Amorphous metal riblets

Patent metadata

Field	Value
Publication number	US-9656743-B2
Application number	US-201314070183-A
Country	US
Kind code	B2
Filing date	Nov 1, 2013
Priority date	Jan 29, 2009
Publication date	May 23, 2017
Grant date	May 23, 2017

Abstract

An array of aerodynamic riblets is created by a plurality of high stiffness tips with a layer supporting the tips in predetermined spaced relation and adhering the tips to a vehicle surface.

First claim

What is claimed is:

1. An array of riblets comprising:
a plurality of amorphous metal tips having a dimension perpendicular to a vehicle surface of approximately 0.002 inch and moduli of elasticity in a range of about 10-30×106 lb/in2, each amorphous metal tip having a respective base expanding from a bottom of the respective tip such that an internal angle of the base is greater than an internal angle of the tip, said tips having longitudinal gaps to segment the tips;
a polymer layer surrounding and at least partially encapsulating the bases to engage each tip supporting said amorphous metal tips in predetermined spaced relation, each of the amorphous metal tips protruding from the polymer forming substantially parallel aerodynamic riblets.

2. The array of riblets as defined in claim 1 wherein the amorphous metal tips are formed from material selected from the set of an alloy of Zr: 52.5 Ti: 5 Cu: 17.9 Ni: 14.6 Al: 10) or an alloy of Zr: 58.5 Cu: 15.6 Ni: 12.8 Al: 10.3 Nb: 2.8.

3. The array of riblets as defined in claim 1 wherein the polymer layer comprises:
an elastomeric layer engaging the amorphous metal tips and supporting said amorphous metal tips in predetermined spaced relation with the base of each tip embedded in the elastomeric layer.

4. The array of riblets as defined in claim 1 further comprising an adhesive layer deposited on the elastomeric layer to form a multilayer appliqué, said adhesive layer adhering the multilayer appliqué to the vehicle surface.

5. An aircraft structure comprising:
an array of aerodynamic riblets having
a plurality of amorphous metal tips formed from material selected from the set of an alloy of Zr: 52.5 Ti: 5 Cu: 17.9 Ni: 14.6 Al: 10 or an alloy of Zr: 58.5 Cu: 15.6 Ni: 12.8 Al: 10.3 Nb: 2.8 and highly reflective for a decorative feature, each amorphous metal tip having a respective base expanding from a bottom of the respective tip such that an internal angle of the base is greater than an internal angle of the tip, and each tip segmented in the flow direction;
an elastomeric layer surrounding and at least partially encapsulating the bases of each amorphous metal tip, to embed said amorphous metal tips in predetermined spaced relation, each of the amorphous metal tips protruding from the elastomeric layer forming substantially parallel aerodynamic riblets;
a preformed appliqué comprising a metallic layer, a polymer support layer and an adhesive layer deposited on the elastomeric layer opposite the tips to form a multilayer appliqué said adhesive layer adhering the multilayer appliqué to a surface of an aircraft.

Assignees

• Boeing Co

Inventors

• Rawlings Diane C
• Christensen Stephen

Classifications

• B64C2230/26

  by using rib lets or hydrophobic surfaces · CPC title

• B64C1/38

  Constructions adapted to reduce effects of aerodynamic or other external heating · CPC title

• B32B2307/702

  Amorphous · CPC title

• B64C21/10 Primary

  using other surface properties, e.g. roughness · CPC title

• B32B2307/50

  having particular mechanical properties · CPC title