Corrosion-resistant heated air data probe methods

US10024877B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10024877-B2
Application numberUS-201715681651-A
CountryUS
Kind codeB2
Filing dateAug 21, 2017
Priority dateApr 2, 2015
Publication dateJul 17, 2018
Grant dateJul 17, 2018

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  6. CPC / IPC classifications

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  7. Citations and related patents

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Abstract

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.

First claim

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.

Assignees

Inventors

Classifications

  • G01P5/165Primary

    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

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What does patent US10024877B2 cover?
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 …
Who is the assignee on this patent?
Rosemount Aerospace Inc
What technology area does this patent fall under?
Primary CPC classification G01P5/165. Mapped technology areas include Physics.
When was this patent published?
Publication date Tue Jul 17 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).