Hybrid solid-inflatable mandrel for blade manufacturing

Patent metadata

Field	Value
Publication number	US-2016354968-A1
Application number	US-201514733077-A
Country	US
Kind code	A1
Filing date	Jun 8, 2015
Priority date	Jun 8, 2015
Publication date	Dec 8, 2016
Grant date	—

Abstract

A mandrel ( 20, 30 ) defines a void geometry in a layup for a blade shell ( 73 ) via a rigid mandrel core ( 22, 32 ) and a plurality of expandable bladders ( 24 A-F, 34 A-F) attached adjacently to each other in sequence around a periphery of the core, forming an expandable outer cover on the mandrel. The bladders are controllably expandable ( 50, 50 B, 60 ) individually or in proper subsets of all the bladders to adjust pressure distribution and mandrel position within the layup after closing a blade shell mold over the layup. The bladders may be transversely partitioned ( 104 ) at multiple spanwise (S) positions along the mandrel in order to define additional sets of adjustable bladders along the span of the mandrel.

First claim

The invention claimed is:

1 . An apparatus for fabrication of a blade, comprising;
a plurality of expandable bladders adjacently attached around a periphery of a substantially rigid core as seen in a transverse sectional view thereof; and a control system that controls an expansion condition of the bladders individually or in selectable proper subsets thereof; wherein the bladders are configured to provide outward force against an interior of a layup of a shell of the blade in a mold while the mold constrains an outer surface of the blade shell layup.

2 . The apparatus of claim 1 , wherein the bladders are individually valved such that an expansion and a contraction of each bladder is individually controlled.

3 . The apparatus of claim 1 , wherein the bladders are valved and controlled such that an expansion gas cannot shift among them during a given stage of fabrication.

4 . The apparatus of claim 1 , wherein the rigid core comprises a forward mandrel core in the shell layup, and the plurality of expandable bladders comprises:
a leading edge bladder; a suction side bladder; a forward suction side spar cap bladder; a bladder for a forward side of a spar webbing; a forward pressure side spar cap bladder; and a forward pressure side bladder.

5 . The apparatus of claim 4 , further comprising an aft mandrel core spaced aft of the forward mandrel core in the shell layup, wherein the aft mandrel core is covered by a second plurality of expandable bladders disposed around a periphery of the aft mandrel core as seen in a transverse sectional view thereof, and the second plurality of expandable bladders comprises:
a bladder for an aft side of the spar webbing; an aft suction side spar cap bladder; a suction side bladder; a trailing edge bladder; an aft pressure side bladder; and an aft pressure side spar cap bladder.

6 . The apparatus of claim 1 , wherein the control system further comprises:
a valve and a gas distribution tube for each bladder; a compressed air source for expanding the bladders via the distribution tubes; and a vacuum source for contracting the bladders via the distribution tubes.

7 . The apparatus of claim 1 , wherein the rigid core has a hollow interior, and further comprising a resilient foam filling and expanding each of the bladders, wherein the control system comprises a gas valve that connects each bladder individually with the interior of the core, a vacuum source that evacuates the interior of the core for contracting the bladders via the gas valves, and an air inlet that communicates with the core interior allowing the bladders to expand by a rebound of the resilient foam therein.

8 . The apparatus of claim 1 , further comprising a rigid bridge plate spanning between adjacent ones of the bladders and defining respective portions of an interior surface of the blade shell.

9 . An apparatus for fabrication of a blade, comprising;
a forward mandrel and an aft mandrel, each mandrel being elongated spanwise and comprising a plurality of expandable bladders disposed around a periphery of a respective substantially rigid core of the respective mandrel as seen in a transverse section thereof, forming an expandable outer cover of the respective mandrel; the forward and aft mandrels configured to define respective forward and aft void geometries of a blade interior; and a control system that expands and contracts the expandable bladders individually or in selectable proper subsets thereof.

10 . A blade fabrication method, comprising;
providing an apparatus as in claim 9 ; placing a suction side fabric layup in a bottom half of a mold for a blade shell; placing the forward and aft mandrels on respective forward and aft sides of the suction side layup, wherein the mandrels are substantially parallel and are spaced chordwise from each other; positioning a spar webbing layup between the mandrels; expanding at least a proper subset of the bladders; placing a pressure side fabric layup on the mandrels; closing the mold over the pressure side fabric layup; and adjusting an expansion of the bladders individually or in selected proper subsets thereof to provide a predetermined distribution of pressure of the bladders on the blade shell during a curing thereof.

Assignees

• Siemens Ag

Inventors

• Zamora Rodriguez Alonso O
• Mayda Edward A

Classifications

• B29C33/505 Primary

  cores or mandrels, e.g. inflatable (B29C33/0016 takes precedence; for winding and joining B29C53/824; for supporting articles during joining B29C66/634; flexible cores for vulcanizing tyres B29D30/0654) · CPC title

• B29L2031/085

  Wind turbine blades · CPC title

• B29C53/02 Primary

  Bending or folding (B29C53/22, B29C53/34, B29C53/36, B29C53/56 take precedence) · CPC title

• Y02P70/50

  Manufacturing or production processes characterised by the final manufactured product · CPC title

• B29C70/44

  using isostatic pressure, e.g. pressure difference-moulding, vacuum bag-moulding, autoclave-moulding or expanding rubber-moulding · CPC title