Turbine Tip Clearance Patents: Who Leads, Where Gaps Are 2026
Turbine Tip Clearance and Sealing Patents
65.6% of all 961 records sit with just five assignees, so most of the claim space around blade tip clearance and sealing is already staked out by a small group of engine OEMs and coating specialists. Filings rose to a peak of 59 in 2019, then eased back; the 2021-to-2024 span shows a 38% decline (24 to 15 records), the most recent period the dataset treats as complete. Later years understate true filing activity because publication has not yet caught up.
- 1GENERAL ELECTRIC CO287
- 2RTX CORP154
- 3UNITED TECH CORP135
- 4ROLLS ROYCE PLC33
- 5OERLIKON METCO (US) INC21
See the full turbine tip clearance and sealing analysis in Eureka
- The complete ranking, not just the top five
- Every IPC branch with its share of the corpus
- The most-cited records, and where claim space is still thin
Common questions on this landscape
Who holds the most patents on turbine tip clearance and sealing?
One assignee leads clearly with 287 of the 961 records in scope, well ahead of the fifth-place holder at 21. The top five assignees combined hold 65.6% of all records, and the top ten hold 74.8%, so this is a field where a small number of engine OEMs and coating specialists control most of the claim space. A newcomer should expect to design around, or license from, one of these established portfolios rather than file into open ground on the core mechanical concepts.
Is filing activity in turbine tip clearance technology growing or slowing?
Filings peaked at 59 records in 2019 and had fallen to 15 by 2024, down 38% from the 24 filed in 2021. That 2021-to-2024 window is the most recent period the dataset can treat as complete, since publication typically lags actual filing by about 18 months. Figures for 2025 and 2026 will rise as those publications catch up, so the apparent recent drop should not be read as the field going quiet.
What is the difference between an abradable coating and a squealer tip in this context?
An abradable coating is a sacrificial layer applied to the casing or shroud that wears away preferentially when a blade tip rubs against it, protecting the blade and controlling the running clearance. A squealer tip is a thin-walled feature machined into the blade tip itself, often with internal cavities, that reduces the contact area and tip leakage vortex losses during any rub incursion. Both approaches appear throughout this dataset, frequently in the same records, because engine designs commonly combine a squealer-tip blade with an abradable casing coating to manage clearance and leakage together.
Disclaimer. This analysis is based on Patsnap Eureka data drawn from a limited snapshot of global patent records and is provided for general information and reference only. Patent data carries inherent limitations — recent filings are under-counted because of publication lag, counts may be on a record or family basis, classification and applicant-name data may contain errors or duplicates, and the underlying search query defines the scope shown — so the analysis may be incomplete or inaccurate and may not reflect the full technology landscape.
Nothing here is an exhaustive prior-art, novelty, freedom-to-operate or validity search, nor does it constitute legal, financial or professional advice, and it should not be relied upon as such. Verify independently and review with qualified patent and legal professionals before acting on it.
Method: Filing trend and technology composition. Derived from a Patsnap search on Turbine Tip Clearance and Sealing covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish. Every share divides by all records in scope. Data: Patsnap Eureka. See the full landscape report.