Systems and methods associated with a removable inlet shield
An inlet shield with a first portion that is configured to be secured to an inlet of a turbocharger, and a second portion that is configured to be removably coupled to the first portion via magnets, wherein different second portions may have different mesh layouts allowing a consumer to choose different levels of protection and air flow based on desired use.
1. An inlet shield system comprising:
a clamping cylinder with an inner circumference that is configured to be positioned around an outer circumference of an air intake of a turbocharger, the clamping cylinder having a clamping inner diameter and a clamping outer diameter, wherein first magnets are positioned on an outer face of the clamping cylinder radially between the clamping inner diameter and the clamping outer diameter;
a first detachable shield with an inner face that is configured to be selectively coupled with the outer face of the clamping cylinder, the first detachable shield having a first guard that covers a first face of the first detachable shield, the first guard occupying a first cross-sectional area, the clamping cylinder having a shield inner diameter and a shield outer diameter, wherein second magnets are positioned on an outer face of the detachable shield radially between the shield inner diameter and the shield outer diameter, wherein a force created by the first magnets and the second magnets to couple the clamping cylinder and the first detachable shield extends in a direction in parallel to airflow through the first detachable shield.
2. The inlet shield system of claim 1 ,
wherein the first magnets have a first polarity and the second magnets have a second polarity.
3. The inlet shield of claim 2 , wherein the clamping cylinder includes a clamp that is configured to apply a radial force against the outer circumference of the air intake.
4. The inlet shield system of claim 1 , further comprising:
an anti-rotation lock formed of castling between depressions and projections positioned on the outer face of the clamping cylinder and the inner face of the first detachable shield, wherein the anti-rotation lock is configured to limit a relative rotation between the clamping cylinder and the first detachable shield.
5. The inlet shield system of claim 1 , wherein the outer face of the clamping cylinder is positioned in front of the air intake of the turbocharger.
6. The inlet shield system of claim 1 , further comprising:
a second detachable shield that is configured to be coupled with the clamping cylinder, the second detachable shield having a second guard that occupies a second cross-sectional area, the first cross-sectional area and the second cross-sectional area being different amounts.
7. The inlet shield system of claim 6 , wherein the clamping cylinder is configured to be secured to the outer circumference of the air intake of the turbocharger when the first detachable shield is decoupled from the clamping cylinder and the second detachable shield is coupled to the clamping cylinder.
8. The inlet shield system of claim 1 , wherein a first diameter extending across the first face of the first detachable shield is larger than a second diameter extending across the air intake of the turbocharger.
9. The inlet shield system of claim 1 , further comprising:
an insulating layer positioned between the inner face of the first detachable shield and the outer face of the clamping cylinder, wherein the insulating layer is affixed to the inner face of the detachable shield.
10. A method for an inlet shield system for an air intake of a turbocharger, the method comprising:
clamping an inner circumference of a clamping cylinder around an outer circumference of the air intake of the turbocharger, wherein the clamping causes a radial force against the outer circumference of the air intake, the clamping cylinder having a clamping inner diameter and a clamping outer diameter, wherein first magnets are positioned on an outer face of the clamping cylinder radially between the clamping inner diameter and the clamping outer diameter;
selectively coupling an inner face of a first detachable shield with the outer face of the clamping cylinder, the first detachable shield having a first guard that covered a first face of the first detachable shield, the first guard occupying a first cross-sectional area, the clamping cylinder having a shield inner diameter and a shield outer diameter, wherein second magnets are positioned on an outer face of the detachable shield radially between the shield inner diameter and the shield outer diameter, wherein a force created by the first magnets and the second magnets to couple the clamping cylinder and the first detachable shield extends in a direction in parallel to airflow through the first detachable shield wherein first magnets are positioned on the outer face of the clamping cylinder and second magnets are positioned on the inner face of the first detachable shield, wherein the first magnets have a first polarity and the second magnets have a second polarity.
11. The method of claim 10 , wherein a force created by the first magnets and the second magnets to couple the cylinder claim and the first detachable shield extends in a direction perpendicular to the radial force of the first clamp.
12. The method of claim 10 , further comprising:
forming an anti-rotation lock via castling between depressions and projections positioned on the outer face of the clamping cylinder and the inner face of the first detachable shield, wherein the anti-rotation lock is configured to limit a relative rotation between the clamping cylinder and the first detachable shield.
13. The method of claim 10 , wherein the outer face of the clamping cylinder is positioned in front of the air intake of the turbocharger.
14. The method of claim 10 , further comprising:
decoupling the first detachable shield from the clamping cylinder;
coupling a second detachable shield that to the clamping cylinder, the second detachable shield has a second guard that occupies a second cross-sectional area, the first cross-sectional area and the second cross-sectional area being different amounts, wherein the clamping cylinder is configured to be secured to the outer circumference of the air intake of the turbocharger when the first detachable shield is decoupled from the clamping cylinder and the second detachable shield is coupled to the clamping cylinder.