Corrision-resistant heated air data probe
US-2016291051-A1 · Oct 6, 2016 · US
US10024877B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10024877-B2 |
| Application number | US-201715681651-A |
| Country | US |
| Kind code | B2 |
| Filing date | Aug 21, 2017 |
| Priority date | Apr 2, 2015 |
| Publication date | Jul 17, 2018 |
| Grant date | Jul 17, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A method of making an air data probe may comprise forming a probe body, forming an interior cavity into the probe body, applying a protective shell to the probe body by an additive manufacturing technique, inserting a heating element into the interior cavity, machining a final profile of the air data probe, and forming a sensing port comprising a port passage defined through the probe body and lined by a portion of the protective shell.
Opening claim text (preview).
The invention claimed is: 1. A method of making an air data probe comprising: forming a probe body; forming an interior cavity into the probe body; applying a protective shell to the probe body by an additive manufacturing technique; inserting a heating element into the interior cavity; machining a final profile of the air data probe; and forming a sensing port comprising a port passage defined through the probe body and lined by a portion of the protective shell. 2. The method according to claim 1 , wherein forming the sensing port further comprises: forming a sensing port recess comprising an indentation formed in the probe body; and applying the portion of the protective shell disposed over the sensing port recess and forming a substantially continuous surface over the indentation, wherein the port passage comprises an aperture defined by the portion of the protective shell and in fluidic communication with an environment and the interior cavity. 3. The method according to claim 2 , wherein the port passage is aligned coincident with a geometric center of the sensing port recess.
Arrangements or constructions of Pitot tubes · CPC title
indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw · CPC title
for speed measuring devices, e.g. pulse generator · CPC title
Housings for sensors · CPC title
Pitot tubes · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.