US5070729A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Multi-colored layers for visualizing aerodynamic flow effects
Assignee: National Aeronautics and Space Administration
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Filing: 1990-12-03
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Granted: 1991-12-10
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Expires: 2010-12-03
Abstract
Abstract A method is provided for visualizing aerodynamic flow effects on a test surface. First, discrete quantities of a sublimating chemical such as naphthalene are distinctively colored via appropriate dyes or paints. Next, a uniform layer of the sublimating chemical having a particular color is applied to the test surface. This layer is covered with a second uniform layer of a different colored sublimating chemical, and so on until a composite of multi-colored layers is formed having a discrete thickness. Friction caused by an airflow results in the distinctly colored layers being removed in proportion to such aerodynamic flow characteristics as velocity and temperature, resulting in a multi-colored portrait which approximates the airflow on the underlying test surface.
Inventors
- 👤 Ronald N. Jensen
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 22:11
CPC Classifications
G; G01; G01P; G01P13/00; G01P13/0093; G01M; G01M9/00; G01M9/06; G01M9/065; G01M9/067; G01P5/00
Claims Analysis
Total Claims: 9
Claim 1
Independent Claim
100 words
A method for visualizing aerodynamic flow effects on a test surface, comprising the steps of: coloring discrete quantities of a sublimating chemical different colors; applying a first uniform colored layer of the sublimating chemical to the test surface; applying a second, different colored uniform layer of the sublimating chemical to the first applied layer to form a composite of layers of different colored sublimated chemicals; and subjecting the test surface and composite to an airflow, whereby the layers of the composite are removed by the airflow to create a portrait of the aerodynamic flow effects on the underlying test surface.
Claim 2
Independent Claim
100 words
A method for visualizing aerodynamic flow effects on a test surface, comprising the steps of: coloring discrete quantities of a sublimating chemical different colors; applying a first uniform colored layer of the sublimating chemical to the test surface; applying a second, different colored uniform layer of the sublimating chemical to the first applied layer to form a composite of layers of different colored sublimated chemicals; and subjecting the test surface and composite to an airflow, whereby the layers of the composite are removed by the airflow to create a portrait of the aerodynamic flow effects on the underlying test surface.
Claim 3
Dependent Claim
40 words
The visualization method according to claim 1, futher comprising applying additional different colored uniform layers of sublimating chemical to said second layer of colored sublimated chemical to form a composite of more than two different colored layers of sublimated material.
Claim 4
Dependent Claim
25 words
The visualization method according to claim 2, wherein said coloring step comprises mixing discrete quantities of the sublimating chemical with oil-based paints of different colors.
Claim 5
Dependent Claim
15 words
The visualization method according to claim 2, wherein each layer is of the same thickness.
Claim 6
Dependent Claim
13 words
The visualization method according to claim 1, wherein the sublimating chemical is naphthalene.
Claim 7
Dependent Claim
25 words
The visualized methods according to claim 5, wherein said coloring step comprises mixing discrete quantities of the sublimating chemical with oil-based paints of different colors.
Claim 8
Dependent Claim
25 words
The visualization method according to claim 1, wherein said coloring step comprises mixing discrete quantities of the sublimating chemical with oil-based paints of different colors.
Claim 9
Dependent Claim
15 words
The visualization method according to claim 1, wherein each layer is of the same thickness.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1994-12-09 | 1995-06-10 | 1995-12-10 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1998-12-09 | 1999-06-10 | 1999-12-10 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2002-12-09 | 2003-06-10 | 2003-12-10 | $7700.00 | Window Closed / Lapsed |