Piston engine with dynamic groove bearing internal to piston and isolated from compression space

Claim 2

A piston engine comprising a circular cylinder, a piston that is reciprocable in said cylinder for working on a gaseous medium present in said cylinder during engine operation, and means for reciprocating said piston in said cylinder, the improvement comprising: said piston being tubular and having an inner and outer wall surface of circular cross-section, said piston being open at one end and having a transverse end face at the opposite end, said engine having a compression space opposite said piston end face into which said gaseous medium is compressed during piston reciprocation, an elongate circular-cylindrical guide concentric with said cylinder having an outer surface, and extending into said piston through said open end, said outer surface of said guide and said inner wall surface of said piston comprising a dynamic groove bearing for centering said piston in said cylinder during reciprocation of said piston, and said piston being sized near said end face for forming a sealing gap with said cylinder, whereby said dynamic groove bearing is isolated from said compression space by said sealing gap.

Claim 3

A piston engine as claimed in claim 1, characterized in that said guide is a fixedly arranged mandrel.

Claim 4

A piston engine as claimed in claim 2, characterized in that said dynamic groove bearing cmprises a groove pattern on said outer surface of said guide.

Claim 5

A piston as claimed in claim 1, wherein said guide comprises a cavity at its end adjacent sai dpiston end face and said piston comprises a support extending into said cavity, and said engine further comprising a rotary electric motor comprising a stator coil secured in said cavity and a permanent rotor magnet fixed on said support and extending within said stator coil.

Claim 6

A piston engine as claimed in claim 3, further comprising a housing adjoining said cylinder at its end opposite said compression space, said piston extending out of said cylinder away from said compression space, and said housing having a wall radially spaced from said psiton, and said means for reciprocating said piston comprises an electric brushless translatory motor comprising stator coils secured to said housing wall and rotor magnets fixed to the outer surface of said piston.

Claim 7

A piston engine as claimed in claim 5, wherein said first set of grooves is axially located on said guide at said rotary motor, and said guide and said inner wall surface of said piston comprises a second groove dynamic bearing having a second set of grooves on said guide axially located at said translatory motor.

Claim 8

A compression device, comprising: a pair of opposing piston engines, each piston engine comprising, a circular cylinder, a piston reciprocable in said cylinder for working on a gaseous medium present in said cylinder during engine operation, said piston being tubular, having an inner and outer wall surface of circular cross-section, an open end and a transverse end face at the opposing end; means for translating said piston in said cylinder; an elongate guide concentric with said piston having a circular cylindrical outer surface and extending into said piston through said open end; said outer surface of said guide and said inner wall surface of said piston comprising a dynamic groove bearing for centering said piston in said engine during reciprocation of said piston; said piston being sized near its end face for forming a sealing gap with said cylinder, whereby said dynamic bearing is isolated from said compression space; and a housing joining said piston engines with said pistons aligned and with said piston end faces in opposition, said housing enclosing a compression space limited on opposing sides by said piston end faces.

Claim 9

A compression device, comprising: a pair of opposing piston engines, each piston engine comprising, a circular cylinder, a piston reciprocable in said cylinder for working on a gaseous medium present in said cylinder during engine operation, said piston being tubular, having an inner and outer wall surface of circular cross-section, an open end and a transverse end face at the opposing end; means for translating said piston in said cylinder; an elongate guide concentric with said piston having a circular cylindrical outer surface and extending into said piston through said open end; said outer surface of said guide and said inner wall surface of said piston comprising a dynamic groove bearing for centering said piston in said engine during reciprocation of said piston; said piston being sized near its end face for forming a sealing gap with said cylinder, whereby said dynamic bearing is isolated from said compression space; and a housing joining said piston engines with said pistons aligned and with said piston end faces in opposition, said housing enclosing a compression space limited on opposing sides by said piston end faces.

Claim 10

A compression device as claimed in claim 7, characterized in that said guide is a fixedly arranged mandrel.

Claim 11

A compression device as claimed in claim 8, wherein said guide comprises a cavity at its end adjacent said piston end face and said piston compreses a support extending into said cavity, and said engine further comprises a rotary electric motor comprising a stator coil secured in said cavity and a permanent rotor magnet fixed on said support and extending within said stator coil.

Claim 12

A compression device as claimed in claim 9, characterized in that said dynamic groove bearing comprises a groove pattern on said outer surface of said guide.

Claim 13

A compression device as claimed in claim 10, further comprising each piston engine having a housing portion adjoining said cylinder at its end opposite said compression space, said piston extending out of said cylinder away from said compression space and said housing portion having a wall radially spaced from said piston, and said means for reciprocating said piston comprises an electric brushless translatory motor comprising stator coils secured to said housing wall and rotor magnets fixed to the outer surface of said piston.

Claim 14

A compression device as claimed in claim 11, wherein said first set of grooves is axially located on said guide at said rotary motor, and said guide and said inner wall surface of said piston comprises a second grooved dynamic bearing the second set of grooves onsaid guide outer surface axially located at said translatory motor.

Claim 15

A cryo-cooler, comprising: a chamber defining an expansion space, a displacer reciprocable in said expansion space; and a piston engine for supplying a gaseous medium under pressure to said expansion space, said piston engine comprising, a circular cylinder, a piston reciprocable in said cylinder for working on a gaseous medium present in said cylinder during engine operation, said piston being tubular, having an inner and outer wall surface of circular cross-section, an open end and a transverse end face at its opposing end, said engine having a compression space opposite said piston end face into which said gas is compressed during piston operation, means for reciprocating said piston in said cylinder, an elongate guide concentric with said piston having a circular cylindrical outer surface and extending into said piston through said open end, said outer guide surface and said inner wall surface of said piston comprising a dynamic groove bearing for centering said piston in said engine during reciprocation of said piston, and said piston being sized near its end face for forming a sealing gap with said cylinder, whereby said dynamic bearing is isolated from said compression space; and a regenerator connected between said expansion space and said compression space of said piston engine.

Claim 16

A cryo-cooler, comprising: a chamber defining an expansion space, a displacer reciprocable in said expansion space; and a piston engine for supplying a gaseous medium under pressure to said expansion space, said piston engine comprising, a circular cylinder, a piston reciprocable in said cylinder for working on a gaseous medium present in said cylinder during engine operation, said piston being tubular, having an inner and outer wall surface of circular cross-section, an open end and a transverse end face at its opposing end, said engine having a compression space opposite said piston end face into which said gas is compressed during piston operation, means for reciprocating said piston in said cylinder, an elongate guide concentric with said piston having a circular cylindrical outer surface and extending into said piston through said open end, said outer guide surface and said inner wall surface of said piston comprising a dynamic groove bearing for centering said piston in said engine during reciprocation of said piston, and said piston being sized near its end face for forming a sealing gap with said cylinder, whereby said dynamic bearing is isolated from said compression space; and a regenerator connected between said expansion space and said compression space of said piston engine.

Claim 17

A cyro-cooler as claimed in claim 13, characterized in that said guide is a fixedly arranged mandrel.

Claim 18

A cryo-cooler as claimed in claim 14, wherein said guide comprises a cavity at its end adjacent said piston end face and said piston comprises a support extending into said cavity, and said engine further comprises a rotary electric motor comprising a stator coil secured in said cavity and a permanent rotor magnet fixed on said support and extending within said stator coil.

Claim 19

A cyro-cooler as claimed in claim 15, characterized in that said dynamic groove bearing comprises a groove pattern on said outer surface of said guide.

Claim 20

A cyro-cooler as claimed in claim 15, wherein said engine further compries a housing adjoining said cylinder at its end opposite said compression space, said piston extending out of said cylinder away from said compression space, and said housing having a wall radially spaced from said piston, and said means for reciprocating said piston comprises an electric brushless translatory motor comprising stator coils secured to said housing wall and rotor coils fixed to the outer surface of said piston.

Claim 21

A cyro-cooler as claimed in claim 17, wherein said first set of grooves is axially located on said guide at said rotary motor, and said guide and said inner surface of said piston comprise a second grooved dynamic bearing having a second set of grooves on said guide outer surface axially located at said translatory motor.

Claim 22

A cyro-cooler as cliamed in claim 18, further comprising another said piston engine, a housing joining said piston engines with said piston end faces aligned and opposing each other, said housing enclosing a compression space limited on opposing sides by said end faces.

Claim 23

A cyro-cooler as claimed in claim 19, wherein for each piston engine said guide is a fixedly arranged mandrel.

Claim 24

A cryo-cooler as claimed in claim 20, wherein for each engine said guide comprises a cavity at its end adjacent said piston end face and said piston comprises a support extending into said cavity, and each engine further comprises a rotary electric motor comprising a stator coil secured in said cavity and a permanent rotor magnet fixed on said support and extending within said stator coil.

Claim 25

A cryo-cooler as claimed in claim 21, wherein for each engine said dynamic groove bearing comprises a groove pattern on said outer surface of said guide.

Claim 26

A cyro-cooler as claimed in claim 22, wherein each engine further comprises a housing portion adjoining said cylinder at its end opposite said compression space, said piston extending out of said cylinder away from said compression space and said housing portion having a wall radially spaced from said piston, and said means for reciprocating said piston comprises an electric brushless translatory motor comprising stator coils secured to said housing wall and rotor magnets fixed to the outer surface of said piston.

Claim 27

A cyro-cooler as claimed in claim 23, wherein for each piston engine said first set of grooves is axially located on said guide at said rotary motor and said guide and said inner surface of said piston comprise a second grooved dynamic bearing having a second set of grooves on said guide outer surface axially located at said translatory motor.