US4612737A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Grit blast drilling of advanced composite perforated sheet
Assignee: Rohr Inc
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Filing: 1985-07-05
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Granted: 1986-09-23
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Expires: 2005-07-05
Abstract
Abstract A method and resulting product produced by attaching a prepared maskant of a desired perforation pattern to cured compound contoured or flat advanced composite materials, directing a narrow stream of highly abrasive grit material of a selected particle size range through a relatively large nozzle under selected high pressure toward the maskant perforations at a very small angle relative to the perforation walls until perforations are formed in the advanced composite material according to the stencil perforation pattern. The perforated sheet produced is particularly adapted for use in sound attenuation structures.
Inventors
- 👤 James M. Adee
- 👤 John A. Frye
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 09:10
CPC Classifications
B; B24; B24C; B24C1/00; B24C1/04; G; G10; G10K; G10K11/00; G10K11/16; G10K11/172
Claims Analysis
Total Claims: 11
Claim 1
Independent Claim
190 words
A method of forming perforations in contoured resin matrix fiber reinforced advanced composite materials for use in sound attenuation structures for aircraft surfaces, comprising the steps of: providing a sheet of imperforate contoured resin matrix fiber reinforced advanced composite material for use in sound attenuation structures for aircraft surfaces; forming a mask having an aperture pattern thereon, the apertures having a diameter in the range of from about 0.010" to about 0.250"; positioning said mask to follow the contour of a surface of said sheet and then releasably adhering said mask to said surface of said sheet; providing a grit having the capability of blasting through said sheet while retaining said mask on said sheet, said grit having a particle grit number range of from about 60 to about 240 grit; blasting said grit against said mask at a pressure in the range of from about 70 to 100 pounds per square inch at an angle of from 0 degrees to about 8 degrees relative to the walls of the apertures in said mask to form apertures in said sheet at the locations of said apertures; and removing said mask.
Claim 2
Independent Claim
190 words
A method of forming perforations in contoured resin matrix fiber reinforced advanced composite materials for use in sound attenuation structures for aircraft surfaces, comprising the steps of: providing a sheet of imperforate contoured resin matrix fiber reinforced advanced composite material for use in sound attenuation structures for aircraft surfaces; forming a mask having an aperture pattern thereon, the apertures having a diameter in the range of from about 0.010" to about 0.250"; positioning said mask to follow the contour of a surface of said sheet and then releasably adhering said mask to said surface of said sheet; providing a grit having the capability of blasting through said sheet while retaining said mask on said sheet, said grit having a particle grit number range of from about 60 to about 240 grit; blasting said grit against said mask at a pressure in the range of from about 70 to 100 pounds per square inch at an angle of from 0 degrees to about 8 degrees relative to the walls of the apertures in said mask to form apertures in said sheet at the locations of said apertures; and removing said mask.
Claim 3
Dependent Claim
14 words
The method of claim 1 wherein the aperture pattern is a predetermined aperture pattern.
Claim 4
Dependent Claim
22 words
The method of claim 1 wherein the apertures typically provide a per cent open area ranging in value from 4 to 34.
Claim 5
Dependent Claim
15 words
The method as defined in claim 1 wherein said mask is formed of polyurethane material.
Claim 6
Dependent Claim
16 words
The method as defined in claim 1 wherein said mask is adhered to said composite material.
Claim 7
Dependent Claim
20 words
The invention as defined in claim 1 wherein said mask is formed of a vinyl material or rubber base material.
Claim 8
Dependent Claim
20 words
The invention as defined in claim 1 wherein the perforated structure has a thickness of from 0.005 to 0.250 inchess.
Claim 9
Dependent Claim
25 words
The invention as defined in claim 1 wherein said grit material is aluminum oxide, silicon carbide or the like having dense, hard, sharp, abrasive grains.
Claim 10
Dependent Claim
11 words
A perforated structure manufactured according to the method of claim 1.
Claim 11
Dependent Claim
28 words
The method as defined in claim 1 wherein the grit blasting is performed with either a suction nozzle blasting system or a non-suction nozzle pressure blasting machine system.
References Cited (Backward Citations)
US2358710A
Cited
JPS5367977A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1989-09-22 | 1990-03-24 | 1990-09-23 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1993-09-22 | 1994-03-24 | 1994-09-23 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1997-09-22 | 1998-03-24 | 1998-09-23 | $7700.00 | Window Closed / Lapsed |