to about 45 degrees.

Claim 25

In an airspring sleeve having a chamber portion interconnecting a rolling lobe portion and of the elastomeric type reinforced with successive layers of embedded cords wound at opposite helical angles, the improvement comprising: cords and each of the successive layers wound at a first helical angle in the chamber portion and at a second, unequal angle in the rolling lobe portion.

Claim 26

In an airspring sleeve having a chamber portion interconnecting a rolling lobe portion and of the elastomeric type reinforced with successive layers of embedded cords wound at opposite helical angles, the improvement comprising: cords and each of the successive layers wound at a first helical angle in the chamber portion and at a second, unequal angle in the rolling lobe portion.

Claim 27

The airspring sleeve as claimed in claim 21 wherein the angle in the chamber portion is greater than the angle in the rolling lobe portion.

Claim 28

The airspring sleeve as claimed in claim 22 wherein the first helical angle is in a range from about 10 to about 89 degrees and the second helical angle is in a range from about 30 to about 62 degrees.

Claim 29

The airspring sleeve as claimed in claim 21 wherein the first helical angle is in a range from about 20 to about 70 degrees and the second helical angle is in a range from about 35 to about 55 degrees.

Claim 30

The airspring sleeve as claimed in claim 21 wherein the first helical angle is in a range from about 30 to about 60 degrees and the second helical angle is in a range from about 38 to about 55 degrees.