Rotary air compressor with thermally responsive oil injection

• US 4,648,815 A
• Filed: 09/05/1985
• Issued: 03/10/1987
• Est. Priority Date: 09/05/1984
• Status: Expired due to Fees

• Current Assignee: The Hydrovane Compressor Company
• Original Assignee: The Hydrovane Compressor Company
• Inventors: Williams, Michael R.
• Primary Examiner(s): Vrablik, John J.
• Application Number:
  US06/772,886
• Time in Patent Office: 551 Days
• Field of Search: 418/84, 418/85, 418/87, 418/97-99, 418/DIG. 1, 184/6.16, 184/6.22, 184/104.1, 55/330, 55/332
• US Class Current: 418/84
• CPC Class Codes: F04C 29/0014 with control systems for the injection of the fluid
• CPC Class Codes: Y10S 418/01 Non-working fluid separation

Abstract

A rotary air compressor of oil sealed type includes a stator containing a rotor, oil injectors arranged to inject oil into the interior of the stator, an oil sump connected by a first oil pathway to the oil injectors and an oil cooler situated in the first oil pathway. A thermally responsive valve situated in the first oil pathway is arranged to open only when the temperature of the oil has reached a predetermined value whereby no oil is injected through the oil injectors before the temperature of the oil has reached the said predetermined value.

Claims

1. A rotary air compressor of oil sealed type including a stator, a rotor within said stator, oil injection means arranged, in use, to inject oil into the interior of said stator, an oil sump, a first oil pathway, connecting said sump to said oil injection means, an oil cooler situated in said first oil pathway and a thermally responsive valve situated in said first oil pathway, said thermally responsive valve being arranged to open only when the temperature of said oil has reached a predetermined value, whereby, in use, no oil is injected through said oil injection means before the temperature of said oil has reached said predetermined value, said compressor including an outer casing which accommodates said stator and defines said sump and which includes primary and secondary oil separation means for removing, in use, substantially all the entrained oil from the compressed air, said primary separation means including one or more surfaces against which said compressed air leaving said stator is constrained to impinge whereby a proportion of said entrained oil is caused to coalesce and then drip downwardly towards said sump, said secondary separation means including at least one coalescing element through which said compressed air is constrained to pass whereby substantially the remainder of said entrained oil is caused to coalesce, said compressor further including a secondary separation housing which accommodates said at least one coalescing element and is arranged below at least a part of said primary separation means and is so situated that at least a proportion of said oil coalesced by said primary separation means runs down over the outer surface of said secondary separation housing, said primary separation means including an annular primary separation chamber extending around said secondary separation housing;

said compressor further including an annular baffle plate extending around but not connected to said secondary separation housing, said annular baffle plate partially defining said primary separation chamber.

2. A compressor as claimed in claim 1 which is of eccentric rotor sliding vane type wherein said stator has two ends and two end plates closing said ends of said stator, said end plates defining respective apertures and carrying bearings within said apertures, said rotor being rotatably supported by said bearings, said compressor further including a second oil pathway extending from said sump to at least one of said bearings and the inner surfaces of said end plates, said second oil pathway being constructed and arranged to permit the flow of said oil therethrough substantially as soon as said compressor is started.

3. A compressor as claimed in claim 1 including a discharge pipe arranged to direct compressed air from said stator into said primary separation chamber and a further pipe arranged to direct compressed air to said secondary separation means, said further pipe having an open end on the side of said annular baffle plate which is remote from said primary separation chamber.

4. A compressor as claimed in claim 3 wherein said annular baffle plate defines one or more apertures which are circumferentially offset from said discharge pipe.