Method of manufacturing composite material blade

• US 5,041,182 A
• Filed: 09/18/1990
• Issued: 08/20/1991
• Est. Priority Date: 09/20/1989
• Status: Expired due to Fees

• Current Assignee: Fuji Jukogyo KK (Subaru Corp.)
• Original Assignee: Fuji Jukogyo KK (Subaru Corp.)
• Inventors: Nishiwaki, Yasuto, Sekiguchi, Takashi
• Primary Examiner(s): HEITBRINK, JILL LYNNE
• Application Number:
  US07/584,727
• Time in Patent Office: 336 Days
• Field of Search: 156/245, 29/889.6, 29/889.61, 29/889.71, 416/229 R, 416/230, 264/250, 264/251, 264/255, 264/257, 264/258, 264/259, 264/294, 264/317, 264/336
• US Class Current: 156/245
• CPC Class Codes: B29C 2791/001 Shaping in several steps
• CPC Class Codes: B29C 70/345 using matched moulds
• CPC Class Codes: B29D 99/0025 Producing blades or the like, e.g. blades for turbines, propellers, or wings
• CPC Class Codes: B29L 2031/082 Blades, e.g. for helicopters
• CPC Class Codes: B64C 2027/4736 from composite materials
• CPC Class Codes: B64C 27/473 Constructional features
• CPC Class Codes: Y10T 29/49337 Composite blade

Abstract

In manufacturing a composite material blade for a helicopter, for example, an upper and a lower dummy skins are disposed on molding surfaces of an upper and a lower mold halves. A dummy block provided with a preliminarily hardened vertical rib and having an outer shape corresponding to the molding surface of the lower mold half is also disposed. A lower portion of a spar is joined to a lower surface front edge cover and the vertical rib and a rear edge reinforcing member is joined to the lower surface rear edge cover. An annular reinforcing member and a front edge block are disposed on the lower portion of the spar and an upper portion of the spar is disposed on the annular reinforcing member and the front edge block. In this state, the upper and the lower mold halves are closed and thermo-setting treatment is performed to the closed mold assembly. After that, the upper and the lower surface dummy skins and the dummy block are removed, and the actual upper and lower skins and the core member are disposed in the mold halves, which are closed and subjected to thermo-setting treatment.

Claims

1. A method of manufacturing a blade member constituted by composite materials comprising the steps of:

preparing a mold assembly provided with an upper and a lower mold halves, each having an inner molding surface;

disposing an upper dummy skin, an upper surface leading edge cover and an upper surface trailing edge cover on the molding surface of the upper mold half;

disposing a lower dummy skin, a lower surface leading edge cover and a lower surface trailing edge cover on the molding surface of the lower mold half;

disposing, on the lower dummy skin between the lower surface leading edge cover and the lower surface trailing edge cover, a dummy block provided with a preliminarily hardened vertical rib on the front end thereof and having an outer shape corresponding to the molding surface of the lower mold half;

joining a lower member of a spar to the lower surface leading edge cover and the vertical rib and joining a trailing edge reinforcing member to the lower surface trailing edge cover;

disposing an annular reinforcing member and a leading edge block on the lower member of the spar and disposing an upper member of the spar on the annular reinforcing member and the leading edge block;

closing the upper and the lower mold halves to perform thermo-setting treatment to the closed mold assembly;

opening the mold assembly;

changing the upper dummy skin on the molding surface of the upper mold half to an upper surface skin;

changing the lower dummy skin and the dummy

block on the molding surface of the lower mold to a lower surface skin and a core member, respectively; and

closing the upper and lower molding halves to perform thermo-setting treatment to the closed mold assembly.

2. The method according to claim 1, wherein

the upper and lower dummy skins and the dummy block have a non-adhesive property.

3. The method according to claim 1, wherein

the upper and lower mold halves are provided with fixing holes aligned with each other when the upper and lower mold halves are closed, the dummy block is provided with a through hole in alignment with the fixing holes when the upper and lower mold halves are closed, and a fixing member is inserted into the fixing holes and the through hole after the upper and lower mold halves are closed and fixed.

4. The method according to claim 3, wherein

said fixing member is a pin.

5. The method according to claim 3, wherein

said fixing member is a plug.

6. The method according to claim 1, wherein

the lower mold half is provided with a fixing hole, the dummy block is provided with a vertical hole which is aligned with the fixing hole of the lower mold half when the dummy block is disposed on the molding surface of the lower mold half and a fixing member is inserted into the fixing holes of the lower mold half and the dummy block.

7. The method according to claim 1, wherein

one of the molding surfaces of the upper and lower mold halves is provided with projections and the other one thereof is provided with recesses, said projections and said recesses engaging when the upper and lower mold halves are closed.

8. The method according to claim 1, wherein

the upper and lower mold halves are firmly engaged by bolts and nuts when said upper and lower mold halves are closed.

9. The method according to claim 1, wherein

the upper surface leading and trailing edge covers and the lower surface leading and trailing edge covers are formed of woven cloth made of resin impregnated glass fibers.

10. The method according to claim 1, wherein

the annular reinforcing member is provided with a core made of a foaming material.

11. The method according to claim 1, wherein

the dummy block is made of a heat resisting resin material.

12. The method according to claim 1, wherein

the leading edge block includes a balance weight for keeping the balance of the blade member.