Method for processing variable section channel of hall thruster
A technology of a Hall thruster and a processing method, which is applied to thrust reversers, machines/engines, using plasma, etc., to achieve the effects of extending working life, improving corrosion conditions and long life
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specific Embodiment approach 1
[0011] Embodiment 1: Combining figure 1 and Image 6 Describe this embodiment, the processing method of the variable cross-section channel of the Hall thruster described in this embodiment, which includes the following specific steps:
[0012] Step 1. Carry out the ignition operation of the Hall thruster, and measure the curve of the wall normal erosion velocity c of the discharge channel of the Hall thruster during the time period from the ignition of the engine to the time when the engine cannot be re-ignited;
[0013] Step 2: Obtain the normal erosion velocity c of the wall at different times through simulation and calculation, and establish a one-to-one correspondence data relationship between the normal erosion velocity c and the topography of the wall;
[0014] Step 3: From the curve of the wall normal erosion velocity c obtained in step 1 and the one-to-one correspondence data relationship between the normal erosion velocity c obtained in step 2 and the wall surface t...
specific Embodiment approach 2
[0016] Specific embodiment 2: This embodiment is a further limitation of the processing method of the variable cross-section channel of the Hall thruster described in the first embodiment. The process of establishing the one-to-one correspondence between the normal erosion velocity c and the wall surface topography is as follows: :
[0017] The wall material of the discharge channel of the Hall thruster is continuously peeled off under the action of ion sputtering erosion, and the surface topography continues to evolve during the erosion process, such as Image 6 shown.
[0018] θ=arccos(n·n′) is the angle formed by the ion incident direction and the surface normal direction, n is the unit vector of the surface normal, n′ is the unit vector pointing to the ion beam incident direction; the normal erosion velocity of the surface c is represented as:
[0019] c=qn (1)
[0020] where q is the sputter erosion rate, which is expressed as:
[0021] q = ...
specific Embodiment approach 3
[0023] Embodiment 3: This embodiment further defines the processing method of the variable cross-section channel of the Hall thruster described in Embodiment 2. The sputtering yield Y(E, θ) is:
[0024] Y(E, θ)=Y′(θ)·Y′(E) (3)
[0025] In the formula, Y'(E) is the energy sputtering yield, and Y'(θ) is the angle sputtering yield;
[0026] at this time,
[0027] q = J i · Y ′ ( E ) N · Y ′ ( θ ) · cos θ - - - ( 4 )
[0028] and get:
[0029] c = qn = n ...
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