Method and apparatus for forming a nacelle leading edge

Patent metadata

Field	Value
Publication number	US-11065668-B2
Application number	US-201916264763-A
Country	US
Kind code	B2
Filing date	Feb 1, 2019
Priority date	Feb 1, 2019
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

An apparatus for forming a nacelle leading edge includes an actuation assembly, a punch, and a die. The punch is in communication with the actuation assembly and annularly disposed about a first axis. The punch is configured to mate with an interior surface of a preform. The die is in communication with the actuation assembly and disposed within the first axis. The die is configured to retain an exterior surface of the preform. The actuation assembly is configured to effect relative motion between the punch and the preform. The actuation assembly is configured to offset the punch so that the punch is annularly disposed about a second axis, different than the first axis.

First claim

What is claimed is:

1. A method for forming a nacelle leading edge, comprising:
positioning a preform between a punch and a die, the punch and the die annularly disposed about a first axis;
moving, relatively, at least one of the punch and the preform towards the other of the punch and the preform along the first axis so that a portion of the preform is formed over a leading edge of the punch; and
rotating the punch so that the punch is annularly disposed about a second axis, different than the first axis.

2. The method of claim 1 , wherein the punch is configured to mate with an interior surface of the preform and the die retains an exterior surface of the preform.

3. The method of claim 1 , further comprising, following rotating the punch, moving at least one of the punch and the die towards the other of the punch and the die.

4. The method of claim 3 , further comprising moving, relatively, the die towards the punch along the first axis.

5. The method of claim 3 , further comprising moving, relatively, the punch towards the die along the second axis.

6. The method of claim 1 , wherein the die retains a first end of the preform and at least one clamp retains an opposing second end of the preform.

7. The method of claim 1 , further comprising positioning a preform holder about an interior surface of the preform opposite the die.

8. The method of claim 1 , wherein the first axis is an axial centerline of the preform.

9. The method of claim 8 , wherein the second axis is a centerline of the nacelle leading edge.

10. The method of claim 1 , wherein the preform comprises a full annulus corresponding to the nacelle leading edge.

11. The method of claim 1 , wherein the preform comprises a segment of a full annulus corresponding to the nacelle leading edge.

12. The method of claim 1 , wherein the first axis intersects the second axis such that the first axis and the second axis define an angle therebetween.

13. An apparatus for forming a nacelle leading edge, comprising:
an actuation assembly;
a punch in communication with the actuation assembly and annularly disposed about a first axis, the punch configured to mate with an interior surface of a preform; and
a die in communication with the actuation assembly and annularly disposed about the first axis, the die configured to retain an exterior surface of the preform;
wherein the actuation assembly is configured to effect relative motion between the punch and the preform; and
wherein the actuation assembly is configured to rotate the punch so that the punch is annularly disposed about a second axis, different than the first axis.

14. The apparatus of claim 13 , wherein the actuation assembly is configured to effect relative movement between the punch and the preform along the first axis and the second axis.

15. The apparatus of claim 13 , wherein the actuation assembly is configured to move the die towards the punch along the first axis.

16. The apparatus of claim 13 , further comprising a preform holder configured to mate with an interior surface of the preform opposite the die.

17. The apparatus of claim 13 , wherein the first axis is an axial centerline of the preform.

18. The apparatus of claim 13 , wherein the preform comprises a full annulus corresponding to the nacelle leading edge.

19. The apparatus of claim 13 , wherein the preform comprises a segment of a full annulus corresponding to the nacelle leading edge.

20. An apparatus for forming a nacelle leading edge, comprising:
an actuation assembly;
a punch in communication with the actuation assembly and annularly disposed about a first axis, the punch configured to mate with an interior surface of a preform; and
a die in communication with the actuation assembly and annularly disposed about the first axis, the die configured to retain an exterior surface of the preform;
wherein the actuation assembly is configured to rotate the punch so that the punch is annularly disposed about a second axis, different than the first axis; and
wherein the actuation assembly is configured to at least one of effect relative movement between the die and the preform along the first axis and effect relative movement between the punch and the preform along one of the first axis and the second axis.

Assignees

• Rohr Inc

Inventors

• Douglas Alan R

Classifications

• B64D29/00

  Power-plant nacelles, fairings or cowlings · CPC title

• B21D53/92

  other parts for aircraft · CPC title

• B64F5/10

  Manufacturing or assembling aircraft, e.g. jigs therefor · CPC title

• B21D39/04 Primary

  of tubes with tubes; of tubes with rods {(crimped pipe joints as such F16L13/14)} · CPC title

• B23P15/04

  turbine or like blades from several pieces · CPC title