Seal grid assembly for rotary piston mechanism
AssigneeCurtiss-Wright Corporation
InventorMurray Berkowitz
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AssigneeCurtiss-Wright Corporation
InventorMurray Berkowitz
Estimating the term…
The improved seal grid assembly is for a rotary compressor or expansion engine of the type having a rotor supported for planetation in a multi-lobe housing cavity and comprises, in combination with a non-rotating seal at the juncture of the housing lobes, a sealing means including a sealing surface movable between a retracted position where it is out of engagement with the peripheral wall and an extended position where it is in engagement with the peripheral wall of the housing cavity. A vent passage means is also provided in the rotor to communicate a space defined between the sealing means and rotor with the working chambers to conduct gaseous fluid which pressurizes said space so as to provide movement of the sealing surface of the associated seal means to the retracted position just prior to engagement with the non-rotating seal and to the extended position after such engagement with the non-rotating seals at each of the housing lobe junctures.
An improved seal grid assembly for rotary piston mechanisms, having a housing with axially spaced end walls and a peripheral wall interconnecting the end walls to form a multi-lobed cavity therebetween and having a rotor mounted within said cavity for rotation on an axis eccentric to the housing cavity axis, the rotor having opposite end faces adjacent the housing end walls and a plurality of flank surfaces converging with each other to form a plurality of circumferentially spaced apex portions so that the rotor defines with the housing walls a plurality of working chambers which vary in volumetric size and gaseous fluid pressure as the rotor rotates within the housing cavity, the improved seal grid assembly comprises, in combination with a seal blade means at each of the junctures of the housing cavity lobes;
A seal means for each of the apex portions of a rotor for a rotary compressor or expansion engine having a housing with axially spaced end walls and a peripheral wall interconnecting the end walls to form a multi-lobed cavity therebetween and with the rotor mounted within said cavity for rotation on an axis eccentric to the housing cavity axis, the rotor having opposite side faces adjacent the housing end walls and a plurality of flank surfaces converging with each other to form a plurality of circumferentially-spaced apex portions so that the rotor defines with the housing walls a plurality of working chambers which successively expand and contract in volumetric size and increase and decrease in gaseous fluid pressure as the rotor rotates relative to the housing cavity, the seal means comprising:
Dependencies are inferred from the claim text.