Claims
- 1. A method of manufacturing a multiple-ply tissue having an unexpectedly low loose dust and lint count by removing dust and lint from both outwardly facing surfaces of a multiple-ply tissue web while the web is traveling with its accompanying boundary layers of air in a predetermined plane and direction in a tissue rewinding machine, comprising the steps of:a) directing scrubber gas in a transversely elongated jet from a slit defining a Coanda nozzle so that the jet forms a thin, non-turbulent layer of rapidly moving gas which moves in a direction opposite to web travel and scrubs the boundary layer of air and entrained dust and lint, as well as dust and lint embedded in one surface of the web, away from the one surface of said web; b) directing said scrubber gas with the air and lint and dust which it has removed from said one surface of said web to follow a Coanda nozzle airfoil surface adjacent said slit until it reaches and is drawn into an exhaust plenum; c) simultaneously directing another transversely elongated jet of scrubber gas from another slit defining a second Coanda nozzle so that it forms a thin, non-turbulent layer of rapidly moving gas which moves in a direction opposite to web travel and scrubs the boundary layer of air and entrained dust and lint as well as dust and lint embedded in the other surface of said web, away from the other surface of said web; and d) directing said scrubber gas with the air and lint and dust which it has removed from said other surface of said web to follow a second Coanda nozzle airfoil surface adjacent said another slit until it reaches and is drawn into an exhaust plenum.
- 2. The method of claim 1 further characterized by and including the step of:a) creating the jets of scrubber gas by maintaining a gas pressure from 20 inches H2O to 80 inches H2O in a plenum from which the gas departs through each slit.
- 3. A method of manufacturing a multiple-ply tissue having an unexpectedly low loose dust and lint count by removing dust and lint from both outwardly facing surfaces of a multiple-ply tissue web while the web is traveling with its accompanying boundary layers of air in a predetermined plane and direction in a tissue rewinding machine, comprising the steps of:a) under a pressure of at least 20 inches H2O, directing scrubber gas in a transversely elongated jet from a slit defining a Coanda nozzle having a width of between 0.002 and 0.015 inches so that the jet forms a thin, non-turbulent layer of rapidly moving gas which moves in a direction opposite to web travel and scrubs the boundary layer of air and entrained dust and lint, as well as dust and lint embedded in the surface of the web, away from one surface of said web; b) directing said scrubber gas with the air and lint and dust which it has removed from said one surface of said web to follow a Coanda nozzle airfoil surface adjacent said slit until it reaches and is drawn into an exhaust plenum; c) simultaneously directing another transversely elongated jet of scrubber gas from another slit defining a second Coanda nozzle having a width of between 0.002 and 0.015 inches so that it forms a thin, non-turbulent layer of rapidly moving gas which moves in a direction opposite to web travel and scrubs the boundary layer of air and entrained dust and lint, as well as dust and lint embedded in the surface of said web, away from the other surface of said web; and d) directing said scrubber gas with the air and lint and dust which it has removed from said other surface of said web to follow a second Coanda nozzle airfoil surface adjacent said another slit until it reaches and is drawn into an exhaust plenum.
- 4. The method of claim 3 further characterized by and including the step of:a) creating the jets of scrubber gas by maintaining a gas pressure from 20 inches H2O to 80 inches H2O in a plenum from which the gas departs through each slit.
- 5. The method of claim 4 further characterized in that:a) said gas pressure is at least 50 inches H2O.
- 6. The method of claim 5 further characterized in that:a) each of said Coanda nozzle slits has a width of about 0.012 inches.
- 7. The method of claims 1 or 3 including the additional step of:a) stabilizing the web before it reaches each of said Coanda nozzle airfoil surfaces by passing it over two additional airfoil surfaces each of which corresponds to one of the two Coanda nozzle airfoil surfaces.
- 8. The method of claim 7 wherein:a) each of said additional two airfoil surfaces is disposed in a plane further from the web than its corresponding Coanda nozzle airfoil surface.
- 9. The method of claims 1 or 3 including the additional step of:a) drawing more air into each exhaust plenums than is supplied by the corresponding Coanda nozzle.
- 10. The method of claim 9 further including the step of:a) controlling the amount of air drawn into each exhaust plenum by adjusting the position of an exhaust damper over which air is drawn into each exhaust plenum.
- 11. The method of claims 1 or 3 wherein:a) each exhaust plenum is approximately frusto-conical in shape so as to be tapered from one end to an opposite end; and b) each exhaust plenum has a tangentially disposed opening so that air being drawn into it is swirled within the plenum.
RELATED APPLICATION
This application is a division of U.S. application Ser. No. 09/102,314, filed Jun. 22, 1998, and now U.S. Pat. No. 5,991,964.
US Referenced Citations (27)