Integral instrumentation in additively manufactured components of gas turbine engines
US-2016348531-A1 · Dec 1, 2016 · US
US10921344B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10921344-B2 |
| Application number | US-201916295240-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 7, 2019 |
| Priority date | Mar 7, 2019 |
| Publication date | Feb 16, 2021 |
| Grant date | Feb 16, 2021 |
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In one embodiment, a probe includes a first facet associated with a first pressure port operable to measure a first wind pressure, a second facet associated with a second pressure port operable to measure a second wind pressure, and a third facet associated with a third pressure port operable to measure a third wind pressure. The second facet is adjacent to the first facet and the third facet adjacent to the second facet. The probe further includes a fourth facet adjacent to the third facet and a fifth facet adjacent to the fourth facet and to the first facet. The first facet, the second facet, the third facet, the fourth facet, and the fifth facet are located between a first end portion and a second end portion of the probe.
Opening claim text (preview).
What is claimed is: 1. A probe, comprising: a first facet associated with a first pressure port operable to measure a first wind pressure; a second facet adjacent to the first facet, the second facet associated with a second pressure port operable to measure a second wind pressure; a third facet adjacent to the second facet, the third facet associated with a third pressure port operable to measure a third wind pressure; a fourth facet adjacent to the third facet; and a fifth facet adjacent to the fourth facet and to the first facet; wherein: the first facet, the second facet, the third facet, the fourth facet, and the fifth facet are located between a first end portion and a second end portion of the probe; the probe is coupled to a vehicle; and a surface of each of the first facet, the second facet, and the third facet of the probe face away from a longitudinal centerline of the vehicle and a surface of each of the fourth facet and the fifth facet face toward the longitudinal centerline of the vehicle. 2. The probe of claim 1 , wherein: the first end portion comprises a fourth pressure port operable to measure a fourth wind pressure; and the fourth wind pressure is a reference pressure. 3. The probe of claim 1 , wherein the first facet, the second facet, the third facet, the fourth facet, and a fifth facet are flat surfaces. 4. The probe of claim 1 , wherein: the first end portion is a cone-shaped tip comprising a first end; the second end portion is a cylindrical base comprising a second end; and a maximum length from the first end to the second end is eight inches. 5. The probe of claim 1 , wherein the first pressure port, the second pressure port, and the third pressure port are located the same distance from the first end portion. 6. The probe of claim 1 , wherein the probe is a solid object comprising at least one of the following materials: aluminum; steel; and plastic. 7. A method, comprising: measuring a first wind pressure using a first pressure port associated with a first facet of a probe; measuring a second wind pressure using a second pressure port associated with a second facet of the probe; measuring a third wind pressure using a third pressure port associated with a third facet of the probe, wherein: the second facet is adjacent to the first facet; the third facet is adjacent to the second facet and a fourth facet; the fourth facet is adjacent to a fifth facet; the fifth facet is adjacent to the first facet; the first facet, the second facet, the third facet, the fourth facet, and the fifth facet are located between a first end portion and a second end portion of the probe; the probe is coupled to a vehicle; and a surface of each of the first facet, the second facet, and the third facet of the probe face away from a longitudinal centerline of the vehicle and a surface of each of the fourth facet and the fifth facet face toward the longitudinal centerline of the vehicle. 8. The method of claim 7 , further comprising measuring a fourth wind pressure using a fourth pressure port, wherein: the first end portion comprises the fourth pressure port; and the fourth wind pressure is a reference pressure. 9. The method of claim 7 , wherein the first facet, the second facet, the third facet, the fourth facet, and a fifth facet are flat surfaces. 10. The method of claim 7 , wherein: the first end portion is a cone-shaped tip comprising a first end; the second end portion is a cylindrical base comprising a second end; and a maximum length from the first end to the second end is eight inches. 11. The method of claim 7 , wherein the first pressure port, the second pressure port, and the third pressure port are located the same distance from the first end portion. 12. The method of claim 7 , wherein the probe is a solid object comprising at least one of the following materials: aluminum; steel; and plastic. 13. One or more computer-readable storage media embodying instructions that, when executed by a processor, cause the processor to perform operations comprising: measuring a first wind pressure using a first pressure port associated with a first facet of a probe; measuring a second wind pressure using a second pressure port associated with a second facet of the probe; measuring a third wind pressure using a third pressure port associated with a third facet of the probe, wherein: the second facet is adjacent to the first facet; the third facet is adjacent to the second facet and a fourth facet; the fourth facet is adjacent to a fifth facet; the fifth facet is adjacent to the first facet; the first facet, the second facet, the third facet, the fourth facet, and the fifth facet are located between a first end portion and a second end portion of the probe; the probe is coupled to a vehicle; and a surface of each of the first facet, the second facet, and the third facet of the probe face away from a longitudinal centerline of the vehicle and a surface of each of the fourth facet and the fifth facet face toward the longitudinal centerline of the vehicle. 14. The one or more computer-readable storage media of claim 13 , the operations further comprising measuring a fourth wind pressure using a fourth pressure port, wherein: the first end portion comprises the fourth pressure port; and the fourth wind pressure is a reference pressure. 15. The one or more computer-readable storage media of claim 13 , wherein the first facet, the second facet, the third facet, the fourth facet, and a fifth facet are flat surfaces. 16. The one or more computer-readable storage media of claim 13 , wherein: the first end portion is a cone-shaped tip comprising a first end; the second end portion is a cylindrical base comprising a second end; and a maximum length from the first end to the second end is eight inches. 17. The one or more computer-readable storage media of claim 13 , wherein the first pressure port, the second pressure port, and the third pressure port are located the same distance from the first end portion.
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by use of non-mechanical means, e.g. acoustic or electromagnetic devices · CPC title
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