Coupling part structure for vane and jet engine including the same

Patent metadata

Field	Value
Publication number	US-9896963-B2
Application number	US-201414398360-A
Country	US
Kind code	B2
Filing date	Oct 31, 2014
Priority date	Jun 20, 2012
Publication date	Feb 20, 2018
Grant date	Feb 20, 2018

Abstract

A coupling support member including a pair of divided pieces is placed in a coupling part between a vane proximal end portion of a guide vane and an attachment flange, and the pair of divided pieces are joined to the vane proximal end portion from both the sides in the vane thickness direction. A groove is formed in one end portion joint surface of the coupling support member, a linear protrusion is formed on the other end portion joint surface, the vane proximal end portion is formed into a concavo-convex shape, a linear protrusion that is engaged with the groove which is formed in the end portion joint surface is formed on a joint surface to the one end portion joint surface, a groove that is engaged with the linear protrusion formed on the end portion joint surface is formed in the joint surface to the other end portion joint surface. The vane proximal end portion is held between the pair of divided pieces of the coupling support member, by the fastening force that is applied to the coupling support member from both the sides in the vane thickness direction. It is possible to obtain a high structural strength while contributing to a reduction in weight of a jet engine.

First claim

The invention claimed is:

1. A coupling part structure for a vane that constitutes a jet engine and is made of a composite material of thermosetting resin or thermoplastic resin and reinforcement fiber, the coupling part structure comprising a vane coupling part, wherein
the vane coupling part includes a coupling support member placed therein, the coupling support member being made of metal and including a pair of divided pieces separated from each other, the pair of divided pieces being joined to an end portion of the vane from both sides in a vane thickness direction and each of the pair of divided pieces being directly attached to an attachment flange of a fan case or a fan frame of the jet engine,
on an either one of respective end joint surfaces of the pair of divided pieces of the coupling support member, a linear protrusion is formed in an axis direction of the jet engine, and in the other end joint surface, a groove is formed in the axis direction of the jet engine to face the linear protrusion,
the end portion of the vane is formed into a concavo-convex shape in a state with a constant vane thickness in a radial direction of the jet engine, the end portion of the vane has a groove that is engaged with the linear protrusion which is formed on the one end joint surface of either one of the pair of divided pieces, in either one joint surface of joint surfaces to the pair of divided pieces, and has a linear protrusion that is engaged with the groove which is formed in the end joint surface of the other one of the pair of divided pieces, on the other joint surface and at a back side position of the groove in the either one joint surface, and
the end portion of the vane is held between the pair of divided pieces of the coupling support member, by fastening force that is applied to the pair of divided pieces of the coupling support member from both the sides in the vane thickness direction.

2. The coupling part structure for the vane according to claim 1 , wherein an adhesive is interposed between the pair of divided pieces of the coupling support member and the end portion of the vane held between the pair of divided pieces.

3. The coupling part structure for the vane according to claim 2 , wherein the vane is a stator vane of the jet engine.

4. A jet engine comprising the coupling part structure for the vane according to claim 2 , as a coupling part structure for a vane constituting the jet engine.

5. The coupling part structure for the vane according to claim 1 , wherein the vane is a stator vane of the jet engine.

6. A jet engine comprising the coupling part structure for the vane according to claim 5 , as a coupling part structure for a vane constituting the jet engine.

7. A jet engine comprising the coupling part structure for the vane according to claim 1 , as a coupling part structure for a vane constituting the jet engine.

Assignees

• Ihi Corp
• Ihi Aerospace Co Ltd

Inventors

• Inada Takaomi
• Tanaka Shinichi

Classifications

• F05D2300/44

  Resins · CPC title

• F01D9/02

  Nozzles; Nozzle boxes; Stator blades; Guide conduits {, e.g. individual nozzles (nozzle boxes F01D9/047)} · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• F05D2260/31

  Retaining bolts or nuts · CPC title

• F02C7/20

  Mounting or supporting of plant; Accommodating heat expansion or creep · CPC title