Aircraft water tank and method for manufacturing same

Patent metadata

Field	Value
Publication number	US-11459169-B2
Application number	US-201816766641-A
Country	US
Kind code	B2
Filing date	Nov 21, 2018
Priority date	Nov 22, 2017
Publication date	Oct 4, 2022
Grant date	Oct 4, 2022

Abstract

In an aircraft water tank, a mouthpiece is attached to an inner liner, and an overflowing adhesive is received in an annular missing portion provided to an expanded portion of the mouthpiece through the gap between a skirt portion and the inner liner. Further, a sealant fills the part of the annular missing portion, which is exposed from an end of a plate portion for the expanded portion.

First claim

The invention claimed is:

1. A method for manufacturing an aircraft water tank, comprising:
forming an inner liner including a dome portion; and
attaching a mouthpiece having an annular shape to a center of the dome portion, the mouthpiece being openable and closable by a lid,
the mouthpiece including:
a cylindrical portion including a joint potion, which is capable of being joined to the lid, at one axial end;
a skirt portion spreading annularly outward of the cylindrical portion in a radial direction from the other axial end of the cylindrical portion; and
an expanded portion that is expanded annularly inward of the cylindrical portion in the radial direction from the other axial end of the cylindrical portion,
the skirt portion including a skirt inner surface to which the inner liner is attached,
the expanded portion including:
a first expanded surface formed of a curved surface that is continuously connected to the skirt inner surface, is displaced inward in the radial direction, and extends toward the one axial end of the cylindrical portion; and
a second expanded surface that is displaced inward in the radial direction from a position corresponding to the expanded portion positioned on the one axial end side of the cylindrical portion, and extends toward the other axial end of the cylindrical portion, and
the inner liner being attached from the skirt inner surface to the first expanded surface with an adhesive, the method further comprising
providing an annular missing portion in the first expanded surface, the annular missing portion being depressed inside of the expanded portion with a width in an axial direction of the cylindrical portion and extending along an entire circumference of the first expanded surface in a circumferential direction,
forming the center of the dome portion of the inner liner of a plate portion for the skirt portion, which is bonded to the skirt inner surface, and a plate portion for the expanded portion, which is connected continuously to an end of the plate portion for the skirt portion and bonded to the first expanded surface, and has an end positioned at an intermediate portion of the annular missing portion in a width direction under a state of being bonded to the first expanded surface,
bringing the center of the dome portion and the mouthpiece close to each other in the axial direction of the mouthpiece, aligning the plate portion for the skirt portion with the skirt inner surface through intermediation of the adhesive, aligning the plate portion for the expanded portion with the first expanded surface, and receiving an excessive part of the adhesive in the annular missing portion, and
filling a part of the annular missing portion, which is exposed from the end of the plate portion for the expanded portion, with a sealant.

2. An aircraft water tank, comprising:
an inner liner including a dome portion; and
a mouthpiece having an annular shape, the mouthpiece being attached to a center of the dome portion and being opened and closed by a lid,
the mouthpiece including:
a cylindrical portion including a joint potion, which is capable of being joined to the lid, at one axial end;
a skirt portion spreading annularly outward of the cylindrical portion in a radial direction from the other axial end of the cylindrical portion; and
an expanded portion that is expanded annularly inward of the cylindrical portion in the radial direction from the other axial end of the cylindrical portion,
the skirt portion including a skirt inner surface to which the inner liner is attached,
the expanded portion including:
a first expanded surface formed of a curved surface that is continuously connected to the skirt inner surface, is displaced inward in the radial direction, and extends toward the one axial end of the cylindrical portion; and
a second expanded surface that is displaced inward in the radial direction from a position corresponding to the expanded portion positioned on the one axial end side of the cylindrical portion, and extends toward the other axial end of the cylindrical portion, and
the inner liner being attached from the skirt inner surface to the first expanded surface with an adhesive, wherein
an annular missing portion is provided in the first expanded surface, the annular missing portion being depressed inside of the expanded portion with a width in an axial direction of the cylindrical portion and extending along an entire circumference of the first expanded surface in a circumferential direction,
an end of the inner liner is positioned at an intermediate portion of the annular missing portion in a width direction, and the adhesive that is left over after bonding the inner liner to the skirt inner surface and the first expanded surface is received in a gap between the inner liner and the annular missing portion, and
a sealant fills a remaining part of the annular missing portion, which does not receive the adhesive, and the adhesive received in the annular missing portion is covered with the inner liner and the sealant.

3. The aircraft water tank according to claim 2 , wherein
the second expanded surface is provided with a cone surface that is displaced inward in the radial direction and extends toward the other axial end of the cylindrical portion, and
a sealing member mounted to the lid is held in elastic contact with the cone surface.

4. The aircraft water tank according to claim 2 , wherein
the annular missing portion is provided from a position in the first expanded surface, which is close to the second expanded surface, to a position in the second expanded surface, which is close to the first expanded surface.

5. The aircraft water tank according to claim 3 , wherein the annular missing portion is provided from a position in the first expanded surface, which is close to the second expanded surface, to a position in the second expanded surface, which is close to the first expanded surface.

Assignees

• Yokohama Rubber Co Ltd

Inventors

• Kato Hayato
• Kobayashi Takafumi

Classifications

• B64D11/02

  Toilet fittings · CPC title

• B65D90/08

  Interconnections of wall parts; Sealing means therefor · CPC title

• B65D2588/54

  characterised by means facilitating filling or emptying · CPC title

• B29C70/72 Primary

  Encapsulating inserts having non-encapsulated projections, e.g. extremities or terminal portions of electrical components {(B29C70/742 takes precedence)} · CPC title

• F17C2209/234

  of closing end pieces, e.g. caps · CPC title