Apparatus and methods for injecting filler material into a hole in a composite layer

Patent metadata

Field	Value
Publication number	US-10603844-B2
Application number	US-201715786665-A
Country	US
Kind code	B2
Filing date	Oct 18, 2017
Priority date	Oct 18, 2017
Publication date	Mar 31, 2020
Grant date	Mar 31, 2020

Abstract

Apparatus and methods for injecting molten filler material into a hole. The method in accordance with one embodiment comprises: drilling a hole in a composite layer; heating filler material comprising an electrically conductive low-melting alloy to a molten state; inserting a nozzle having an internal channel system into the hole with a gap separating the nozzle and the hole; forcing molten filler material into, through and out of the internal channel system of the nozzle and into the gap; and retracting the nozzle from the hole. The nozzle may be rotary or not rotary.

First claim

The invention claimed is:

1. A method for injecting molten filler material into a hole, the method comprising:
(a) drilling the hole in a composite layer;
(b) heating filler material comprising an electrically conductive low-melting alloy to a molten state to produce the molten filler material;
(c) inserting a nozzle having an internal channel system into the hole with a gap separating the nozzle and the hole;
(d) forcing the molten filler material into, through, and out of the internal channel system of the nozzle and into the gap; and
(e) retracting the nozzle from the hole.

2. The method as recited in claim 1 , further comprising rotating the nozzle as the molten filler material exits the nozzle.

3. The method as recited in claim 2 , wherein the molten filler material exits the nozzle through a plurality of circumferentially distributed side openings.

4. The method as recited in claim 1 , wherein the molten filler material exits the nozzle during retraction of the nozzle.

5. The method as recited in claim 4 , wherein the molten filler material exits the nozzle through a circular circumferential orifice and is redirected and pushed in a direction having a radially outward component by a contoured flow-redirecting surface of the nozzle during retraction of the nozzle.

6. The method as recited in claim 1 , further comprising guiding excess molten filler material to flow from the gap to a reservoir external to the hole.

7. The method as recited in claim 1 , wherein step (a) comprises drilling a hole that has a chamfer in an uppermost portion of the hole, the method further comprising guiding a flow of the molten filler material to coat a surface of the chamfer.

8. The method as recited in claim 1 , further comprising heating the molten filler material as the molten filler material flows through the internal channel system of the nozzle.

9. The method as recited in claim 1 , wherein the nozzle is retracted until the nozzle is completely removed from the hole, the method further comprising inserting a fastener into the hole with an interference fit.

10. The method as recited in claim 9 , further comprising heating the fastener before insertion.

11. An apparatus for injecting molten filler material into a hole, the apparatus comprising:
a reservoir for storing the molten filler material that is electrically conductive;
a pump assembly in fluid communication with the reservoir; and
a nozzle in fluid communication with the pump assembly for receiving the molten filler material pumped from the reservoir and ejecting the molten filler material, wherein the nozzle comprises:
a proximal body portion having an internal volume in fluid communication with the pump assembly;
an intermediate body portion comprising a plurality of longitudinal melt channels configured to guide the molten filler material entering from the internal volume of the proximal body portion to flow parallel to a longitudinal axis of the nozzle and away from the proximal body portion; and
a distal body portion comprising a flow-redirecting surface configured to divert a longitudinal flow of the molten filler material to flow radially outward from the nozzle,
wherein a portion of the flow-redirecting surface of the distal body portion and a portion of the intermediate body portion define a circular circumferential orifice.

12. The apparatus as recited in claim 11 , wherein the intermediate body portion of the nozzle comprises an outer circumferential wall having a circular terminal portion, and a portion of the intermediate body portion that partly defines the circular circumferential orifice comprises the circular terminal portion of the outer circumferential wall.

13. The apparatus as recited in claim 12 , wherein the intermediate body portion of the nozzle further comprises:
an inner circumferential wall; and
a plurality of radial spacers that maintain separation between the inner circumferential wall and the outer circumferential wall,
wherein the longitudinal melt channels are defined by respective portions of an inner surface of the outer circumferential wall, by respective portions of an outer surface of the inner circumferential wall, and by respective surfaces of respective pairs of radial spacers.

14. The apparatus as recited in claim 12 , wherein the flow-redirecting surface of the distal body portion of the nozzle is a circumferential surface of revolution having a diameter that increases continuously to a maximum diameter of the distal body portion that is greater than an outer diameter of the outer circumferential wall.

15. The apparatus as recited in claim 11 , further comprising:
a recycling pump in fluid communication with the reservoir;
a pipe in fluid communication with the recycling pump; and
an end cap in fluid communication with the pipe, wherein the end cap is configured to sit atop the hole in a composite material and cover a volume of space that is in fluid communication with the pipe and have an opening through which a portion of the nozzle is passed.

16. The apparatus as recited in claim 11 , further comprising:
a retraction mechanism for retracting the nozzle; and
a control computer configured with programming for controlling a rate of rotation of the pump assembly and a rate of displacement of the retraction mechanism during a filling operation.

17. The apparatus as recited in claim 11 , further comprising a heating element disposed inside the nozzle.

18. An apparatus for injecting molten filler material into a hole, the apparatus comprising:
a reservoir for storing the molten filler material that is electrically conductive;
a pump assembly in fluid communication with the reservoir;
a rotary nozzle in fluid communication with the pump assembly for receiving the molten filler material pumped from the reservoir and ejecting the molten filler material; and
a motor for driving rotation of the rotary nozzle,
wherein the rotary nozzle comprises a circular cylindrical intermediate body portion having an internal channel system and a plurality of side openings that are circumferentially distributed and extend a length of the circular cylindrical intermediate body portion and allow the molten filler material to flow radially outward from the rotary nozzle, and wherein the plurality of side openings are linear or the plurality of side openings are helical.

19. The apparatus as recited in claim 18 , further comprising respective pairs of beveled projections disposed at opposite edges of each side opening.

20. The apparatus as recited in claim 18 , further comprising a control computer configured with programming for controlling a rate of rotation of the pump assembly and a rate of rotation of the rotary nozzle during a filling operation.

21. A structural assembly for an aircraft, the structural assembly comprising:
a composite layer having a hole with a relatively rough surface that has concavities; and
a coating adhered to the relatively rough surface of the hole and filling the concavities, the coating defining a smooth circular cylindrical surface of a coated hole, which smooth circular cylindrical surface circumscribes an empty space,
wherein the composite layer comprises fibers made of electrically conductive material and the coating comprises an electrically conductive low-melting alloy.

Assignees

• Boeing Co

Inventors

• Khosravani Shahriar
• Simpson Blake A
• Hansen Darrin M
• Dufour Mark J

Classifications

• B29C65/542 Primary

  by injection · CPC title

• B29C70/88

  characterised primarily by possessing specific properties, e.g. electrically conductive or locally reinforced · CPC title

• F16B1/00

  Devices for securing together, or preventing relative movement between, constructional elements or machine parts · CPC title

• B22D41/60

  with heating or cooling means · CPC title

• B22D17/2023 Primary

  Nozzles or shot sleeves · CPC title