Tool alignment system and method

Patent metadata

Field	Value
Publication number	US-12390865-B2
Application number	US-202217650091-A
Country	US
Kind code	B2
Filing date	Feb 7, 2022
Priority date	Feb 7, 2022
Publication date	Aug 19, 2025
Grant date	Aug 19, 2025

Abstract

A system and a method include a fixture template configured to be secured to a component. The fixture template includes a plurality of insert holes. A plurality of guide inserts have channels. Each of the channels has an orientation. The orientation of at least two of the plurality of guide inserts differs. Each of the plurality of guide inserts is removably secured within a respective one of the plurality of inserts holes to position and orient the channels in relation to a pattern of openings to be formed in relation to the component. Each of the channels is configured to receive an operative member of a tool that is configured to form the pattern of openings in relation to the component.

First claim

What is claimed is:

1. A system comprising:
a fixture template configured to be secured to a component, the fixture template including a plurality of insert holes; and
a plurality of guide inserts, wherein each of the plurality of guide inserts comprises:
a respective plug;
a respective collar; and
a respective channel formed through the plug and the collar corresponding thereto, and wherein the respective plug of each of the plurality of guide inserts is configured to be received and retained by one of the plurality of insert holes of the fixture template,
wherein the respective channel formed through the plug and the collar corresponding thereto has a longitudinal axis, and the respective channel extends a length that spans an entirety of said plug and an entirety of said collar,
wherein, when each of the plurality of guide inserts is received and is retained by one of the plurality of insert holes of the fixture template, the respective longitudinal axis for each respective channel has an oblique orientation with respect to a vertical extending longitudinal axis of a corresponding key of each of the plurality of guide inserts,
wherein outer dimensions of the respective plug and the respective collar for each of the plurality of guide inserts are the same, and wherein the oblique orientation of the respective channel of at least two of the plurality of guide inserts differs,

wherein each of the plurality of guide inserts is removably secured within a respective one of the plurality of inserts holes to position and orient the respective channel of each of the plurality of guide inserts in relation to a pattern of openings to be formed in the component, and
wherein the respective channel of each of the plurality of guide inserts is configured to receive an operative member of a tool that is configured to form the pattern of openings in the component.

2. The system of claim 1 , wherein the tool is a drill.

3. The system of claim 1 , wherein the component is a portion of an aircraft.

4. The system of claim 1 ,
wherein the fixture template further comprises a plurality of index slots,
wherein each one of the plurality of index slots is connected to a corresponding one of the plurality of insert holes, and
wherein each of the plurality of guide inserts comprises a respective key that is configured to be removably secured within a corresponding one of the plurality of index slots.

5. The system of claim 1 , wherein the oblique orientation of each of and all of the plurality of guide inserts differs.

6. The system of claim 1 , wherein, for at least two of the plurality of guide inserts, a respective length, a respective axial angle, and a respective radial angle of the corresponding channel differs for each of the at least two of the plurality of guide inserts.

7. The system of claim 1 , wherein the fixture template further comprises a different fixture identifier proximate to each of the plurality of insert holes, wherein each of the plurality of guide inserts comprises a different insert identifier, and wherein each of the different insert identifiers corresponds to one of the different fixture identifiers to ensure proper location of the plurality of guide inserts within the plurality of insert holes.

8. The system of claim 1 , wherein the plurality of insert holes includes four or more insert holes, and the plurality of guide inserts includes four or more guide inserts.

9. The system of claim 1 , wherein the fixture template comprises a main body having a first surface and a second surface opposite from the first surface, wherein each of the plurality of insert holes is formed through the main body between and through the first surface and the second surface.

10. A system comprising:
a fixture template configured to be secured to a component, the fixture template including a plurality of insert holes and a plurality of index slots, wherein each one of the plurality of index slots is connected to a corresponding one of the plurality of insert holes; and
a plurality of guide inserts, wherein each of the plurality of guide inserts comprises:
a respective plug;
a respective collar;
a respective key that is configured to be removably secured within a corresponding one of the plurality of index slots, and
a respective channel formed through the plug and the collar corresponding thereto, and wherein the respective plug of each of the plurality of guide inserts is configured to be received and retained by one of the plurality of insert holes of the fixture template,
wherein the respective channel formed through the plug and the collar corresponding thereto has a longitudinal axis, and the respective channel extends a length that spans an entirety of said plug and an entirety of said collar, and
wherein, when each of the plurality of guide inserts is received and is retained by one of the plurality of insert holes of the fixture template, the respective longitudinal axis for each respective channel has an oblique orientation with respect to a vertical extending longitudinal axis of the corresponding key of each of the plurality of guide inserts,
wherein the oblique orientation of the respective channel of at least two of the plurality of guide inserts differs, and wherein outer dimensions of the respective plug and the respective collar for each of the plurality of guide inserts are the same,

wherein each of the plurality of guide inserts is removably secured within a respective one of the plurality of inserts holes to position and orient the respective channel of each of the plurality of guide inserts in relation to a pattern of openings to be formed in the component, and
wherein the respective channel of each of the plurality of guide inserts is configured to receive an operative member of a drill that is configured to form the pattern of openings in the component.

11. The system of claim 10 , wherein the fixture template further comprises a different fixture identifier proximate to each of the plurality of insert holes, wherein each of the plurality of guide inserts comprises a different insert identifier, and wherein each of the different insert identifiers corresponds to one of the different fixture identifiers to ensure proper location of the plurality of guide inserts within the plurality of insert holes.

12. A method of operating the system according to claim 1 , the method comprising:
providing the system of claim 1 ;
securing the fixture template to a component;
removably securing each of the plurality of guide inserts within a respective one of the plurality of insert holes of the fixture template so as to position and orient the respective channel of each of the plurality of guide inserts in relation to the pattern of openings that is to be formed in the component; and
inserting, in the respective channel of each of the plurality of guide inserts, the operative member of the tool which is configured to form the pattern of openings in the component.

13. The method of claim 12 , wherein the tool is a drill.

14. The method of claim 12 , wherein the component is a portion of an aircraft.

15. The method of claim 12 , further comprising removably securing a respective key of each of the plurality of guide inserts within a corresponding one of a plurality of index slots, wherein each of the plurality of index slots is connected to a corresponding one of the plurality of insert holes.

16. The method of claim 12 , wherein the oblique orientation of each of and all of the plurality of guide inserts differs.

17. The method of claim 12 , wherein, for at l

Assignees

• Boeing Co

Inventors

• Farniok Craig Martin
• Roffo Todd Jeremy
• Brown Thomas A

Classifications

• Y10T408/03

  Processes · CPC title

• Y10T408/569

  Bushing · CPC title

• Y10T408/568

  Guide bushing · CPC title

• B23B2215/04

  Aircraft components · CPC title

• B23B2260/026

  Bushings, e.g. adapter sleeves · CPC title