System and method for providing integrated antenna
A method for providing an integrated antenna for an aircraft includes identifying a target antenna for an aircraft, identifying a target interior antenna location in the aircraft according to the target antenna, verifying antenna operation, at the target interior antenna location, of the target antenna, mounting the target antenna to a mounting plate, providing a replacement radio transmissive panel (RTP), and attaching the replacement RTP to the aircraft with an exterior surface of the replacement RTP substantially maintaining an outer mold line (OML) of the aircraft, the replacement RTP at least partially covering the target antenna and the mounting plate after the mounting plate is affixed to the aircraft in an antenna cavity associated with the target interior antenna location and after the target antenna is mounted to the mounting plate.
1 . A method, comprising:
identifying a target interior antenna location in an aircraft having a first outer mold line (OML) formed by an exterior skin;
verifying antenna operation, at the target interior antenna location, of a target antenna, wherein the verifying the antenna operation of the target antenna comprises at least one performing a radiation analysis, verifying a range of an antenna in the target interior antenna location meets a minimum threshold, or verifying that transmission angles of an antenna in the target interior antenna location meets a minimum transmission angle threshold;
providing a mounting plate configured to accept mounting of the target antenna;
mounting the target antenna to the mounting plate;
providing a replacement radio transmissive panel (RTP), wherein the replacement RTP has a first outer surface that substantially conforms to a second outer surface of an exterior panel of the exterior skin; and
attaching the replacement RTP to the aircraft with the first outer surface forming a second OML with a portion of the exterior skin, wherein the second OML is substantially the same as the first OML.
2 . The method of claim 1 , further comprising, identifying the target antenna, wherein identifying the target interior antenna location comprises identifying the target interior antenna location according to the target antenna.
3 . The method of claim 2 , wherein the identifying the target antenna comprises identifying an antenna mounted on an exterior of the aircraft for relocation to an interior space.
4 . The method of claim 2 , wherein the identifying the target antenna comprises identifying an antenna mounted in an antenna cavity for replacement with the target antenna.
5 . The method of claim 1 , wherein the replacement RTP is formed from one or more composite layers, wherein each composite layer of the one or more composite layers is a radio-transmissive material.
6 . The method of claim 1 , further comprising affixing the mounting plate to the aircraft in an antenna cavity associated with the target interior antenna location after mounting the target antenna to the mounting plate.
7 . The method of claim 1 , wherein the mounting the target antenna to the mounting plate comprises mounting the target antenna to a sub-plate, and mounting the sub-plate to the mounting plate.
8 . The method of claim 1 , wherein the mounting the target antenna to the mounting plate comprises mounting the target antenna to the mounting plate after the mounting plate is affixed to the aircraft.
9 . The method of claim 1 , wherein the replacement RTP has an edge portion at least partially bounding a body portion, wherein the body portion has a radio transmissive stiffening element and is free of metal features, wherein the body portion is thicker than the edge portion.
10 . A method, comprising:
identifying a target antenna for an aircraft;
identifying a target interior antenna location in the aircraft according to the target antenna;
verifying antenna operation, at the target interior antenna location, of the target antenna;
mounting the target antenna to a mounting plate;
providing a replacement radio transmissive panel (RTP), wherein the replacement RTP has an edge portion at least partially bounding a body portion, wherein the body portion has a radio transmissive stiffening element and is free of metal features, wherein the body portion is thicker than the edge portion; and
attaching the replacement RTP to the aircraft with an exterior surface of the replacement RTP substantially maintaining an outer mold line (OML) of the aircraft, the replacement RTP at least partially covering the target antenna and the mounting plate after the mounting plate is affixed to the aircraft in an antenna cavity associated with the target interior antenna location and after the target antenna is mounted to the mounting plate.
11 . The method of claim 10 , wherein the replacement RTP is formed from one or more composite layers, wherein each composite layer of the one or more composite layers is a radio-transmissive composite material that is selected from a group consisting of an aramid, quartz glass, and fiberglass.
12 . The method of claim 10 , wherein the identifying the target antenna comprises identifying at least one of an antenna mounted on an exterior of the aircraft for relocation to an interior space or an antenna mounted in an antenna cavity for replacement with the target antenna.
13 . The method of claim 10 , wherein the verifying the antenna operation of the target antenna comprises at least one performing a radiation analysis, verifying a range of an antenna in the target interior antenna location meets a minimum threshold, or verifying that transmission angles of an antenna in the target interior antenna location meets a minimum transmission angle threshold.
14 . The method of claim 10 , wherein the mounting plate is attached at a first end to a first support, and is attached at a second end to a second support.
15 . The method of claim 10 , wherein the replacement RTP is one of a stabilizer RTP, an underbody RTP or a body side RTP.
16 . An apparatus, comprising:
a mounting plate affixed in an antenna cavity of an aircraft, wherein the mounting plate is connected to at least two supports of the aircraft, and is recessed from an exterior skin of the aircraft;
a first antenna disposed in the antenna cavity and removably mounted to the mounting plate; and
a replacement radio transmissive panel (RTP), wherein the replacement RTP comprises one or more composite layers, wherein each composite layer of the one or more composite layers is a radio-transmissive material, wherein the replacement RTP is attached to the aircraft with a first outer surface of the replacement RTP substantially conforms to a second outer surface of the exterior skin of the aircraft, wherein at least a portion of the exterior skin of the aircraft adjacent to the replacement RTP comprises a material that is non-transmissive to radio, wherein the replacement RTP at least partially encloses the antenna cavity.
17 . The apparatus of claim 16 , wherein the first antenna is an aerodynamic external antenna.
18 . The apparatus of claim 16 , wherein the replacement RTP is one of a stabilizer RTP, an underbody RTP or a body side RTP.
19 . The apparatus of claim 16 , wherein the mounting plate comprises a removable sub-plate, and wherein the first antenna is removably affixed to the sub-plate.
20 . The apparatus of claim 16 , further comprising a second antenna that is a satellite communications antenna and that is removably mounted to the mounting plate separate from the first antenna, wherein the first antenna is a type of antenna different than the satellite communications antenna.