[0001] This invention pertains to gas compressors, and in particular to a gas compressor
of novel design in which the compression cylinder thereof confines therewithin both
the inlet and discharge valves, and the latter valves are piston ringed to serve as
the gas compressing pistons.
[0002] Conventional, prior art gas compressors require inlet and discharge valves, and gas
compressing pistons. Too, commonly, the valves are external to the compression cylinder.
[0003] It is an object of this invention to set forth a novel gas compressor which obviates
any need for separate pistons, and such a compressor of simple, albeit efficient configuration.
[0004] Particularly, it is an object of this invention to set forth a gas compressor comprising
a cylinder having a longitudinal axis; and headers at opposite ends of said cylinder;
wherein one of said headers has a tapped hole formed in a surface thereof which opens
onto said cylinder; the other of said headers has a tapped bore opening therethrough;
and a first inlet valve threadedly engaged with said tapped hole and confined within
said cylinder; a second inlet valve threadedly engaged with said tapped bore and confined
within said cylinder; said second inlet valve has a throughgoing bore formed therein
which is coaxial with said tapped bore; a piston rod in penetration of said bores,
and having an end projecting outwardly from said other header; a pair of discharge
valves coupled to said piston rod, and spaced apart along said rod, confined within
said cylinder; gas inlet ports formed in said cylinder at opposite ends thereof; and
a gas outlet port formed in said cylinder intermediate said ends thereof.
[0005] Further objects of this invention, as well as the novel features thereof, will become
more apparent by reference to the following description, taken in conjunction with
the accompanying figures, in which:
Figure 1 is a perspective illustration of a gas compressor, according to an embodiment
of the invention, the same being partly cut away along the axis thereof;
Figure 2 is a perspective illustration of the piston rod assembly of the Figure 1
embodiment, the same also being cut away in part;
Figure 3 is a partly cut away perspective illustration of the cylinder and porting;
and
Figures 4 and 5 are cut away depictions of the frame header assembly and outer header
assembly, respectively, showing the tie rods and the inlet valves.
[0006] As shown in the figures, the novel compressor 10 comprises a straight cylinder 12,
having a longitudinal axis 14, with shouldered recesses 16 and 18 at opposite axial
ends thereof. An outer header 20, having a prominent, circular land 22 in the centre
thereof, is set, with an O-ring for sealing, into the recess 16. Similarly, a frame
header 24, which also has a prominent, circular land 26 in the centre thereof, is
set too with an O-ring for sealing, into the recess 18.
[0007] The header 20 has a tapped hole 28 formed in the land 22. An inlet valve 30, having
a threaded stub 32, is threadedly engaged with the hole 28. Valve 30, of the one-way,
check type, has an annular body 34 with piston ring grooves 36 formed thereabout (in
which to receive piston rings). The land 26 in the frame header 24 also has a tapped
bore 38 formed therein; it threadedly receives a second inlet valve 30a. Valve 30a,
however, is centrally bored to accommodate therethrough a piston rod 40.
[0008] The piston rod 40 penetrates the tapped bore 38 and is slidably engaged with the
central bore in the valve 30a. One end of the piston rod 40 projects outwardly from
the header 24, via one end thereof, and into the cylinder 12 via the opposite end
thereof. The termination of the in-cylinder end of the rod 40 is threaded; too, intermediate
the length of the rod 40 there is a shoulder 42. A tubular spacer 44, internally threaded
at one end thereof, and externally threaded at opposite ends thereof, is set against
the shoulder 42, and threadedly engaged with the threaded termination of the rod 40.
A pair of discharge valves 46 and 46a, the same having annular bodies 48, are centrally
threaded and threadedly engaged with external threads of the spacer 44. Valves 46
and 46a, too, are of the one-way, check type, and also have piston ring grooves formed
thereabout in which to nest piston rings for sealing against the inner surface of
th cylinder 12.
[0009] A pair of inlet ports 50 and 50a are formed in the cylinder 12, adjacent to the axial
ends thereof, the same opening onto the inlet valves 30 and 30a. Intermediate the
length of the cylinder 12 there is also formed a single discharge port 52. Ends of
the cylinder 12 abut the headers 20 and 24 and nest, in grooves formed therefor, O-ring
seals 54. Tie rods 56, fastened in the header 24, and in penetration of the header
20, receive nuts 58 on the threaded ends thereof and clamp the cylinder 12 and the
headers 20 and 24 securely together. Inlet conduits 60 and 60a are welded to the cylinder
12 for communication with the ports 50 and 50a, and a discharge conduit 52 is similarly
welded to the cylinder 12 for communication with the discharge port 52.
[0010] The simplicity of the configuration of the compressor 10, in this embodiment thereof,
can readily be seen; the same offers manufacturing and maintenance ease. More significantly,
pistons per se are not required, as the valves 46 and 46a serve the double purpose
of piston-compression of the gas, and valved discharge of the compressed gas. Only
inlet and discharge ports need to be formed in the cylinder 12, as the valves 30 and
30a, and 46 and 46a are confined within the cylinder. The headers 20 and 24 fit firmly
into the ends of the simple, straight cylinder 12, and only tie rods are required
to clamp the assembly together.
1. A gas compressor (10), comprising:
a single, straight, walled cylinder (12) having (a) a longitudinal axis (14), and
(b) a single, circumferential wall; and
headers (20, 24) at opposite ends of said cylinder (12); wherein
one of said headers (20) has a tapped hole (28) formed in a surface thereof which
opens onto said cylinder (12);
the other of said headers (24) has a tapped bore (38) opening therethrough; and
a first inlet vlave (30) threadedly engaged with said tapped hole (28) and confined
within said cylinder (12);
a second inlet valve (30a) threadedly engaged with said tapped bore (38) and confined
within said cylinder (12);
said second inlet valve (30a) has a throughgoing bore formed therein which is coaxial
with said tapped bore (38);
a piston rod (40) in penetration of said bores, and having one end thereof projecting
outwardly from said other header (24);
a pair of discharge valves (46, 46a) coupled to said piston rod (40), and spaced
apart along said rod (40), confined within said cylinder (12);
gas inlet ports (50, 50a) radially formed in said cylinder (12) at opposite ends
thereof; and
a gas outlet port (52) formed in said cylinder intermediate said ends thereof.
2. A gas compressor according to claim 1, wherein:
said inlet ports (50, 50a) open directly onto said cylinder-confined inlet valves
(30, 30a).
3. A gas compressor, according to claim 1, wherein:
said discharge valves (46, 46a) have annular bodies (48); and
said bodies (48) have piston ring grooves formed thereon to accommodate therein
piston rings for effecting sealing engagement with said cylinder (12).
4. A gas compressor, according to claim 3, wherein:
the end of said piston rod (40) which is opposite said projecting end thereof is
threaded; and further including
a tubular spacer (44), internally and externally threaded, is threadedly engaged
with said threaded, opposite end of said piston rod (40);
said bodies (48) are internally threaded; and
said bodies (48) are threadedly engaged with said tubular spacer (44).
5. A gas compressor, according to claim 4, wherein:
said spacer (44) is externally threaded, as aforesaid, at opposite ends thereof;
and
said bodies (48) are threadedly engaged with said spacer (44) at said threaded
ends of said spacer (44).
6. A gas compressor, according to claim 1, wherein:
opposite axial ends of said cylinder (12) have shouldered recesses (16, 18) formed
therein;
said headers (20, 24) have circular lands (22, 26) in the centres thereof; and
said lands (22, 26) are set into said shouldered recesses (16,18).
7. A gas compressor, according to claim 6, further including:
seals (54) interposed between said headers (20,24) and said opposite axial ends
of said cylinder (12).
8. A gas compressor, according to claim 6, further including:
tie rods (56) fastened to said headers (20, 24) securing said headers (20, 24)
to opposite axial ends of said cylinder (12).
9. A gas compressor, according to claim 4, wherein:
said spacer (44), discharge valves (46, 46a), and said cylinder (12) cooperatively
define, within said cylinder, a fixed volume, gas-discharge chamber which opens onto
said outlet port (52).
10. A gas compressor, according to claim 3, wherein:
said discharge valves (46, 46a) comprise gas compressing pistons.