https://www.patsnap.com/resources/blog/rd-blog/turbofan-fan-blade-design-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Aerospace Propulsion
Turbofan fan blade design patents: who holds the ground and where it is still open
  • 84.1% of all 621 records sit with just five assignees — this field is about as concentrated as jet-engine IP gets.
  • Filings grew 22% from 2021 to 2024 (9 to 11 among the tracked years), the last span not distorted by publication lag.
  • F01D turbines dominate at 69.9% of records, but B23K welding/brazing and B21D sheet-metal classes show real, separately-claimed manufacturing routes.
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621
Published Records
84%
Top-5 Share of All Records
+22%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (9 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 621 records in scope (CR5), not by the ranked leaders only.

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

What the fan blade patent record actually shows

Turbofan fan blade design sits at the intersection of aerodynamics, metallurgy and manufacturing process claims. The search set spans 621 records published between 2015 and mid-2026, built around the recurring technical anchors of hollow fan blade construction, wide-chord geometry, blade root and dovetail design, and the joining processes — diffusion bonding and superplastic forming — that turn those geometries into manufacturable parts. Filtering against flutter margin, bird-strike resistance and leading-edge sheath claims keeps the set tied to blades that must survive both aerodynamic loading and foreign-object impact, not generic turbine hardware.

The assignee ranking is unusually top-heavy: five companies account for 84.1% of all records in scope, and the top ten reach 96.9%. That leaves a genuine long tail of single- or low-filing entrants below rank ten, which matters more for freedom-to-operate checks than for identifying who sets the pace.

Filing trend and technology composition, 2015-2026
  1. 1UNITED TECH CORP168
  2. 2RTX CORP134
  3. 3ROLLS ROYCE PLC131
  4. 4GENERAL ELECTRIC CO70
  5. 5FEDERALNOE GOSUDARSTVENNOE BJUDZHETNOE UCHREZHDENIE NAUKI INST PROBLEM SVERKHPLASTICHNOSTI METALLOV ROSSIJSKOJ AKADI NAUK IPSM RAN19
  6. 6OTKRYTOE AKTSIONERNOE OBSHCHESTVO AVIADVIGATEL18
  7. 7SAFRAN AIRCRAFT ENGINES SAS17
  8. 8UFA ENGINE IND ASSOC17
  9. 9SN DETUDE & DE CONSTR DE MOTEURS DAVIATION (S N E C M A)16
  10. 10BARNES GROUP INC12
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Turbofan Fan Blade Design 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
The Numbers

Filing trend and technology composition

Publication lag means the most recent one to two years always understate real filing activity; treat 2025 and 2026 as still filling in rather than as a slowdown.

Filing activity, 2017-2026

Filings ran from 13 in 2017 to a peak of 27 in 2018, then settled into a steadier band. The cleanest recent read is 2021 to 2024, where filings rose from 9 to 11 records — a 22% increase over that span, and the last stretch not yet thinned out by publication lag.

Filing activity, 2017-202608152330132017272018201920202021202220232024202512026Most recent year is partial — publication lag means later filings are not yet visible.

Where the classes concentrate

F01D (turbines and non-positive engines) touches 69.9% of the 621 records, confirming that most filings frame the blade as engine hardware rather than a standalone part. F04D (pumps) and B23P (general metal working) each cross a quarter of records, and the welding/brazing (B23K) and sheet-metal (B21D) classes, each around 15.5-15.8%, mark out the manufacturing-process side of the art as a distinct, heavily claimed track rather than an afterthought to the aerodynamic geometry claims.

Where the classes concentrateF01D · Turbines & non-positive engines43469.9%F04D · Non-positive-displacement pumps21234.1%B23P · Metal working (general)17428.0%F02C · Gas-turbine plants9815.8%B23K · Welding, soldering & brazing9715.6%B21D · Sheet-metal working9615.5%F02K · Jet & reaction propulsion538.5%B21K · Forged metal products386.1%Other31250.2%

Shares are the percentage of the 621 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 Turbofan Fan Blade Design covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

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Foundational Filings

The patents that keep getting cited

Representative Filing
US4882823A1989-11-28

Superplastic forming diffusion bonding process (US4882823A)

ONTARIO TECHNOLOGIES CORPORATION, A CA. CORP.

The filing sets out a method for forming a hollow structure with varying mass distribution from two sheets of a diffusion-bondable, superplastic-formable material. A stop-off material blocks bonding at selected non-peripheral zones, an optional flat core sheet sits between the two outer sheets, and the assembly is first diffusion-bonded then superplastically formed to the contoured target shape.This is the process family underlying hollow wide-chord fan blade manufacture — the technique that let engine makers replace solid titanium blades with lighter hollow ones without losing the joint integrity needed to survive bird-strike loading.

US4882823A — patent drawing 1US4882823A — patent drawing 2
View full record
Most-cited records in the fan blade design set
#Publication no.Patent titleCitations
1US5141400AWide chord fan blade390
2US6039542APanel damped hybrid blade209
3US5785498AComposite fan blade trailing edge reinforcement163
4US5725355AAdhesive bonded fan blade136
5US4631092AMethod for heat treating cast titanium articles to improve their mechanical properties134
6US4882823ASuperplastic forming diffusion bonding process119
7EP0926312A2Damped turbomachine blade115
8US20110211965A1Hollow fan blade114
9US6669447B2Turbomachine blade109
10US6033186AFrequency tuned hybrid blade107

Citation counts reward older filings that later art had to reference — read them as markers of influence on the field's vocabulary, not as a ranking of current commercial relevance.

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 Turbofan Fan Blade Design 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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Signals

What the data tells a strategy or IP team

Three read-throughs matter more than the raw counts: how concentrated the field is, how the manufacturing-process claims sit apart from the geometry claims, and where citation influence has settled.

Concentration
84.1% of 621 records
top 5 assignees

Five filers set the terms of the field

With top-5 concentration at 84.1% of all 621 records and the top 10 reaching 96.9%, any new entrant is filing into a space where the dominant claim language is already established by a small group of engine OEMs. Freedom-to-operate work here is mostly a check against a short list, not a broad landscape scan.

Leader alone accounts for 168 records.
Process vs geometry
B23K 15.6% · B21D 15.5%
of 621 records

Joining and forming claims are a separate battleground

Welding/brazing (B23K) and sheet-metal working (B21D) each sit around 15.5% of records — comparable weight to each other and distinct from the F01D aerodynamic-structure claims that dominate at 69.9%. Diffusion bonding and superplastic forming processes are claimed on their own terms, independent of the specific blade geometry they produce.

B23P general metal working reaches 28.0% of records.
Citation influence
US5141400A · 390 citations
most-cited record

Wide-chord geometry set the reference point

The most-cited record in the set, on wide-chord fan blade design, carries 390 citations — well ahead of the next tier. That reflects its role as an early reference point for later filings, not a signal that wide-chord claims are still the most active filing target today.

Next-ranked record: 209 citations.
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Looking for what nobody has claimed yet?

Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to turbofan fan blade design, 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 Turbofan Fan Blade Design 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
Who's Filing

The assignee landscape

The ranking covers 42 companies as returned by the data endpoint — not a top-50 or top-100 cut. Filing counts concentrate hard at the top, and momentum in the most recent tracked year has cooled across the leaders, consistent with publication lag rather than a real pullback.

Scale
168 records
leading assignee

One filer well ahead of the field

The top-ranked assignee alone holds 168 of the 621 records in scope, more than the combined total of ranks six through 42. That scale reflects decades of continuation filing across successive fan blade generations rather than a single burst of activity.

Fifth place holds 19 records; tenth place holds 12.
Long tail
42 ranked companies
full ranking

A sharp drop after the top ten

Past the top ten, which together hold 96.9% of records, the remaining ranked companies each hold a small handful of filings. That long tail is where research institutes and specialist manufacturing houses sit, often filing around a single process innovation rather than a full blade platform.

Top 10 combined: 602 of 621 records.
Momentum
-83% to -100% YoY
latest-year filings among leaders

Recent-year counts look thin — read that with caution

Several leading assignees show sharply lower or zero filings in the latest tracked year. Given the roughly 18-month lag between filing and publication, this is expected thinning rather than evidence that engine OEMs have stopped filing in this area.

One leading Russian pairing shows a strong internal co-filing relationship (20 shared records).
🔍
Under-claimed sub-areas worth checking
Branches adjacent to the core geometry and joining claims that carry comparatively thin coverage in this set.
Leading-edge sheath attachment methodsBlade dovetail fatigue-life claimsHybrid metal-composite trailing edge reinforcementBird-strike-specific damping structuresDiffusion-bond stop-off material chemistry
Rank all filers by momentum →
Recent-year filing momentum by assignee
AssigneeRecent yearYoY
Raytheon Technologies Corporation1-83%
United Technologies Corporation0
Rolls-Royce plc0
General Electric Company0-100%
SNECMA (Safran Aircraft Engines)0
Aviadvigatel Open Joint Stock Company0
Institute for Metals Superplasticity Problems of the Russian Academy of Sciences0
Ufa Engine Industrial Association Joint Stock Company0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Turbofan Fan Blade Design 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
Next Steps

Where to take this next

The dataset points to specific follow-up work rather than a single conclusion.

Map the blocking claims before you design

With 84.1% of records held by five assignees, a freedom-to-operate review should start with their dovetail, hollow-core and diffusion-bonding claim families before looking at the long tail.

Run a claim map in Eureka

Track the manufacturing-process split separately

B23K and B21D claims form a track distinct from the aerodynamic geometry claims in F01D — treat process and structure as two separate landscapes when scoping new filings.

Explore process claims in Eureka

Revisit the trend once 2025-2026 fill in

Publication lag means the current tail understates real activity; a re-run against this same search string in a year will sharpen the 2024-2026 read.

Set up a monitoring search in Eureka
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Turbofan Fan Blade Design 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 on fan blade design patents

Answers are grounded in the same dataset. Derived from a Patsnap search on Turbofan Fan Blade Design 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.