Turbopump Magnetic Torque Generator for Intermediate Regime Control
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Solution Overview
Problem
Conventional turbopump control systems struggle to maintain stable operation between the standby and nominal regimes, often converging to either regime due to thermodynamic energy inputs, lacking a controlled transition between them.
Innovation Solution
Incorporation of a magnetic torque generator that selectively applies torque to the drive shaft, allowing for precise control through a control unit and magnetic poles on the stator and rotor, enabling the generation of a radial or axial flux, and providing a bearing function to stabilize the drive shaft.
Engineering Contradictions & Design Principles
Engineering Contradiction Analysis
1Adaptability or versatility
If conventional control methods (flow restriction or speed control) are used, then the turbopump can operate in nominal regime R3, but it cannot maintain stable operation in intermediate regimes between standby R2 and nominal R3
Solution Approach 1:
The patent replaces conventional mechanical control systems (flow restriction valves, mechanical governors) with a magnetic torque generator that uses electromagnetic fields to apply controlled torque to the drive shaft. This substitution enables precise torque control in intermediate operating regimes where conventional mechanical controls cannot maintain stability, allowing the turbopump to operate stably between standby and nominal regimes without converging to extreme states.
2Speed
If energy input is increased to transition from standby to nominal regime, then the turbopump reaches nominal speed R3, but it tends to converge to nominal regime or remain in standby without controlled intermediate operation
Solution Approach 1:
The patent implements a control system that continuously monitors the turbopump's operating state and adjusts the magnetic torque generator's output accordingly. This feedback mechanism enables precise control of the transition between standby and nominal regimes by applying appropriate torque to counteract thermodynamic energy inputs that would otherwise cause convergence to nominal regime, allowing stable operation at intermediate speeds.
3Adaptability or versatility
If magnetic torque generator is added to enable controlled transition, then intermediate stable regimes are achieved, but device complexity increases
Solution Approach 1:
The magnetic torque generator is designed to perform multiple functions: it provides controlled torque for regime transitions, acts as a magnetic bearing to support the drive shaft, and enables precise speed control in intermediate regimes. By consolidating these functions into a single integrated component rather than adding separate mechanical controls, the patent reduces overall system complexity while achieving superior adaptability.
4Reliability
If magnetic holding field is generated to perform bearing function, then wear is reduced by preventing contact, but energy consumption increases
Solution Approach 1:
The magnetic torque generator utilizes the same electromagnetic field mechanism to provide both torque control and bearing support functions. The magnetic field that generates torque also creates the holding effect that prevents drive shaft contact with mechanical bearings, reducing wear. This self-service approach eliminates the need for separate magnetic bearing systems, thereby avoiding additional energy consumption that would result from redundant systems.
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 solution enables an additional stable speed between the nominal and standby regimes, improving transition efficiency and reducing energy consumption, while also facilitating controlled propellant circulation and precise starting sequences, and reducing wear by generating a repulsive field to prevent contact between the drive shaft and stator.
Implementation Method 1
a magnetic torque generator configured to selectively apply torque to the drive shaft
Implementation Method 2
The magnetic torque generator can be configured so as to establish a radial holding magnetic field of the drive shaft and thus perform a bearing function
Implementation Method 3
Said holding magnetic field is for example a repulsive field, configured to hold the drive shaft spaced from the stator of the turbopump
Data Source
Figure 1~3
AI summary
Spacecraft turbopump (1) comprising - a fixed assembly defining a stator of the turbopump (1), and - a moving assembly defining a rotor of the turbopump, comprising a drive shaft (2), - a magnetic torque generator (5) configured to selectively apply a torque on the drive shaft (2), the turbopump (1) having two disjoint stable operating regimes (R2, R3), characterized in that it further comprises a control unit (6), configured to drive the magnetic torque generator (5) in order to selectively apply a driving or resisting torque on the drive shaft (2) according to an applied command, so as to define an intermediate stable regime (R3) between said two disjoint stable operating regimes (R2, R3).