Honeycomb structural body and method of manufacturing honeycomb structural body

Patent metadata

Field	Value
Publication number	US-9802382-B2
Application number	US-201514644915-A
Country	US
Kind code	B2
Filing date	Mar 11, 2015
Priority date	Mar 25, 2014
Publication date	Oct 31, 2017
Grant date	Oct 31, 2017

Abstract

A honeycomb structural body includes multiple cores, at least face sheet, and at least one reinforcement sheet. The multiple cores each have a honeycomb structure, and are bonded to each other with foamed adhesive in a direction in which the number of multiple pores formed by the honeycomb structure increases. The at least one face sheet is adhered to the multiple cores so as to cover the multiple pores. The reinforcement sheet is placed between the multiple cores and the at least one face sheet, at a position where the reinforcement sheet covers the foamed adhesive.

First claim

The invention claimed is:

1. A honeycomb structural body, comprising:
multiple cores that have a honeycomb structure, and which are bonded to each other with foamed adhesive in a direction in which the number of multiple pores that is formed by the honeycomb structure is increased;
at least one face sheet adhered to the multiple cores so as to cover the multiple pores, the at least one face sheet being made of composite material; and
multiple reinforcement sheets each placed on an outer surface side of the at least one face sheet, and at a position where the reinforcement sheets cover the foamed adhesive, the multiple reinforcement sheets being used to reinforce the composite material upon curing,
wherein the reinforcement sheets are adhered with film adhesive to the at least one face sheet.

2. The honeycomb structural body of claim 1 , wherein the reinforcement sheets are made of composite material.

3. The honeycomb structural body of claim 1 , wherein the reinforcement sheets are formed with chamfers.

4. The honeycomb structural body of claim 1 , wherein the at least one face sheet and the multiple cores constitute components of an airplane, and the multiple cores are made of composite material or metal.

5. The honeycomb structural body of claim 1 , wherein the reinforcement sheets are laminated such that widths of the reinforcement sheets gradually decrease outward from the outer surface side of the at least one face sheet.

6. The honeycomb structural body of claim 1 , further comprising an intermediate reinforcement sheet positioned between the multiple cores and the at least one face sheet.

7. The honeycomb structural body of claim 6 , wherein the intermediate reinforcement sheet is adhered to the multiple cores, the at least one face sheet, or both the multiple cores and the at least one face sheet with film adhesive.

8. A honeycomb structural body, comprising:
multiple cores that have a honeycomb structure, and which are bonded to each other with foamed adhesive in a direction in which the number of multiple pores that is formed by the honeycomb structure is increased;
at least one face sheet adhered to the multiple cores so as to cover the multiple pores, the at least one face sheet being made of composite material; and
multiple reinforcement sheets each placed on an outer surface side of the at least one face sheet, and at a position where the reinforcement sheets cover the foamed adhesive, the multiple reinforcement sheets being used to reinforce the composite material upon curing,
wherein the reinforcement sheets are formed with chamfers.

9. The honeycomb structural body of claim 8 , further comprising an intermediate reinforcement sheet positioned between the multiple cores and the at least one face sheet.

10. The honeycomb structural body of claim 9 , wherein the intermediate reinforcement sheet is adhered to the multiple cores, the at least one face sheet, or both the multiple cores and the at least one face sheet with film adhesive.

11. A method of manufacturing a honeycomb structural body, comprising:
placing multiple cores that each have a honeycomb structure on both sides of foamed adhesive in a direction in which the number of multiple pores formed by the honeycomb structure is increased;
placing at least one skin prepreg on the multiple cores so as to cover the multiple pores;
protecting an outer surface side of the at least one skin prepreg by a bagging film;
placing multiple reinforcement sheets between the at least one skin prepreg and the bagging film, and at a position where the reinforcement sheets cover the foamed adhesive for reinforcing the at least one skin prepreg upon curing, the reinforcement sheets being adhered with film adhesive to the at least one skin prepreg; and
manufacturing the honeycomb structural body in which the multiple cores are bonded to each other with the foamed adhesive and the at least one skin prepreg that is cured is bonded to the multiple cores, by heating and pressurizing the multiple cores, the at least one skin prepreg, the bagging film, and the reinforcement sheets in a set state.

12. The method of manufacturing the honeycomb structural body of claim 11 , wherein cured prepregs are used as the reinforcement sheets.

13. The method of manufacturing the honeycomb structural body of claim 12 , wherein the reinforcement sheets comprise sheets that have mutually different widths and are placed between the at least one skin prepreg and the bagging film in order of width.

14. The method of manufacturing the honeycomb structural body of claim 12 , wherein the reinforcement sheets comprise sheets such that a first reinforcement sheet made of a cured prepreg is placed between the at least one skin prepreg and the multiple cores, a second reinforcement sheet made of glass fiber reinforced plastics is placed on the at least one skin prepreg side between the at least one skin prepreg and the bagging film, and a third reinforcement sheet made of carbon fiber reinforced plastics is placed on the bagging film side between the at least one skin prepreg and the bagging film.

15. The method of manufacturing the honeycomb structural body of claim 11 , wherein the reinforcement sheets comprise sheets that have mutually different widths and are placed between the at least one skin prepreg and the bagging film in order of width.

16. The method of manufacturing the honeycomb structural body of claim 11 , wherein the reinforcement sheets comprise sheets such that a first reinforcement sheet made of a cured prepreg is placed between the at least one skin prepreg and the multiple cores, a second reinforcement sheet made of glass fiber reinforced plastics is placed on the at least one skin prepreg side between the at least one skin prepreg and the bagging film, and a third reinforcement sheet made of carbon fiber reinforced plastics is placed on the bagging film side between the at least one skin prepreg and the bagging film.

Assignees

• Fuji Heavy Ind Ltd
• Subaru Corp

Inventors

• Sugihara Yasunori

Classifications

• Y10T156/10

  Methods of surface bonding and/or assembly therefor · CPC title

• B32B7/12

  using interposed adhesives or interposed materials with bonding properties · CPC title

• B32B37/146 Primary

  whereby one or more of the layers is a honeycomb structure · CPC title

• B32B3/14

  characterised by a face layer formed of separate pieces of material {which are juxtaposed side-by-side (B32B5/02 takes precedence)} · CPC title

• B32B37/1018

  using only vacuum · CPC title