US4537647A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Method for applying turbulators to wind tunnel models
Assignee: Boeing Co
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Filing: 1982-10-06
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Granted: 1985-08-27
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Expires: 2002-10-06
Abstract
Abstract A method for forming turbulators on scale model airplanes used in wind tunnel testing for accurately simulating a transition point on the model surface equivalent to that produced on the full scale airplane. The transition point is where the boundary layer airflow goes from a laminar airflow condition to a turbulent airflow condition. The method relates to applying a perforated tape mask (14) to the model surface (12) at a predetermined location and filling the perforations (15) with a fast cure epoxy (17). After the epoxy has cure hardened, the tape mask (14) is peeled off in the direction of the arrow (16), leaving a series of in situ formed disk turbulators (10) which function to produce the transition point on the model surface.
Inventors
- 👤 Clark B. Foster
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-09 16:44
CPC Classifications
B; B05; B05D; B05D1/00; B05D1/32; B29; B29C; B29C67/00; B29C67/08; G; G01; G01M; G01M9/00; G01M9/06; G09; G09B; G09B23/00; G09B23/06; G09B23/08; G09B23/12; B29K; B29K2063/00; B29L; B29L2031/00; B29L2031/30; B29L2031/3076; B29L2031/40
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
134 words
A method for forming turbulators in situ on the surface of a scale model airfoil used in wind tunnel testing, comprising the steps of: forming a mold by applying an adhesive backed tape stencil having a series of circular apertures, to a predetermined location on said airfoil; filling the apertures in said tape stencil with an epoxy resin; leveling the epoxy resin with the surface of said tape stencil; cure hardening said epoxy resin; removing said tape stencil from said airfoil and leaving in situ formed epoxy disk turbulators on said airfoil; predetermining a thickness of said tape stencil for substantially producing a height of the epoxy disk turbulators which protrudes into free airstream flow in the wind tunnel during testing of said scale model airfoil for producing a transition point on said airfoil.
Claim 2
Independent Claim
134 words
A method for forming turbulators in situ on the surface of a scale model airfoil used in wind tunnel testing, comprising the steps of: forming a mold by applying an adhesive backed tape stencil having a series of circular apertures, to a predetermined location on said airfoil; filling the apertures in said tape stencil with an epoxy resin; leveling the epoxy resin with the surface of said tape stencil; cure hardening said epoxy resin; removing said tape stencil from said airfoil and leaving in situ formed epoxy disk turbulators on said airfoil; predetermining a thickness of said tape stencil for substantially producing a height of the epoxy disk turbulators which protrudes into free airstream flow in the wind tunnel during testing of said scale model airfoil for producing a transition point on said airfoil.
Claim 3
Dependent Claim
36 words
The method set forth in claim 1, including: spacing the series of circular apertures in said tape stencil such that the distance between them is within the range of from approximately one diameter to two diameters.
Claim 4
Dependent Claim
81 words
In a method for forming turbulators as recited in claim 1, including: applying a release agent line on the surface of said scale model airfoil prior to the application of said tape stencil; and positioning the series of circular apertures of said tape stencil over said release agent line which functions to decrease the bond area between the in situ formed epoxy disk turbulators and the model surface, thereby making said turbulators more easily removable without damage to the model surface.
Claim 5
Independent Claim
162 words
A method for forming turbulators on an aerodynamic scale model used in wind tunnel testing to simulate a transition point of laminar to turbulent airflow occurring on a full scale aerodynamic craft, comprising the steps of: forming a mold by applying a tape mask having a series of circular perforations, to a predetermined location on said model; filling the series of circular perforations in said tape mask with a cure hardening epoxy resin liquid; removing excess epoxy resin to precisely limit epoxy filled perforations to a surface level of said tape mask; cure hardening said epoxy resin; peeling off said tape mask after the epoxy resin has cure hardened and leaving a series of in situ formed epoxy disk turbulators on said model; predetermining a thickness of said tape mask for substantially producing a height of epoxy disk turbulators which protrude into free airstream flow and function to produce a transition point on the surface of said model during wind testing thereof.
Claim 6
Independent Claim
162 words
A method for forming turbulators on an aerodynamic scale model used in wind tunnel testing to simulate a transition point of laminar to turbulent airflow occurring on a full scale aerodynamic craft, comprising the steps of: forming a mold by applying a tape mask having a series of circular perforations, to a predetermined location on said model; filling the series of circular perforations in said tape mask with a cure hardening epoxy resin liquid; removing excess epoxy resin to precisely limit epoxy filled perforations to a surface level of said tape mask; cure hardening said epoxy resin; peeling off said tape mask after the epoxy resin has cure hardened and leaving a series of in situ formed epoxy disk turbulators on said model; predetermining a thickness of said tape mask for substantially producing a height of epoxy disk turbulators which protrude into free airstream flow and function to produce a transition point on the surface of said model during wind testing thereof.
Claim 7
Dependent Claim
36 words
The method set forth in claim 4, including: spacing the series of circular perforations in said tape mask such that the distance between them is within the range of from approximately one diameter to two diameters.
Claim 8
Dependent Claim
80 words
In a method for forming turbulators as recited in claim 4, including: applying a release agent line on the surface of said scale model prior to the application of said tape mask; and positioning the series of circular perforations of said tape mask over said release agent line which functions to decrease the bond area between the in situ formed epoxy disk turbulators and the model surface, thereby making said turbulators more easily removable without damage to the model surface.
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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) | 1988-08-26 | 1989-02-25 | 1989-08-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-08-26 | 1993-02-25 | 1993-08-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-08-26 | 1997-02-25 | 1997-08-27 | $7700.00 | Window Closed / Lapsed |