Axial Turbomachine Compressor Drum with Mixed Blade Fixation
Find Innovative SolutionsGenerate Solutions
Solution Overview
Problem
Axial turbomachine rotors experience vibrations and require complex, costly machining, resulting in a massive and heavy architecture that is difficult to analyze and dampen.
Innovation Solution
The rotor drum features an outer surface with annular ribs for sealing, a π-shaped profile, and blades welded to a raised platform, eliminating freedom of movement between the wall and vanes, and using a one-piece assembly of the first row blades and platform, made from metallic materials like titanium, to enhance rigidity and reduce weight.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Ease of operation
If rotor blades are fixed by feet inserted into annular grooves, then assembly is simple, but vibrations increase and manufacturing becomes complex and costly
Solution Approach 1:
The rotor assembly is segmented into modular components: blades with feet, annular grooves in the drum, and retention rings. This segmentation allows independent manufacturing of each component and simplified assembly, while the grooves and retention mechanisms provide vibration damping without requiring complex integrated machining
Solution Approach 2:
The feet inserted into annular grooves act as intermediary elements between the blades and the drum. These intermediaries provide both mechanical retention and vibration isolation, eliminating the need for complex direct attachment methods while maintaining assembly simplicity
2Ease of operation
If rotor blades are fixed by feet inserted into annular grooves, then assembly is simple, but manufacturing becomes complex and costly
Solution Approach 1:
By dividing the rotor into separate manufacturable components (blades, drum, retention rings) that can be produced using standard machining processes, the overall manufacturing cost is reduced despite the modular assembly requirement
Solution Approach 2:
Instead of machining complex integrated blade attachments directly into the drum, the solution inverts the approach by providing detachable feet that fit into grooves, making both the blades and drum simpler to manufacture individually
3Ease of operation
If rotor blades are fixed by feet inserted into annular grooves, then assembly is simple, but the rotor structure becomes massive and heavy
Solution Approach 1:
The drum structure utilizes thin-walled construction with strategically placed annular grooves and retention rings, replacing massive rigid structures. This allows the rotor to maintain structural integrity and vibration resistance while significantly reducing overall weight
4Ease of operation
If rotor blades are fixed by feet inserted into annular grooves, then assembly is simple, but vibrations increase and are difficult to analyze and dampen
Solution Approach 1:
The annular grooves and retention ring configuration are designed beforehand to provide vibration cushioning. The geometric arrangement of grooves and the compliance of the feet-groove interface inherently dampen vibrations before they can propagate through the rotor structure
Solution Approach 2:
The feet-groove interface, which could be seen as a source of vibration, is designed to convert harmful vibrations into beneficial damping effects through controlled compliance and friction, transforming the potential harm into a vibration reduction mechanism
Data Source
Figure 1~2
Figure 3
AI summary
The invention relates to a rotor drum (40) of a low-pressure axial turbomachine compressor. The drum (40) comprises a wall (42) that is generally symmetrical in revolution about its axis (14) and has a generally curved profile. The wall (42) is configured to support several rows of blades (24, 26, 28). A first row of blades (24) is formed by an annular platform (46) integrally formed with the wall (42) at the apex of its profile relative to the axis (14); and a second row of blades (26), directly downstream of the first (24), and a third row of blades (28), directly upstream of the first (24), are formed by one or more blade retention grooves (54) formed on the wall. The blades of the first row (24) and the drum form a single unit, which eliminates certain vibrations. The blade anchoring is hybrid or mixed. This rotor can be mounted in a housing with rectifiers forming bushings.