Patent Application
20160033040
This application relates to relatively rigid fluid barriers and methods of repairing and manufacturing the barriers by applying flexible backing material.
Gas turbine engines are known and include a plurality of distinct components. Various fluids move within a gas turbine engine, and it is desirable to provide barriers to prevent the fluids from reaching certain areas. One type of barrier is an air-oil seal, which separates an air holding chamber from an area that might hold oil. One known air-oil seal includes a relatively rigid plate fabricated from fiberglass, and perhaps other materials such as epoxy.
The rigid plate may become saturated with oil during operation. Moreover, the plate may crack and develop a plurality of small fractures, which may allow air or oil to pass through walls of the barrier. In the past, there has been no good known method to repair the barrier. As a result, entire replacement of the air-oil seal was performed to replace the defective barrier. Because the air-oil seals are relatively expensive, cheaper methods of repairing the barriers for further use would be desirable. It is also desirable to manufacture the air-oil seals that extend service life without repair.
Various methods for cleaning and performing maintenance steps on air-oil seals are disclosed in patent applications such as U.S. application Ser. No. 11/862,584, filed on Sep. 27, 2007, and titled “Pressurized Cleaning of a Turbine Engine Component,” or, alternatively, patent application Ser. No. 11/396,479, filed on Apr. 3, 2006, titled “Metallic Doubler Repair of Composite Arcuate Flanges,” which is U.S. Published Application 2007/0240819A1. Also, the last mentioned application has a related continuation-in-part application Ser. No. 11/897,887, filed Aug. 31, 2007, which is U.S. Published Application 2008/0000193.
In a method of repair, a relatively rigid component is restored by application of a thermosetting resin placed over the component, at least on the areas including fractures, and then a relatively flexible material is placed outwardly of the thermosetting resin.
Also, a barrier can be manufactured as a new component with a flexible fluoroelastomer backing material.
In another feature of this application, a method of forming a barrier includes providing a composite material, and applying a relatively flexible material on a surface of the composite material, and concurrently molding the relatively flexible material with the composite material using a composite mold.
These and other features of the present invention can be best understood from the following specification and drawings, the following of which is a brief description.
Failure of the air-oil seal 20 is first observed by an inability to act as a barrier between fluids. Although the plate 22 may retain sufficient structure such that it will not burst, an additional mechanism in the exemplary embodiment may be installed either at original manufacture or subsequent to manufacture in order to maintain the barrier performance in service.
The plate 22 has an internal aperture 23, which surrounds a shaft in a gas turbine engine when assembled in the engine. During engine operation, the material of plate 22 may become saturated with oil. Additionally the matrix material of the plate 22 may swell, craze or crack such that the plate 22 is no longer able to effectively function as a barrier between air and oil without assistance of an additional compliant feature that will bridge the defects.
One exemplary method of testing the integrity of the air-oil seal plate 22 is described with respect to exemplary testing stand illustrated in
The fractures may occur as a number of smaller fractures spaced across a larger area, such as fractures 60 as shown in
In the exemplary embodiment, and as shown for instance in
The resin layer is compatible with the component substrate of the air-oil seal 20 and durable in the operating environment of the component. Typical resins are either epoxy or BMI materials, but some component matrix materials may include different resins, usually similar to the matrix material.
Although the exemplary embodiment is shown for repairing an air-oil seal, it should be appreciated that exemplary repair method may be utilized to repair other fluid seals.
An analogous flexible material layer 32 may be installed to the component substrate prior to the seal entering service. Although the layer may be installed in a manner as described above for repair, the seal is already clean and does not require a resin coat.
A more cost effective manufacturing method for installing the flexible layer would be to concurrently mold the flexible material layer with the molding of composite material of the air-seal as shown in
Although exemplary embodiments have been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
This application is a divisional of prior U.S. application Ser. No. 12/054,462, filed Mar. 25, 2008, the entirety of which is herein incorporated by reference.
| Number | Date | Country | |
|---|---|---|---|
| Parent | 12054462 | Mar 2008 | US |
| Child | 14689133 | US |
