MULTI-PORT SANDBLASTING MANIFOLD AND METHOD

• US 20060199477A1
• Filed: 05/05/2006
• Published: 09/07/2006
• Est. Priority Date: 03/10/2004
• Status: Active Grant

• Current Assignee: Mark F. Gabriel, Robert C. Larsen
• Original Assignee: Mark F. Gabriel, Robert C. Larsen
• Inventors: Gabriel, Mark F., Larsen, Robert C.
• Granted Patent: US 7,125,317 B2
• Time in Patent Office: Days
• US Class Current: 451/38
• CPC Class Codes: B24C 7/0046 the abrasive material being fed in a gaseous carrier
• CPC Class Codes: B24C 9/00 Appurtenances of abrasive blasting machines or devices, e.g. working chambers, arrangements for handling used abrasive material

Abstract

A method and apparatus is provided to simplify sandblasting processes while increasing applied coverage areas in sandblasting operations. The method and apparatus provide a manifold assembly having a plurality of nozzles and that is rigidly attached to an air supply. The manifold is supplied with abrasive material via a plurality of angularly attached sand supply hoses which are coupled to an abrasive material supply. The manifold assembly is pressurized with the supply of air. An article is sandblasted by drawing sand through the hoses and out of the plurality of nozzles using the pressurized air through the manifold assembly.

Claims

1. A method comprising:

attaching an air supply to a longitudinal passage in a manifold assembly, the manifold assembly comprising a plurality of outlet passages and a plurality of material passages, the plurality of outlet passages being serially connected to the longitudinal passage, wherein each of the plurality of outlet passages are oriented in a different direction relative to a remainder of the outlet passages;

providing a supply of abrasive material;

attaching a respective first end of a plurality of material supply hoses to a corresponding plurality of material passages, each material passage of the plurality of material passages being in fluid connection with a corresponding outlet passage of the plurality of outlet passages, wherein each material passage intersects the corresponding outlet passage at an angle to generate a venturi effect;

coupling the material supply hoses to the abrasive material supply at a respective second ends of the material supply hoses;

pressurizing the manifold assembly with the supply of air; and

sandblasting an article by drawing abrasive material through the hoses and out of the plurality of nozzles using the pressurized air.

2. The method of claim 1, further comprising rigidly attaching a plurality of manifold assemblies to the same air supply.

3. The method of claim 1, wherein the manifold assembly further comprises a chambered block and a plenum cap.

4. The method of claim 3, further comprising rigidly attaching the air supply to an end of the plenum cap.

5. The method of claim 3, further comprising rigidly attaching the air supply to a top surface of the plenum cap.

6. The method of claim 3, further comprising:

pressuring the supply of air in the plenum cap.

7. A method of abrading a surface of an aircraft component, the method comprising:

attaching an air supply to a manifold assembly, the manifold assembly comprising a plurality of outlet passages, wherein each of the plurality of outlet passages are oriented in a different direction relative to a remainder of the outlet passages;

providing a supply of abrasive material; and

attaching a respective first end of a plurality of material supply hoses to a corresponding plurality of material passages, each material passage of the plurality of material passages being in fluid connection with a corresponding outlet passage of the plurality of outlet passages.

8. The method of claim 7, further comprising:

pressurizing a longitudinal passage of the manifold in response to attaching the air supply to the manifold, the longitudinal passage being serially connected to the plurality of outlet passages.

9. The method of claim 8, further comprising:

generating a venturi at the intersection of each material passage and corresponding outlet passage.

10. The method of claim 9, further comprising:

sandblasting the aircraft component by drawing the abrasive material through the material supply hoses in response to generating the venturi and expelling the abrasive material out of the plurality of nozzles in response to the pressurized longitudinal passage.

11. A system for blasting abrasive material onto an article comprising:

a compressed air supply;

a supply of abrasive material;

a manifold assembly comprising;

a longitudinal passage;

a plurality of outlet passages serially connected to the longitudinal passage, wherein each of the plurality of outlet passages are oriented in a different direction relative to a remainder of the outlet passages; and

a plurality of material passages, each material passage of the plurality of material passages being in fluid connection with a corresponding outlet passage of the plurality of outlet passages, wherein each material passage intersects the corresponding outlet passage at an angle to generate a venturi effect;

an air supply line coupled to the compressed air supply and further connected to the longitudinal passage;

a plurality of sand supply hoses, each sand supply hose being connected to a respective one of the plurality of material passages and further coupled to the supply of abrasive material; and

a plurality of nozzles, each nozzle being connected to a respective one of the plurality of outlet passages to direct the abrasive material from said manifold assembly towards the article.

12. The system of claim 11, wherein the manifold assembly further comprises:

a chambered block; and

a plenum cap attached to the chambered block.

13. The system of claim 11, wherein the manifold assembly further comprises:

an air inlet port that receives the air supply line;

a plurality of cross chambers intersecting the air inlet port wherein each respective cross chamber comprises a material outlet attachment port at one end and is closed off at another end; and

a plurality of material inlet attachment ports each angularly intersecting a respective cross chamber.

14. The apparatus of claim 11, wherein the air supply line is rigidly connected to the manifold assembly.

15. The apparatus of claim 13, further comprising:

a plurality of sand supply hoses each connected to a respective one of the plurality of material inlet attachment ports.