NACELLE INLET AND SYSTEM AND METHOD FOR MAKING SAME

• US 20200130856A1
• Filed: 10/24/2018
• Published: 04/30/2020
• Est. Priority Date: 10/24/2018
• Status: Abandoned Application

• Current Assignee: Spirit Aerosystems Incorporated (Spirit Aerosystems Holdings Incorporated)
• Original Assignee: Spirit Aerosystems Incorporated (Spirit Aerosystems Holdings Incorporated)
• Inventors: West, Randall Ray
• Application Number:
  US16/169,612
• Publication Number:
  US 20200130856A1
• Time in Patent Office: Days
• CPC Class Codes: B33Y 10/00 Processes of additive manufacturing
• CPC Class Codes: B33Y 30/00 Apparatus for additive manufacturing; Details thereof or accessories therefor
• CPC Class Codes: B33Y 70/10 Composites of different types of material, e.g. mixtures of ceramics and polymers or mixtures of metals and biomaterials
• CPC Class Codes: B33Y 80/00 Products made by additive manufacturing
• CPC Class Codes: B64D 2033/0206 comprising noise reduction means, e.g. acoustic liners
• CPC Class Codes: B64D 2033/0226 comprising boundary layer control means
• CPC Class Codes: B64D 2033/0286 for turbofan engines
• CPC Class Codes: B64D 29/00 Power-plant nacelles, fairings, or cowlings nacelles not otherwise provided for B64C
• CPC Class Codes: B64D 33/02 of combustion air intakes air intakes for gas-turbine plants or jet-propulsion plants per se F02C7/04; air intakes for combustion engines in general F02M35/00
• CPC Class Codes: F02C 7/04 Air intakes for gas-turbine plants or jet-propulsion plants
• CPC Class Codes: F02C 7/045 having provisions for noise suppression
• CPC Class Codes: F05D 2230/10 by removing material
• CPC Class Codes: F05D 2230/233 Electron beam welding
• CPC Class Codes: F05D 2230/234 Laser welding
• CPC Class Codes: F05D 2230/239 Inertia or friction welding
• CPC Class Codes: F05D 2230/31 Layer deposition
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft

Abstract

An inlet for a nacelle and an AM system and method for manufacturing the inlet having fewer discontinuities on the exterior surface to achieve a smoother flow over the inlet. The inlet includes an annular lip-cowl and a supporting framework. The AM system includes a support structure providing a form, and AM heads for depositing materials onto the form, with the materials subsequently hardening to become the lip-cowl. The support structure may have an upright or inverted orientation, is rotatable, and may be tiltable. Components may protrude from the form to be incorporated into the lip-cowl. The AM heads are mounted on moveable arms and are computer-controlled to deposit the material onto the form, and may be moveable along a radial axis to accommodate an asymmetrical portion of the form. The AM system may further include one or more machining heads for subtractively machining the deposited material.

Claims

1. A method of manufacturing a lip-cowl for an inlet of a nacelle, the lip-cowl including a lip portion and a cowl portion and having an interior surface and an exterior surface, the method comprising:

manufacturing a first portion of the lip-cowl using a first manufacturing technique;

positioning the first portion of the lip-cowl on a temporary support structure configured as a form; and

manufacturing a second portion of the lip-cowl using an additive manufacturing technique to deposit a material onto the form and over at least an area of the first portion of the lip-cowl positioned on the temporary support structure, wherein the material subsequently hardens so that the first and second portions of the lip-cowl are connected.

2. The method of claim 1, the first portion being the cowl portion and the second portion being the lip portion.

3. The method of claim 2, the first manufacturing technique being a spin-forming technique or a stretch-forming technique.

4. The method of claim 1, the first portion including a scarf at an interface between the first portion and the second portion so that the connection between the first and second portions includes a scarf joint.

5. The method of claim 1, the first portion including a connection structure at an interface between the first portion and the second portion so that the connection between the first and second portions includes the connection structure.

6. The method of claim 1, the first portion being manufactured from a different material than the second portion.

7. The method of claim 1, the temporary support structure having an upright orientation with the lip portion located above the cowl portion.

8. The method of claim 1, the temporary support structure having an inverted orientation with the lip portion located below the cowl portion.

9. The method of claim 1, the temporary support structure being rotatable about a vertical axis, and the method further including rotating the temporary support structure about the vertical axis as an additive manufacturing head deposits the material onto the form to manufacture the second portion.

10. The method of claim 1, the temporary support structure being tiltable about a horizontal axis, and the method further including tilting the temporary support structure about the horizontal axis as the additive manufacturing head deposits the material onto the form to manufacture the second portion.

11. The method of claim 1, further including—

manufacturing a third portion of the lip-cowl;

positioning the third portion of the lip-cowl on the form; and

manufacturing the second portion of the lip-cowl using the additive manufacturing technique to deposit the material onto the form and over at least an area of the third portion of the lip-cowl positioned on the form, wherein the material subsequently hardens so that the first and third portions of the lip-cowl are connected.

12. The method of claim 11, the third portion of the lip-cowl being one or more stiffener elements.

13. The method of claim 11, the third portion of the lip-cowl being one or more connection elements positioned at an interface between the first and second portions of the lip-cowl.

14. The method of claim 1, further including machining an area of the material deposited onto the form by the additive manufacturing head.

15. A method of manufacturing an annular lip-cowl for an inlet of a nacelle, the annular lip-cowl including a lip portion and a cowl portion and having an interior surface and an exterior surface, and the annular lip-cowl having no protruding fastener heads and no annularly-extending joints on the exterior surface, the method comprising:

manufacturing a first portion of the annular lip-cowl using a first manufacturing technique;

positioning the first portion of the annular lip-cowl on a temporary support structure configured as a form; and

manufacturing a second portion of the annular lip-cowl using an additive manufacturing technique in which the temporary support structure is rotated about a vertical axis while one or more additive manufacturing head deposits a material onto the form and over at least an area of the first portion of the annular lip-cowl positioned on the temporary support structure, wherein the material subsequently hardens so that the first and second portions of the annular lip-cowl are connected.

16. The method of claim 15, the first portion being manufactured from a different material than the second portion.

17. The method of claim 15, further including—

manufacturing a third portion of the annular lip-cowl;

positioning the third portion of the annular lip-cowl on the form; and

manufacturing the second portion of the annular lip-cowl using the additive manufacturing technique to deposit the material onto the form and over at least an area of the third portion of the annular lip-cowl positioned on the form, wherein the material subsequently hardens so that the first and third portions of the annular lip-cowl are connected.

18. A method of manufacturing an inlet of a nacelle, the method comprising:

manufacturing an annular lip-cowl including a lip portion and a cowl portion and having an interior surface and an exterior surface, and the annular lip-cowl having no protruding fastener heads and no annularly-extending joints on the exterior surface, by—

manufacturing a first portion of the annular lip-cowl using a first manufacturing technique,

positioning the first portion of the annular lip-cowl on a temporary support structure configured as a form, and

manufacturing a second portion of the annular lip-cowl using an additive manufacturing technique in which the temporary support structure is rotated about a vertical axis while one or more additive manufacturing head deposits a material onto the form and over at least an area of the first portion of the annular lip-cowl positioned on the temporary support structure, wherein the material subsequently hardens so that the first and second portions of the annular lip-cowl are connected;

manufacturing a framework configured to physically support the annular lip-cowl; and

attaching the framework to the interior surface of the annular lip-cowl.

19. The method of claim 18, the first portion being manufactured from a different material than the second portion.

20. The method of claim 18, further including—

manufacturing a third portion of the annular lip-cowl;

positioning the third portion of the annular lip-cowl on the form; and

manufacturing the second portion of the annular lip-cowl using the additive manufacturing technique to deposit the material onto the form and over at least an area of the third portion of the annular lip-cowl positioned on the form, wherein the material subsequently hardens so that the first and third portions of the annular lip-cowl are connected.