Method for additive manufacturing nacelle inlet lipskins

Patent metadata

Field	Value
Publication number	US-10507548-B2
Application number	US-201715720098-A
Country	US
Kind code	B2
Filing date	Sep 29, 2017
Priority date	Sep 29, 2017
Publication date	Dec 17, 2019
Grant date	Dec 17, 2019

Abstract

An apparatus for fabricating a part, comprising a curved shaft; a build plate connected to the curved shaft; a motor; and a transmission connecting the motor and the curved shaft. The build plate moves along a curved path having a radius of curvature originating on an axis when the transmission transfers power from the motor to the curved shaft. Material deposited on the build plate along the curved path forms the part comprising a solid of revolution around the axis. In one or more examples, the part is an aircraft engine inlet.

First claim

What is claimed is:

1. An additive manufacturing apparatus for fabricating a part, comprising:
a movable nozzle;
a curved shaft;
a build plate connected to the curved shaft;
a motor;
a transmission connecting the motor and the curved shaft; and
a computer configured to control motion of the movable nozzle and the motor; and
wherein:
the transmission is configured to drive the curved shaft forwards or backwards such that the movement of the curved shaft moves the build plate along a curved path having a radius of curvature R originating on an axis when the transmission transfers power from the motor to the curved shaft,
the movable nozzle is configured to deposit material onto the build plate, and
the material deposited on the build plate moving along the curved path forms the part which has a shape of an arc having a center coinciding with the axis.

2. The apparatus of claim 1 , wherein:
the transmission further comprises gearing and a guide engaging the curved shaft,
the gearing, the guide, and a stiffness of the curved shaft provide a rigid support for the build plate, and
the build plate is configured to move in increments along the curved path such that the material is deposited in layers, each of the layers comprising a cross-sectional profile of the part.

3. The apparatus of claim 2 , further comprising a laser coupled to the movable nozzle, wherein the movable nozzle is configured to eject metal particles and the laser is configured to emit a laser beam to melt the metal particles to form the material deposited on the build plate.

4. The apparatus of claim 3 ,
wherein:
the movable nozzle follows a pattern tracing the cross-sectional profile of the part, and
the material deposited on the build plate moving along the curved path forms the part having exact dimensions D (within 1%) and curvature C defined in a computer generated representation of the part stored in the computer.

5. The apparatus of claim 4 , wherein the computer is configured to control a flow rate of the material from the movable nozzle and motion of the movable nozzle so that an outermost end of each of the layers is thicker than an innermost end of each of the layers.

6. The apparatus of claim 2 , wherein the computer is configured to control the motion of the movable nozzle and the motor such that each increment is a thickness of each of the layers and the thickness is in a range of 1-500 micrometers.

7. The apparatus of claim 2 , wherein the computer is configured to control the motion of the movable nozzle and the motor such that:
the part is a section of an engine inlet, and
a centerline of the section of the engine inlet coincides with the axis.

8. The apparatus of claim 7 , wherein the computer is configured to control the motion of the movable nozzle and the motor such that the cross-sectional profile comprises a profile of a lipskin comprising an outer barrel and a profile of a forward bulkhead connected to the lipskin.

9. The apparatus of claim 8 , wherein the computer is configured to control the motion of the movable nozzle and the motor such that the cross-sectional profile further comprises:
a profile of a stiffener connected to the profile of the outer barrel;
a profile of an inner barrel attached to the profile of the forward bulkhead;
a profile of an inner barrel connected to the profile of the outer barrel; and
a profile of an inlet attach flange connected to the profile of the inner barrel.

10. The apparatus of claim 7 , wherein the computer is configured to control the motion of the movable nozzle and the motor such that the cross-sectional profile further comprises a joint for connecting with an adjacent cross-sectional profile.

11. An apparatus, comprising:
a curved shaft;
a build plate connected to the curved shaft;
a motor; and
a transmission connecting the motor and the curved shaft; and
wherein, the transmission is configured to drive the curved shaft forwards or backwards such that the movement of the curved shaft moves the build plate along a curved path having a radius of curvature R originating on an axis when the transmission transfers power from the motor to the curved shaft.

12. The apparatus of claim 11 , wherein:
the transmission further comprises gearing and a guide engaging the curved shaft, and
the gearing, the guide, and a stiffness of the curved shaft provide a rigid support for the build plate, and
the build plate is configured to move in increments along the curved path.

13. A method for fabricating a part, comprising:
obtaining or providing an additive manufacturing apparatus for fabricating the part including:
a curved shaft
a build plate connected to the curved shaft;
a movable nozzle configured to deposit material onto the build plate;
a motor
a transmission connecting the motor and the curved shaft, the transmission configured to drive the curved shaft forwards or backwards such that the movement of the curved shaft moves the build plate along a curved path having a radius of curvature R originating on an axis when the transmission transfers power from the motor to the curved shaft; and
a computer configured to control motion of the movable nozzle and the motor; driving the curved shaft connected to the build plate,

moving the build plate along the curved path; and
depositing the material on the build plate moving along the curved path, wherein the material forms the part which has a shape of an arc having a center coinciding with the axis.

14. The method of claim 13 , further comprising:
engaging the curved shaft with the transmission comprising gearing and a guide; and
transferring power from the motor to the curved shaft using the transmission so that the build plate moves in increments along the curved path such that the material is deposited in layers, each of the layers comprising a cross-sectional profile of the part; and
wherein:
the gearing, the guide, and a stiffness of the curved shaft provide a rigid support for the build plate.

15. The method of claim 14 , further comprising:
ejecting metal particles from the movable nozzle; and
melting the metal particles using a laser beam emitted from a laser to form the material deposited on the build plate.

16. The method of claim 15 , further comprising:
controlling motion of the movable nozzle and the motor using the computer, wherein:
the movable nozzle follows a pattern tracing the cross-sectional profile of the part, and
the material deposited on the build plate moving along the curved path forms the part having the exact dimensions D and curvature C defined in a computer generated representation of the part stored in the computer.

17. The method of claim 16 , further comprising using the computer to control a flow rate of the metal particles from the nozzle and the motion of the nozzle so that an outermost end of each of the layers is thicker than an innermost end of each of the layers.

18. The method of claim 17 , wherein each increment is a thickness of each of the layers and the thickness is in a range of 1-500 micrometers.

Assignees

• Boeing Co

Inventors

• Bol Eric D

Classifications

• B23K26/147

  Features outside the nozzle for feeding the fluid stream towards the workpiece · CPC title

• B64D33/02

  of combustion air intakes · CPC title

• B23K2101/045

  Hollow panels · CPC title

• B23K2103/42

  Plastics other than composite materials · CPC title

• F05D2230/31

  Layer deposition · CPC title