Motor air flow cooling
In one possible embodiment, an aircraft electric motor cooling system is provided having an airflow path through a spinner which includes a first airflow path between an inner rotor and a stator, a second airflow path between an outer rotor the stator and a third airflow path along an outer surface of the outer rotor.
1. A method for air cooling an electric aircraft motor comprising:
a) passing an air flow through a spinner;
b) directing a first portion of the air flow to flow between a stator and an inner rotor such that the first portion extends between and along inner rotor magnets and one side of a stator coil;
c) directing a second portion of the air flow to flow between the stator and an outer rotor, such that the second portion extends between and along outer rotor magnets and an other side of the stator coil;
d) directing a third portion of the air flow to flow along an outer surface of the outer rotor; and
e) directing a front cooling fin portion of the air flow through front stator cooling fins, and wherein the second and third portion are derived at least in part from the cooling fin portion of the air flow through the spinner.
2. The method of claim 1 , wherein the first portion flows along inner rotor magnets.
3. The method of claim 2 , wherein the second portion of the air flow flows along outer rotor magnets.
4. The method of claim 2 , wherein the first portion flows along a front stator yoke and along a rear stator yoke.
5. The method of claim 1 , wherein the second portion of the air flow flows along outer rotor magnets.
6. The method of claim 5 , wherein the second portion flows along a front stator yoke and a rear stator yoke.
7. The method of claim 1 , further comprising returning the first, second, and third portions of the air flow to an air stream.
8. An electric aircraft motor comprising:
a) an inner rotor connected with an outer rotor;
b) a stator comprising a winding located between the inner rotor and the outer rotor;
c) a spinner;
d) a cooling system comprising:
i) an airflow path through the spinner comprising:
(1) a first airflow path between an inner rotor and a stator; and
(2) a second airflow path between an outer rotor the stator; and
e) rear cooling fins thermally coupled to a rear portion of the stator, the rear cooling fins extending beyond an outer radius of the spinner.
9. The motor of claim 8 , further comprising
the airflow path through the spinner extending through the rear cooling fins.
10. The motor of claim 8 , wherein the first airflow path extends along inner rotor magnets, and wherein the second airflow path extends along outer rotor magnets.
11. The motor of claim 8 , wherein the first airflow path extends along a front stator yoke and along a rear stator yoke.
12. The motor of claim 8 , wherein the second airflow path extends along a front stator yoke and a rear stator yoke.
13. A method for air cooling an electric aircraft motor comprising:
a) passing an air flow through a spinner;
b) directing a first portion of the air flow to flow between a stator and an inner rotor;
c) directing a second portion of the air flow to flow between the stator and an outer rotor;
d) directing a third portion of the air flow to flow along an outer surface of the outer rotor;
e) directing a front cooling fin portion of the air flow through front stator cooling fins, and wherein the second and third portion are derived at least in part from the cooling fin portion of the air flow through the spinner; and
f) returning the first portion, the second portion, and the third portion of the air flow to an air stream.