IR absorbing coatings comprising fluorinated nanoparticles
09951232 ยท 2018-04-24
Assignee
Inventors
- Larken E. Euliss (Calabasas, CA, US)
- Brett Nosho (Santa Monica, CA, US)
- Nicole L. Abueg (Seattle, WA)
- G. Michael Granger (Redmond, WA, US)
- Peter D. Brewer (Westlake Village, CA, US)
- Maryam Behroozi (Woodland Hills, CA, US)
Cpc classification
Y10T428/24612
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B64G1/226
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/24628
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
Y10T428/2438
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
B82Y15/00
PERFORMING OPERATIONS; TRANSPORTING
C08K3/30
CHEMISTRY; METALLURGY
B64D47/00
PERFORMING OPERATIONS; TRANSPORTING
Y10T428/254
GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
International classification
B64D47/00
PERFORMING OPERATIONS; TRANSPORTING
B82Y15/00
PERFORMING OPERATIONS; TRANSPORTING
C08K3/30
CHEMISTRY; METALLURGY
C09D5/00
CHEMISTRY; METALLURGY
Abstract
The present disclosure relates to solution processed nanomaterials, and methods for their manufacture, with activity in the infrared (IR) region for a variety of commercial and defense applications, including conformal large-area IR coatings, devices and pigments that necessitate an absorption band edge in the MWIR or LWIR.
Claims
1. An infrared-absorbing coating material comprising: a fluorinated resin comprising quantum nanoparticles, said quantum nanoparticles consisting of SnTe quantum nanoparticles, said SnTe quantum nanoparticles embedded into the fluorinated resin; wherein the quantum nanoparticles comprise at least partially fluorinated surface ligands; wherein the infrared-absorbing coating material absorbs infrared bandwidth from about 3 m to about 15 m; and wherein the infrared-absorbing coating material is configured to provide a substantially conformal coating including uniform infrared absorption on an exterior of an atmospheric vehicle or a space vehicle.
2. A base material comprising an infrared-absorbing coating material, said base material comprising: an external surface of an atmospheric vehicle or space vehicle, said infrared-absorbing coating material comprising: fluorinated resin quantum nanoparticles, said quantum nanoparticles consisting of SnTe quantum nanoparticles; wherein the SnTe quantum nanoparticles comprise at least partially fluorinated surfaces ligands, wherein the SnTe quantum nanoparticles are embedded into the fluorinated resin; and wherein the infrared-absorbing coating material absorbs infrared bandwidth from about 3 m to about 15 m; and wherein the infrared-absorbing coating material is configured to provide a substantially conformal coating including uniform infrared absorption.
3. The base material of claim 2, wherein the quantum nanoparticles comprise particles selected from the group consisting of: quantum dots, tetrapods, nanorods, cubes, and combinations thereof.
4. The base material of claim 2, wherein the quantum nanoparticles comprise quantum dots.
5. The base material of claim 2, wherein the quantum dot nanoparticles have an average diameter of from about 2 nm to about 100 nm.
6. The base material of claim 2, wherein the infrared absorbing coating material absorbs mid-wavelength infrared bandwidth from about 3 m to about 5 m.
7. The base material of claim 2, wherein the infrared absorbing coating material absorbs long-wavelength infrared bandwidth from about 6 m to about 15 m.
8. The base material of claim 2, wherein the base material comprises at least one area selected from the group consisting of: a flat surface, a compound contour surface, a curved surface, and combinations thereof.
9. The infrared-absorbing coating material of claim 1, wherein the coating material is delivered to the exterior as a spray.
10. The base material of claim 2, wherein the coating material is delivered to a surface as a spray.
Description
BRIEF DESCRIPTION OF THE DRAWING(S)
(1) Having thus described variations of the disclosure in general terms, reference will now be made to the accompanying drawings, which are not necessarily drawn to scale, and wherein:
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DETAILED DESCRIPTION
(7) The present invention will be described more fully hereinafter with reference to the accompanying drawings, where preferred alternatives are shown. The disclosures may, however, be embodied in many different forms and should not be construed as limited to the examples set forth. Rather, these examples are provided so that this disclosure will convey the scope of the inventions to those skilled in the field. Like numbers refer to like elements throughout.
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(10) As shown schematically in
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EXAMPLE 1
(13) Synthesis of SnTe Quantum Dot nanoparticles
(14) SnTe quantum dot nanoparticles were synthesized with stabilizing ligands on the surface of the nanoparticles. Bis[bis(trimethylsilyl)amino] tin (II) was combined with 1-octadecene (ODE, 90%), oleic acid (OA, 90%), trioctylphosphine (TOP, 90%) oleylamine (OLA, 70%) and tellurium powder (98.99%). The aforelisted chemicals were obtained from Aldrich (St. Louis, Mo.). ODE was vacuum dried at 140 C. for 2 hours and stored in an argon-filled glove box with bis[bis(trimethylsilyl)amino] tin (II), TOP and the tellurium (Te) powder. A 10 wt % solution of Te in TOP was prepared in a glove box by dissolving elemental Te in TOP at 200 C. for 6 hours. Monodispersed SnTe quantum dots were obtained using 90% purity TOP. The steps in the SnTe quantum dot synthesis were carried out in a glove box or on a vacuum/argon gas Schlenck line. Prior to synthesis, a tin precursor was formed in a glove box by dissolving 0.16 ml (0.4 mmol) of bis[bis(trimethylsilyl)amino] tin (II) in 6 ml of dry ODE. This solution was loaded into a 20 ml syringe with an 18 gauge needle and sealed in a 1 liter Nalgene bottle to prevent oxidation when the syringe was moved out of the glove box. Additionally, 1 ml of the Te in TOP solution (0.73 mmol) was loaded into a syringe. Next, a 3-neck 100 ml flask with a condenser column and septa on the side necks was attached to the Schlenk line. A solution (14 ml) comprising a mixture of OLA and ODE was placed into the flask and vacuum dried at 100 C. for one hour (20 or 70% OLA). The flask was then backfilled with argon and the syringe with 1 ml of Te in TOP was injected thereto. The reaction temperature was raised to 150 C. and the tin precursor syringe was removed from the Nalgene bottle and the contents were injected quickly into flask with the contents rapidly stirred. The temperature of the contents of the flask was allowed to drop to 30 to 40 C. after injection with the higher temperature maintained for 90 seconds. The heating mantle was removed and the reaction was allowed to cool to room temperature. Next, 3 ml of OA was injected to the cooled mixture, followed by adding 10 ml of 1:1 chloroform:acetone mixture, followed by an additional amount of acetone to cause precipitation of the quantum dot nanoparticles. The mixture was then centrifuged to separate the SnTe nanocrystals. The supernatant was poured off, and the nanocrystals were redissolved in chloroform or acetone. The precipitation, centrifugation and redissolution of SnTe were performed three times to increase nanocrystal purity.
EXAMPLE 2
(15) Interchanging Surface Ligands into Fluorinated Ligands
(16) SnTe quantum dot nanoparticles were prepared as stated in Example 1. An amount of 50 mg of the original SnTe dots (with oleic acid (OA) stabilizing ligands) were dissolved in 5 ml of dichloromethane with 200 mg of perfluorodecanoic acid and 200 mg of 1H, 1H, 2H, 2H perfluorodecane thiol. The mixture was purged with nitrogen and heated for 2 days at 40 C. in a closed 2-neck flask. The dichloromethane was removed and the free ligands were removed by washing out with acetone two times. The resulting quantum dot nanoparticles were redispensed in the following solvents: hexafluorobezene, pentafluorothiophenol, trifluorotoluene, and tetrafluorohexane. Verification of the successful ligand exchange was done by checking the ATR absorption. A reduction in the absorbance of the CH peak and a new CF absorption peak was observed. See
EXAMPLE 3
(17) Spraying or Dip Coating the Resin Mixture Comprising the Quantum Dot Nanoparticles with Fluorinated Ligands
(18) An amount of 50 mg of fluorinated quantum dot nanoparticles was dispersed in 5 ml of solvent (hexafluorobenzene) and 2 ml of fluorinated resin in a 1.5 g:0.5 g ratio. The mixture was cast in a Teflon mold and cured at room temperature. The quantum dot nanoparticle/fluorinated resin was allowed to cure for 48 hours. A 2.5% mixture of modified quantum dot nanoparticles in the fluorinated resin was obtained. The mixture was spray-coated, using an Iwata High Performance Plus HP-BC1 spraying gun. The spray gun used can be any spray gun used to apply paint or coatings over a large area (greater than about, for example, one inch). The fluorinated resin was then sprayed onto an aluminum coupon and cured at room temperature. The quantum dot nanoparticle/fluorinated resin coating was allowed to cure for 48 hours.
(19) Although most examples here have discussed usefulness of the IR absorbing nanomaterial distributed within the fluorinated resin to be positioned on the exterior or interior of atmospheric and aerospace vehicles and other objects and structures designed for use in space or other upper-atmosphere environments, further uses abound where IR absorption would be useful, including, for example, manned or unmanned operation of objects and structures in an atmospheric or space environment. Contemplated objects include structures and vehicles, such as, for example, aircraft, satellites, rockets, missiles, etc., and therefore include manned and unmanned aircraft, spacecraft, terrestrial, non-terrestrial and even surface and sub-surface water-borne marine vehicles, objects, and structures.
(20) While the preferred variations and alternatives of the present disclosure have been illustrated and described, it will be appreciated that various changes and substitutions can be made therein without departing from the spirit and scope of the disclosure. Accordingly, the scope of the disclosure should only be limited by the accompanying claims and equivalents thereof.