Electrical power feed thru for aircraft fuselages
An electrical power feed thru for thin-walled vessels such as aircraft fuselages is disclosed which allows high electrical current power lines, and their associated high operating temperatures, to transition from the inside to the outside of the aircraft. The feed thru includes sealing surfaces, anti-rotation features and safety covers. This low-profile configuration permits the attached cables to run close to the fuselage walls, permitting easier routing and clamping. The feed thru has a variable geometry which permits alternate spacing of the end terminations in reference to the fuselage while maintaining the same parts. Installation is simplified through a single fuselage wall mounting hole design that can be done with a standard punch. The feed thru exceeds the shock and vibration environments of various aircraft such as a military aircraft.
1. An electrical power feed thru for a thin-walled vessel comprising: an electrically conductive bus bolt structured and arranged to extend along an axis through a wall of the vessel; an outside wall insulator surrounding a first portion of the bus bolt structured and arranged for installation adjacent to an exterior surface of the wall; and an inside wall insulator surrounding a second portion of the bus bolt structured and arranged for installation adjacent to an interior surface of the wall, wherein the electrically conductive bus bolt is prevented from rotating around the axis with respect to the outside wall insulator and the inside wall insulator, and wherein the outside and inside wall insulators are shaped to prevent rotation around the axis with respect to each other.
2. The electrical power feed thru of claim 1 , wherein the electrically conductive bus bolt comprises a hex head received within a corresponding hex indentation in either the outside or inside wall insulator.
3. The electrical power feed thru of claim 1 , wherein the electrically conductive bus bolt comprises a threaded end and a nut is secured on the threaded end.
4. The electrical power feed thru of claim 1 , wherein one of the outside and inside wall insulators has an axially extended portion and the other one of the outside and inside wall insulators has an axially recessed portion which receives the extended portion to prevent said rotation.
5. The electrical power feed thru of claim 1 , wherein at least one of the outside and inside wall insulators contacts the wall of the vessel.
6. The electrical power feed thru of claim 5 , wherein the at least one of the outside and inside wall insulators forms a seal against the wall of the vessel.
7. The electrical power feed thru of claim 1 , wherein at least one end of the electrically conductive bus bolt comprises a tapped hole which receives a threaded bolt for securing an electrical cable connector to the bus bolt.
8. The electrical power feed thru of claim 7 , wherein the electrical cable connector extends from the bus bolt in a direction substantially perpendicular to an axial direction of the bus bolt.
9. The electrical power feed thru of claim 1 , further comprising:
an exterior cable connector extending from one end of the bus bolt; and
an interior cable connector extending from another end of the bus bolt.
10. The electrical power feed thru of claim 9 , wherein the cable connectors extend from the bus bolt in directions substantially perpendicular to an axial direction of the bus bolt.
11. The electrical power feed thru of claim 1 , further comprising a locator insulator surrounding a third portion of the bus bolt positioned between the outside and inside wall insulators.
12. The electrical power feed thru of claim 11 , wherein the locator insulator has at least one axially extended portion received within a corresponding axially recessed portion of either the outside or inside wall insulator to prevent rotation of the locator insulator with respect to the outside or inside wall insulator.
13. The electrical power feed thru of claim 11 , wherein the locator insulator has at least one axially recessed portion which receives a corresponding axially extended portion of either the outside or inside wall insulator to prevent rotation of the locator insulator with respect to the outside or inside wall insulator.
14. The electrical power feed thru of claim 11 , wherein the locator insulator contacts the wall of the vessel.
15. The electrical power feed thru of claim 1 , further comprising:
an outside insulating cover adjacent to one end of the bus bolt; and
an inside insulating cover adjacent to another end of the bus bolt.
16. The electrical power feed thru of claim 15 , wherein the outside insulating cover is mounted on the outside wall insulator, and the inside insulating cover is mounted on the inside wall insulator.
17. The electrical power feed thru of claim 1 , wherein the thin walled vessel comprises an aircraft fuselage.
18. The electrical power feed thru of claim 17 , wherein the aircraft fuselage is pressurized.