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Thermal Barrier Coatings Patents: Who Leads, Filing Trends 2026

Thermal Barrier Coatings Patents: Who Leads, Filing Trends 2026
https://www.patsnap.com/resources/blog/rd-blog/thermal-barrier-coatings-for-gas-turbines-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Coatings & Surface Treatment
Thermal Barrier Coating Patents for Gas Turbines
  • Filing has declined since its 2018 peak of 78, with the 2022 midpoint at 37 — the claim space built up over the last decade is now being consolidated rather than expanded.
  • Momentum has stalled across every major assignee, with GE, Honeywell and both Rolls-Royce entities showing 0 filings and -100% YoY in the most recent year of the dataset.
  • C23C coating claims dominate at 1,860 of 2,137 records, while F23R combustion-chamber integration (105) and B23P metalworking process claims (77) remain comparatively thin.
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2,137
Published Records
69%
Top-5 Share of All Records
-79%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (53 records) with 2024 (11) — a three-year span. 2024 is the most recent year we treat as complete: publication lags filing by roughly 18 months, so 2025 onwards are still filling in and any growth rate that ends there would understate the field. Top-5 share is the combined record count of the five largest assignees divided by all 2,137 records in scope (CR5), not by the ranked leaders only.

Published byPatsnap Research··7 min readSourced from Patsnap Eureka
Overview

What this dataset covers

This landscape draws on 2,137 patent families published between 2015 and mid-2026, filtered to documents claiming a thermal barrier coating system, bond coat, or thermally grown oxide behaviour under CMAS attack, spallation or electron beam PVD deposition, and classified under C23C, C23C28 or F01D5. It is a coatings-and-turbine-hardware crossover: the majority of records sit in coating deposition classes, but over 1,300 also carry a turbine-component classification, meaning most applicants are claiming the coating as installed on a specific blade, vane or combustor part rather than as a standalone material.

Because publication typically lags filing by around 18 months, the last one to two years in any trend chart will read lower than the true filing rate once those applications publish. That lag does not explain a decline stretching back to a 2018 peak, however — the flattening in this dataset reflects filing behaviour, not a reporting artefact.

Filing activity, 2017–2026
  1. 1GENERAL ELECTRIC CO817
  2. 2UNITED TECH CORP257
  3. 3RTX CORP199
  4. 4HONEYWELL INTERNATIONAL INC123
  5. 5SIEMENS AG87
  6. 6ROLLS ROYCE PLC70
  7. 7ROLLS ROYCE CORP65
  8. 8SIEMENS ENERGY INC64
  9. 9CHROMALLOY UK39
  10. 10HOWMET CORPORATION37
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP

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The Numbers

Filing trend and technology composition

Two views of the same 2,137-family dataset: how filing volume has moved year over year, and how those families distribute across the IPC subclasses that make up a TBC system.

A decade of rise and plateau

Filings rose from 60 in 2017 to a peak of 78 in 2018, then eased back through the 2022 midpoint of 37 and continued down toward single digits by 2026 — consistent with a technology area where the core claim territory was staked out early and new entrants now face dense prior art.

A decade of rise and plateau020406080602017782018201920202021202220232024202522026Most recent year is partial — publication lag means later filings are not yet visible.

Coating claims outweigh everything else

C23C (coating and surface deposition) accounts for 1,860 of the 2,137 records, well ahead of F01D turbine hardware (1,302) and C04B ceramics (375). The smaller counts in F23R combustion chambers (105) and B23P metalworking (77) mark where integration- and process-level claims are comparatively sparse.

Coating claims outweigh everything elseC23C · Coating & surface deposition1,86087.0%F01D · Turbines & non-positive engines1,30260.9%C04B · Ceramics, cement & refractories37517.5%F02C · Gas-turbine plants25912.1%B32B · Layered products & laminates21910.2%C22C · Alloys1205.6%F23R · Combustion chambers1054.9%B23P · Metal working (general)773.6%Other59427.8%

Shares are the percentage of the 2,137 records in scope. A patent can carry several IPC classes, so the shares add up to more than 100%.

Source: Patsnap Eureka. Filing trend and technology composition. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

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Key Patents

The foundational filings this field cites back to

Representative Filing
US20210180191A12021-06-17

Rare-earth doped bond coat for thermally grown oxide luminescence sensing

UNIVERSITY OF CENTRAL FLORIDA RESEARCH FOUNDATION, INC.

A thermal barrier coated turbine component carries a metallic bond coat doped with rare-earth luminescent ions. As the thermally grown oxide (TGO) layer forms at the bond coat/top coat interface, dopant ions migrate into it, enabling real-time phosphor thermometry — optical temperature sensing of the TGO layer itself rather than of the component surface.Filed by University of Central Florida Research Foundation, published 2021-06-17.

US20210180191A1 — patent drawing 1US20210180191A1 — patent drawing 2
View full filing
Most-cited records in this dataset
#Publication no.Patent titleCitations
1US20090324989A1Multilayer thermal barrier coating443
2US5514482AThermal barrier coating system for superalloy components277
3US5683825AThermal barrier coating resistant to erosion and impact by particulate matter234
4US6177200B1Thermal barrier coating systems and materials233
5US6284323B1Thermal barrier coating systems and materials232
6US6117560AThermal barrier coating systems and materials230
7US6102656ASegmented abradable ceramic coating230
8US5716720AThermal barrier coating system with intermediate phase bondcoat220
9US6465090B1Protective coating for thermal barrier coatings and coating method therefor219
10US5705231AMethod of producing a segmented abradable ceramic coating system218

Citation counts accumulate over time and favour older filings; treat this table as a map of foundational influence, not of which claims are commercially active today.

Each row carries its publication number; clicking a row searches Eureka by that number.

Source: Patsnap Eureka. Citation counts and representative records. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
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Insights

What the numbers mean for a filing decision

Four read-throughs from the trend, classification and citation data above.

Filing Trend
78 → 2 (2018–2026)
peak to trough

Growth phase has closed

The jump from 60 filings in 2017 to a peak of 78 in 2018 marked an active buildout period. The steady decline since — through 37 at the 2022 midpoint and down toward the low single digits by 2026 — indicates applicants have largely staked their positions rather than continuing to expand claim territory.

Trend data, 2017–2026
Classification Spread
1,860 of 2,137
records in C23C

Coating claims crowd the top classification

Nearly nine in ten records touch C23C, the coating and surface deposition subclass, confirming this is fundamentally a materials and deposition-process field even though most filings also name a turbine application.

IPC composition
Assignee Momentum
0 filings, -100% YoY
across major assignees

Incumbents have gone quiet at once

GE, Honeywell and both Rolls-Royce entities each show zero filings and a -100% year-on-year change in the latest period. A simultaneous pullback across multiple large filers this pronounced usually signals either a maturing claim base or a reporting lag rather than a genuine collapse in R&D.

Recent-year momentum
Citation Concentration
443 citations
top-cited record

A handful of 1990s-2000s filings anchor the field

The most-cited records in this dataset date to the multilayer and erosion-resistant TBC systems era; their citation counts (up to 443) reflect decades of accumulation and mark foundational prior art that later filings must design around, not current competitive activity.

Citation ranking
Eureka AI Agent
Looking for what nobody has claimed yet?

Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to thermal barrier coatings for gas turbines, with the prior art for and against each one.

Find the white space →
Source: Patsnap Eureka. Co-assignee relationships and derived observations. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
Players

Who holds the claim space

Filing here concentrates among a small group of turbine OEMs and their coating-services affiliates, several of which also appear as co-assignee pairs — a sign of joint filings between parent and subsidiary or between OEM and licensed coating applicator.

Co-Filing Pattern
41 shared families
strongest co-assignee pair

OEM–applicator pairing dominates joint filings

The strongest co-assignee link in this dataset pairs a turbine OEM with an independent coating applicator at 41 shared families, well ahead of the next-strongest pairs. That pattern points to coordinated IP strategy between the component designer and the shop actually applying the coating.

Co-assignee pairs, n=10
Momentum Reversal
-100% YoY
at multiple top assignees

Every major incumbent shows zero recent filings

GE, United Technologies, Honeywell, Siemens and both Rolls-Royce entities all register zero filings in the latest tracked year. Given the ~18-month publication lag, some of this is likely unpublished pipeline rather than an actual freeze on R&D.

Recent-year momentum
Filing Footprint
743 US, 737 EPO
top receiving offices

US and European filings run near parity

The United States (743) and the EPO (737) receive almost identical volumes, with WIPO PCT filings (168) a distant third — suggesting most applicants pursue direct national/regional protection in the two largest turbine markets rather than routing everything through PCT first.

Receiving-office counts
🔍
Under-claimed sub-areas worth checking before filing
These sit at the thin edges of the IPC composition data — fewer families, less crowded prior art.
CMAS-resistant top coat chemistriesTGO growth-rate sensing methodsCombustor-liner-specific bond coat integration (F23R)Metalworking/deposition process claims (B23P)Rare-earth doped luminescent thermometry layers
Rank all filers by momentum →
Recent-year filing momentum by assignee
AssigneeRecent yearYoY
General Electric Company0-100%
United Technologies Corporation0
Honeywell International Inc.0-100%
Siemens AG0
Rolls-Royce plc0-100%
Rolls-Royce Corporation0
Raytheon Technologies Corporation0-100%
CHROMALLOY UK0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
What's Next

Where to take this analysis

The dataset points to a mature core and a thinner set of adjacent claims. Two directions make sense from here.

Map freedom-to-operate against the top-cited patents

The five most-cited records anchor decades of prior art in multilayer and erosion-resistant TBC systems. Any new bond coat or top coat composition claim should be checked against these before drafting.

Explore prior art in Eureka

Track whether the assignee pullback is real or a lag artefact

Zero recent filings across every major incumbent is a striking signal. Re-running this trend in twelve months, once the publication lag clears, will show whether it reflects a genuine slowdown or a temporary gap.

Set up monitoring in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP
FAQ

Common questions about thermal barrier coating patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Thermal Barrier Coatings for Gas Turbines covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.Run this in Eureka MCP

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Disclaimer. This page is generated from Patsnap Eureka data drawn from a limited snapshot of global patent and scientific-literature records, and is provided for general information and reference only.

Patent data carries inherent limitations: recent filings (typically the most recent 18–24 months) are under-counted due to standard publication lag; counts may be reported at either a patent-family or a patent-record basis and are not always directly comparable; classification, applicant-name, and citation data may contain errors, duplicates, or omissions; and the underlying search query defines and constrains the scope shown. As a result, the analysis may be incomplete or inaccurate and may not reflect the full technology landscape.

Nothing on this page constitutes an exhaustive prior-art, novelty, freedom-to-operate, or validity search, nor does it constitute legal, financial, investment, or professional advice, and it should not be relied upon as such. Any patent, commercial, or strategic decision should be verified independently and reviewed with qualified patent, legal, and domain professionals. Patsnap makes no warranties, express or implied, as to the accuracy, completeness, or fitness for any particular purpose of the information presented.

Machine translation. Assignee and organisation names originally recorded in Chinese, Japanese or Korean have been rendered into English by an AI translation step so that the tables stay readable. These renderings are best-effort and may not match a company’s registered English name; the original name is what the underlying patent record carries, and it is what any Eureka query launched from this page uses.

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