System for attaching heat generating equipment to an exterior of an aircraft
A system and method for attaching heat generating equipment to an exterior of an aircraft. The mounting system comprises a heat chamber formed by a number of conductive materials, the heat chamber having a recess open to an environment outside the aircraft, heat generating equipment secured within the recess, and a layer of insulation between the heat chamber and the aircraft, the layer of insulation positioned on an opposite side of the heat chamber than an opening of the recess.
1. A mounting system for attaching heat generating equipment to an exterior of an aircraft, the mounting system comprising:
a heat chamber formed by a number of conductive materials, wherein the heat chamber has a recess open to an environment outside the aircraft, wherein the heat chamber comprises a shroud and a subplate, and wherein the subplate is a unitary metal structure;
heat generating equipment secured within the recess;
a layer of insulation between the heat chamber and the aircraft, wherein the layer of insulation is positioned on an opposite side of the heat chamber than an opening of the recess; and
a skirt seal connected to a lower ring of the shroud; and
a thermal isolator positioned between the lower ring and a skin of the aircraft.
2. The mounting system of claim 1 , wherein the heat generating equipment comprises a number of electronic antennas.
3. The mounting system of claim 1 , wherein the shroud comprises a plurality of portions secured together.
4. The mounting system of claim 1 , wherein the subplate comprises the recess and a flange surrounding the recess.
5. The mounting system of claim 4 , wherein the flange of the subplate is secured to the shroud.
6. The mounting system of claim 1 , further comprising:
a number of thermal isolators positioned between the heat chamber and the aircraft.
7. The mounting system of claim 1 , wherein the subplate is formed of aluminum.
8. The mounting system of claim 1 , wherein the shroud is formed of a conductive material.
9. The mounting system of claim 1 , wherein the shroud provides lightning protection.
10. A mounting system for attaching heat generating equipment to an exterior of an aircraft, the mounting system comprising:
a subplate having a recess surrounded by a flange, wherein the subplate is formed of a unitary metal;
heat generating equipment positioned within the recess;
a layer of insulation secured to a backside of the subplate;
an adapter plate configured to connect components to a skin of the aircraft; and
fittings connecting the subplate to the adapter plate.
11. The mounting system of claim 10 , wherein the heat generating equipment comprises a number of electronic antennas.
12. The mounting system of claim 10 , wherein a number of thermal isolators is positioned between the subplate and the adapter plate.
13. The mounting system of claim 10 , further comprising:
a shroud comprising a plurality of portions secured together, wherein the shroud is formed of a conductive material and configured to provide an aerodynamic design.
14. The mounting system of claim 13 , wherein the plurality of portions of the shroud comprises a skin and access panels, wherein the skin is secured to an adapter plate configured to connect components to a skin of the aircraft, and wherein the access panels are designed to accommodate cross-sectional shapes of the heat generating equipment.
15. The mounting system of claim 13 , wherein a number of thermal isolators is positioned between the shroud and a skin of the aircraft.
16. The mounting system of claim 10 , wherein the subplate is formed of aluminum.
17. A method of attaching heat generating equipment to an exterior of an aircraft, the method comprising:
positioning a layer of insulation between the heat generating equipment and a skin of a fuselage of the aircraft; and
securing a shroud over the layer of insulation to form a heat chamber between the layer of insulation and an outside environment;
wherein said securing the shroud comprises connecting a skin of the shroud to an adapter plate secured to the fuselage, wherein said securing the shroud further comprises connecting access panels of the shroud to a subplate holding the heat generating equipment, and wherein the subplate is a unitary metal structure which forms the heat chamber with the shroud.
18. The method of claim 17 , wherein said positioning the layer of insulation comprises connecting a fabricated antenna assembly comprising the layer of insulation, a subplate, and a number of electronic antennas to the fuselage.
19. The method of claim 18 , wherein said connecting the fabricated antenna assembly to the fuselage comprises connecting the fabricated antenna assembly to an adapter plate secured to the fuselage.
20. The method of claim 17 , wherein said securing the shroud comprises:
assembling a plurality of portions of the shroud; and
securing the plurality of portions to the adapter plate secured to the fuselage and to the subplate holding the heat generating equipment.