Carbon Face Seal Geometry to Limit Dynamic Seal Instability
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Carbon face seals in gas turbine engines are prone to dynamic instability, leading to coupled radial and axial displacements that result in leaks, rapid wear, and premature failure due to excessive stresses beyond the capability of the spring element.
Innovation Solution
The solution involves a radial gap formed between the outer diameter surface of the seal and the inner diameter surface of the seat, with specific geometric features such as a chamfer surface and axial undercut, which help to limit dynamic radial excursions and prevent axial separation.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Reliability
If the carbon seal is axially spring biased into engagement with the seat to maintain sealing contact, then sealing effectiveness is improved, but dynamic instability leading to coupled axial and radial displacements causes premature failure
Solution Approach 1:
The invention introduces a radial dimension constraint by providing a radial stop surface that limits radial displacement of the seal. This adds a radial constraint dimension to the existing axial spring bias, creating a two-dimensional constraint system that prevents the coupled radial-axial dynamic instability while maintaining axial sealing contact.
Solution Approach 2:
The radial stop surface acts as an intermediary element between the seal and the seat structure. It mediates the radial displacement by providing a physical barrier that limits radial movement without interfering with the axial spring bias mechanism, thereby decoupling the radial and axial motion constraints.
2Adaptability or versatility
If the seal is allowed radial movement to accommodate dynamic conditions, then adaptability is improved, but coupled radial and axial displacements lead to leaks and rapid wear
Solution Approach 1:
The radial stop surface introduces a radial constraint dimension that works alongside the axial spring bias. This creates a controlled two-dimensional movement envelope that allows necessary radial accommodation while preventing the excessive coupled displacements that lead to sealing failures.
Solution Approach 2:
The invention changes the displacement parameters by limiting the radial displacement magnitude through the radial stop surface. This parameter control ensures that radial movements remain within acceptable bounds that prevent coupled axial displacements and maintain sealing integrity under dynamic conditions.
3Strength
If the spring element is designed to handle high stresses from dynamic instability, then durability is improved, but the spring element still fails under extreme coupled displacements
Solution Approach 1:
The radial stop surface provides preliminary anti-action by preventing the radial displacement that would lead to coupled axial displacements. This preemptive constraint stops the instability mechanism before it can generate excessive stresses that would overwhelm the spring element's capacity.
Solution Approach 2:
The radial stop surface acts as a protective constraint that cushions against the development of dynamic instability. By limiting radial movement in advance, it prevents the chain of events that would lead to coupled displacements and spring element failure, effectively cushioning the system against premature failure.
Applied Scientific Principles
This section explains which scientific principles are used to turn an abstract innovation direction into a practical engineering solution.
Function Achieved in This Case
This configuration effectively limits coupled dynamic displacements, preventing leaks and reducing wear and stress on the seal, thereby extending its operational life and maintaining the structural integrity of the gas turbine engine.
Implementation Method 1
The seal is mounted to a first structure and biased into engagement with a seat by a bellows spring
Implementation Method 2
The sliding engagement causes frictional heating. The heat must be dissipated.
Implementation Method 3
oil cooled carbon seals are divided into two categories: 'dry face' seals wherein the oil passes through passageways in the seat without encountering the interface between seal face and seat face; and 'wet face' seals wherein the oil passes through the seat to the interface so that the oil that flows through the seat cools the seat
Implementation Method 4
oil cooled carbon seals are divided into two categories: 'dry face' seals wherein the oil passes through passageways in the seat without encountering the interface between seal face and seat face
Data Source
Figure 1
Figure 1A
Figure 2
AI summary
An apparatus has a first member (36), a shaft (40, 50) rotatable relative to the first member (36) about an axis (A), and a seal system (100). The seal system (100) has: a seal (102) carried by the first member (36) and having a seal face (106); and a seat (104) carried by the shaft (40, 50) and having a seat face (108) in sliding sealing engagement with the seal face (106). The seal system (100) is a dry face seal system. The seat (104) further includes a seat section (210) having: an outer diameter surface (216) encircled by the seal (102); and a rim (212).