High-viscosity sealant application system

1. An apparatus comprising:

a structure, wherein the structure is selected from one of a workpiece, an assembly of components, and a sub-assembly;

a robotic attachment element configured for attachment to a robotic device, wherein the robotic device is configured to move the nozzle system relative to the structure such that the sealant material is applied with a desired level of consistency and accuracy;

a source attachment element configured for attachment to a source holding a sealant material having a viscosity greater than a selected threshold of about 100,000 centipoise; and

a nozzle system positioned at least 1.0 inches away from the structure during application of the sealant material onto the structure and configured to apply the sealant material onto the structure in a number of streams to form a sealant deposit having a desired shape wherein the desired shape of the sealant deposit is a bead having a substantially uniform thickness and width along a length of the bead, wherein the nozzle system is configured to apply the sealant material onto the structure in one of a monostream mode and a multistream mode using a selected application pattern, wherein the selected application pattern is a swirl pattern;

the nozzle system having a temperature controlling element configured to alter a temperature of the sealant material flowing through the nozzle system to change the viscosity of the sealant material to control an exit velocity of the sealant material.

2. The apparatus of claim 1 , wherein the nozzle system is configured to apply the sealant material in the number of streams over a number of features of the structure such that the sealant deposit cures to form a seal over the number of features having the desired shape.

3. The apparatus of claim 2 , wherein a feature in the number of features is selected from one of a joint, a fastener element, an end of a fastener element, an interface between one or more components, a groove, and a seam.

4. The apparatus of claim 3 , wherein the structure comprises a number of components for an aerospace vehicle.

5. The apparatus of claim 4 , wherein the robotic attachment element, the source attachment element, and the nozzle system form a sealant material application system.

6. The apparatus of claim 5 , wherein the sealant material that is applied onto the structure is cured to form a seal having a rigid surface and the desired shape within selected tolerances.

7. The apparatus of claim 6 , wherein the sealant material application system is an end effector for the robotic device.

8. The apparatus of claim 6 , wherein the source is a sealant cartridge.

9. A sealant material application system comprising:

a structure for an aerospace vehicle, wherein the structure is selected from one of a workpiece, an assembly of components, and a sub-assembly;

a robotic attachment element configured for use in attaching the sealant material application system to a robotic device;

a source holding a multi-component sealant material having a viscosity greater than about 100,000 centipoise;

a source attachment element configured to attach the sealant material application system to the source;

a nozzle system positioned at least 1.0 inches away from the structure and configured to eject the sealant material at a pressure greater than 500 pounds per square inch in a swirl pattern over a number of features of the structure in a number of streams with a desired level of consistency and accuracy to form a sealant deposit having a substantially uniform thickness and width along the length of the bead in which the sealant deposit is cured to form a seal having a rigid surface over the number of features, wherein the thickness of the sealant deposit is controlled by controlling a translational speed of the nozzle system; and

a temperature controlling element associated with the nozzle system and configured to control a temperature of the sealant material flowing through the nozzle system to change the viscosity of the sealant material within selected tolerances in order to achieve a desired exit velocity.