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Geared Turbofan Reduction Gearbox Patents: Who Leads 2026

Geared Turbofan Reduction Gearbox Patents: Who Leads 2026
https://www.patsnap.com/resources/blog/rd-blog/geared-turbofan-reduction-gearbox-patent-landscape/ · Patsnap · data cut-off 2026-07-31 · downloaded from the live page
Patent Landscape · Aerospace Propulsion
Geared Turbofan Reduction Gearbox Patents: Mapping the Field
  • 90.7% concentration. The top five assignees account for 1,195 of 1,318 records in scope — this is a field with almost no room for a new entrant to build a position by volume.
  • Filing rebounded, not faded. Filings rose from 63 in 2021 to 113 in 2024, a 79% increase over that span, even though the peak year on record remains 2019 at 204.
  • Gearing itself is a minority claim. Only 24.7% of records carry an F16H gearing/transmission class — most of the corpus sits in F02C gas-turbine plant claims, meaning gearbox-specific mechanical detail is comparatively thin.
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1,318
Published Records
91%
Top-5 Share of All Records
+79%
Filing Growth 2021→2024
US
Leading Jurisdiction

Filing growth compares 2021 (63 records) with 2024 (113) — 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 1,318 records in scope (CR5), not by the ranked leaders only.

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

What this dataset covers

The geared turbofan reduction gearbox sits at the mechanical core of modern high-bypass engines: a planetary gear stage that lets the fan turn slower than the low-pressure turbine, improving propulsive efficiency. This landscape covers 1,318 published records filed or published between 2015 and mid-2026, drawn from claims and descriptions referencing planetary reduction gearboxes, fan drive gearboxes and related mechanical elements — tooth profile modification, flexible support, journal bearings, oil jets, mesh efficiency and planet carriers.

Because a single family can generate several publications across jurisdictions, the record count above is best read alongside the assignee ranking, which is expressed in the same units. Publication typically lags filing by around 18 months, so the most recent one to two years in any trend chart will understate actual filing activity.

Filing activity and technology composition, 2015–2026
  1. 1ROLLS ROYCE PLC675
  2. 2RTX CORP230
  3. 3ROLLS ROYCE DEUT LTD & CO KG137
  4. 4UNITED TECH CORP105
  5. 5GENERAL ELECTRIC CO48
  6. 6GE AVIO SRL46
  7. 7ROLLS ROYCE CORP23
  8. 8PRATT & WHITNEY CANADA CORP18
  9. 9MUL TECHNOLOGIES LLC13
  10. 10AXLETECH INTERNATIONAL IP HOLDINGS LLC5
Source: Patsnap Eureka. Assignee ranking and totals. Derived from a Patsnap search on Geared Turbofan Reduction Gearbox 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

Two views of the same 1,318 records: how filing activity has moved year over year, and how it distributes across IPC subclasses that a record can carry in combination.

Filing trend, 2017–2026

Filings ran from 113 in 2017 to a peak of 204 in 2019, then rebuilt from 63 in 2021 to 113 in 2024 — a 79% increase across that three-year window. 2025 and 2026 figures are still filling in as publications catch up to filing dates, so they should not be read as a decline.

Filing trend, 2017–202606312518825011320172018204201920202021202220232024202552026Most recent year is partial — publication lag means later filings are not yet visible.

IPC subclass composition

F02C (gas-turbine plants) touches 69.6% of the 1,318 records, and F01D (turbines) touches 40.4% — both far ahead of F16H (gearing and transmissions) at 24.7%. That gap suggests most filings frame the gearbox as one element within a broader engine architecture claim rather than isolating gearing mechanics on their own.

IPC subclass compositionF02C · Gas-turbine plants91769.6%F01D · Turbines & non-positive engines53340.4%F16H · Gearing & transmissions32624.7%F02K · Jet & reaction propulsion28621.7%B64D · Aircraft equipment1078.1%F04D · Non-positive-displacement pumps765.8%F16C · Shafts, bearings & couplings503.8%F16D · Clutches & brakes423.2%Other34526.2%

Shares are the percentage of the 1,318 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 Geared Turbofan Reduction Gearbox covering 2015–2026, data cut-off 2026-07-31. Counts reflect published records only and shift as new filings publish.

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Representative Filing

A representative claim on the gearbox mechanism

Representative Record · US10443708B2
US10443708B22019-10-15

Journal bearing for rotating gear carrier

RTX CORPORATION

A gear system for a geared turbofan engine includes a sun gear, a planet gear supported in a carrier and engaged to the sun gear, a forward journal bearing and an aft journal bearing both supporting the planet gear. The carrier includes a forward wall supporting the forward journal bearing and an aft wall supporting the aft journal bearing. A ring gear is engaged to the planet gear. A geared turbofan engine is also disclosed.Filed by RTX Corporation, published 2019-10-15 — one of the field's structural claims on carrier-supported journal bearings.

US10443708B2 — patent drawing 1US10443708B2 — patent drawing 2
View full record →
Most-cited records in this landscape
#Publication no.Patent titleCitations
1US7021042B2Geartrain coupling for a turbofan engine484
2US4827712ATurbofan gas turbine engine384
3US20080317588A1Managing spool bearing load using variable area flow nozzle267
4US4782658ADeicing of a geared gas turbine engine246
5US4751816ATurbofan gas turbine engine234
6US8261527B1Gas turbine engine with geared turbofan and oil thermal management system with unique heat exchanger structure168
7US20110286836A1Geared turbofan engine with integral gear and bearing supports118
8US20180252166A1Geared turbofan115
9US6964155B2Turbofan engine comprising an spicyclic transmission having bearing journals106
10US6855089B2Reduced twist carrier96

Citation counts accumulate over time and favour older filings; treat them as a signal of influence within this corpus, not 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 Geared Turbofan Reduction Gearbox 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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Analysis

What the data means for filing strategy

Three findings shape where a new filing is likely to clear prior art, and where it is not.

Concentration
90.7%
of 1,318 records held by top 5 assignees

The field is a five-player game

Top 5 combined filings reach 1,195 of the 1,318 records in scope, and the top 10 extend that to 98.6%. A long tail of single-filing entrants exists below that line, but it holds essentially no share of the record base.

Ranking covers 58 companies total.
Growth
+79%
filing growth, 2021 to 2024

Activity rebuilt after a mid-cycle dip

Filings fell from the 2019 peak of 204 before recovering from 63 in 2021 to 113 in 2024. That is a genuine rebound in a complete-year window, not an artefact of publication lag.

2019 remains the single peak year on record.
Composition
24.7%
of records carry an F16H gearing class

Gearbox mechanics are often a supporting claim

F02C gas-turbine plant classifications appear in 69.6% of records and F01D turbine classifications in 40.4%, well ahead of F16H. Most filings anchor gearbox innovation inside a broader engine or turbine claim rather than filing gearing mechanics standalone.

A record can carry multiple IPC classes.
Jurisdiction
552
US-office records, the largest single office

Filing is concentrated in a small set of offices

The United States leads with 552 records, followed by the EPO at 345, with UK, Germany and Austria each contributing over 80. WIPO/PCT filings sit lowest among the offices listed at 38.

Offices reflect receiving office of record, not nationality of applicant.
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Eureka can read the same corpus for gaps instead of for coverage: under-claimed branches adjacent to geared turbofan reduction gearbox, with the prior art for and against each one.

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Source: Patsnap Eureka. Co-assignee relationships and derived observations. Derived from a Patsnap search on Geared Turbofan Reduction Gearbox 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
Assignee Landscape

Who is filing, and where momentum has cooled

The ranking is dominated by a small number of engine manufacturers with decades of continuation filings; momentum data shows even the leaders pulling back from recent peaks.

Leader
675
records held by the top-ranked assignee

One assignee holds more than half the top-5 total

The leading assignee's 675 records exceed the combined total of the next four ranked companies. That scale reflects both organic filing and consolidation of related corporate entities across jurisdictions.

Counted in records, per the assignee ranking.
Mid-tier
48
records at fifth place in the ranking

A steep drop after the leader

Fifth place holds 48 records, and tenth place only 5 — the ranking falls away quickly outside the top few names, leaving a genuine long tail rather than a gradual slope.

58 companies appear in the full ranking.
Momentum
-85% to -100%
YoY change among leading assignees in the latest year

Recent-year filings are down across the board

Leading assignees show sharp year-over-year declines in the latest year, from -85% to -100% depending on the company. Given the roughly 18-month publication lag, this likely reflects incomplete data for the most recent filing year rather than an actual pullback in R&D.

Momentum is measured against each assignee's prior-year count.
🔍
Where filing activity is thin
Sub-areas inside this landscape that carry comparatively few dedicated claims
oil jet lubrication targeting for planet gearsflexible support compliance tuningtooth profile modification for mesh efficiencyjournal bearing wear monitoringplanet carrier structural load paths
Rank all filers by momentum →
Year-over-year filing momentum by assignee
AssigneeRecent yearYoY
Rolls-Royce plc3-85%
General Electric Company1-94%
United Technologies Corporation0
Rolls-Royce Deutschland Ltd & Co KG0
RTX Corporation0
GE Avio S.r.l.0-100%
Rolls-Royce Corporation0
Pratt & Whitney Canada Corp.0
Source: Patsnap Eureka. Assignee-level momentum. Derived from a Patsnap search on Geared Turbofan Reduction Gearbox 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 analysis

The dataset points to a concentrated field with specific mechanical sub-areas that remain comparatively open. The next step is turning that into a filing or freedom-to-operate position.

Map claim scope against the leader's portfolio

With one assignee holding 675 of 1,318 records, any new filing in core gearbox mechanics needs a clause-level comparison against that portfolio before drafting.

Explore assignee claims in Eureka →

Test white-space sub-areas for novelty

Oil jet targeting, flexible support tuning and tooth profile modification each carry lighter claim density than the F02C/F01D core — worth a dedicated novelty search before committing R&D.

Run a novelty search in Eureka →

Track momentum, not just headcount

Recent-year declines across leading assignees may reflect publication lag rather than reduced R&D; revisit the trend once 2025-2026 data fills in.

Set up monitoring in Eureka →
Source: Patsnap Eureka. Forward-looking reading of the same dataset. Derived from a Patsnap search on Geared Turbofan Reduction Gearbox 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 this landscape

Answers are grounded in the same dataset. Derived from a Patsnap search on Geared Turbofan Reduction Gearbox 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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