Claims
- 1. Apparatus, comprising:
- at least a first surface, of finite dimensions, including an entrance edge and an exit edge and characterized by an axis extending from said entrance edge to said exit edge;
- means for transporting a substrate over said surface at a distance, H, from said surface, from said entrance edge to said exit edge along a transport direction which is parallel to said axis, Characterized In That
- said apparatus further comprises a plurality of spaced-apart fluid jet injectors, each characterized by a diameter, D, and each capable of producing a fluid jet which impinges upon said substrate, said plurality of fluid jet injectors being arranged so that an imaginary line drawn along said surface in a direction which is parallel to said transport direction, which extends from said entrance edge to said exit edge, and which intersects the center of at least one fluid jet injector, intersects the same total number of fluid jet injector centers as any other such imaginary line drawn along said surface in a direction which is parallel to said transport direction, which extends from said entrance edge to said exit edge, and which intersects the center of at least one fluid jet injector, any two such adjacent imaginary lines being spaced apart by a distance S1, where S1/D is greater than 0 but less than or equal to about 10.
- 2. The apparatus of claim 1, wherein any two adjacent fluid jet injectors from among said plurality are separated by a distance S2, where S2/D is equal to or greater than about 2 but less than or equal to about 20.
- 3. The apparatus of claim 1, wherein S1/D is greater than 0 but less than or equal to about 1.3.
- 4. The apparatus of claim 2, wherein S2/D is equal to or greater than about 2 but less than or equal to about 12.
- 5. The apparatus of claim 1, wherein each of said fluid jets is characterized by a fluid speed, V, at said fluid jet injectors, and the fluid of said fluid jets is characterized by a kinematic viscosity, nu, and wherein a Reynolds number associated with each of said fluid jets, defined as the ratio V*D/nu, ranges from about 1000 to about 15,000.
- 6. The apparatus of claim 1, wherein the ratio H/D ranges from about 0.3 to about 12.
Parent Case Info
This is a divisional of copending application Ser. No. 08/206,308 filed on Mar. 4, 1994.
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Divisions (1)
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Number |
Date |
Country |
Parent |
206308 |
Mar 1994 |
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