Two-stage composite piston

Claim 2

A composite two-stage piston, comprising: an annular cup; a hollow annular core bonded to the periphery of said annular cup having an outer shell sized to receive a connecting rod within its interior; coupling means in said annular shell adapted to operatively couple the piston rod to the shell; an elongated first piston having a base at one of its ends and a first piston head formed at its other end, said base being entrained within and bonded to said cup; a second piston having an annular sleeve concentrically spaced from the periphery of said shell and a second piston head formed at one end of said sleeve about the base of said first piston bonded to said cup and said annular core; and at least one spacer ring interposed and bonded between said shell and sleeve.

Claim 3

The two-stage piston of claim 1, and said cup being formed of metal and said core, pistons and spacer ring being formed of a relatively lightweight plastic material.

Claim 4

The two-stage piston of claim 1, and said cup being formed of steel and said core and pistons being formed of a carbon fiber would epoxy resin plastic.

Claim 5

The two-stage piston of claim 1, and said shell having a pair of transversely aligned apertures and an annular collar bonded within each of said apertures sized to receive a transverse pin to form said coupling means adapted to secure the connecting rod to the shell.

Claim 6

The two-stage piston of claim 4, and clamping means in at least one of said annular collars adapted to secure the transverse pin against rotation within said collar.

Claim 7

The two-stage piston of claim 4, and at least one of said spacer rings being interposed and bonded between said shell and sleeve axially adjacent each side of said apertures.

Claim 8

The two-stage piston of claim 1, and said core having a head portion embracing the periphery of said cup, and said cup having a pair of axially spaced outwardly radiating annular rims embracing the marginal peripheral edges of said head portion.

Claim 9

The two-stage piston of claim 1, and said core including a generally conically-shaped head portion radiating inwardly from said shell to said cup, and said shell having an outer end portion abutting said second piston head.

Claim 10

The two-stage piston of claim 1, and said base having an annular shoulder about its periphery, and said cup having a pair of axially spaced inwardly radiating tabs retaining said shoulder within the cup.

Claim 11

The two-stage piston of claim 1, and each of said piston having at least one circumferential groove about its periphery sized to receive a piston ring therewithin.

Claim 12

The two-stage piston of claim 1, and said first piston having a metal sleeve secured about its other end proximate the first piston head, and said metal sleeve and said annular sleeve each having at least one circumferential groove about its periphery sized to receive a piston ring therewithin.

Claim 13

A composite two-stage piston for a compressor, comprising: an annular metal cup having a pair of axially spaced outwardly radiating annular rims disposed about its periphery and a pair of axially spaced inwardly radiating tabs; a hollow annular core having an outer shell sized to receive a connecting rod within its interior and a conically-shaped head portion bonded to said cup radiating inwardly from said shell in a fashion embracing the periphery of the cup between said annular rims; said shell having a pair of transversely aligned apertures and an annular collar bonded within each of said apertures sized to receive a transverse pin adapted to secure the connecting rod to the shell; a hollow elongated first piston having a base at one of its ends bonded to the cup and a first piston head at its other end, said base including an annular shoulder retained within the cup by said tabs; a second piston having an annular sleeve concentrically spaced from the periphery of said shell and a second piston head formed at one end of said annular sleeve about the base of said first piston bonded to said cup and the shell; a spacer ring interposed and bonded between said shell and sleeve axially adjacent each of said apertures; and said core, pistons and spacer rings being formed of a relatively lightweight plastic material.

Claim 14

A composite two-stage piston for a compressor, comprising: an annular metal cup having a pair of axially spaced outwardly radiating annular rims disposed about its periphery and a pair of axially spaced inwardly radiating tabs; a hollow annular core having an outer shell sized to receive a connecting rod within its interior and a conically-shaped head portion bonded to said cup radiating inwardly from said shell in a fashion embracing the periphery of the cup between said annular rims; said shell having a pair of transversely aligned apertures and an annular collar bonded within each of said apertures sized to receive a transverse pin adapted to secure the connecting rod to the shell; a hollow elongated first piston having a base at one of its ends bonded to the cup and a first piston head at its other end, said base including an annular shoulder retained within the cup by said tabs; a second piston having an annular sleeve concentrically spaced from the periphery of said shell and a second piston head formed at one end of said annular sleeve about the base of said first piston bonded to said cup and the shell; a spacer ring interposed and bonded between said shell and sleeve axially adjacent each of said apertures; and said core, pistons and spacer rings being formed of a relatively lightweight plastic material.