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Turbofan Engine Additive Manufacturing Patent Landscape

Turbofan Engine Additive Manufacturing Patent Landscape
Competitive Landscape
Turbofan Engine Additive Manufacturing Patent Landscape in 2026

The turbofan engine additive manufacturing patent field is highly concentrated, with RTX Corp, General Electric, and Rolls-Royce collectively anchoring the top tier among 4,691 patent families in scope. Annual filing volume has eased substantially from its 2018 peak, though the corpus reflects a decade of deep, sustained investment by a small number of aerospace primes.

4,691
Patent families in scope
78%
Top-5 share of top-100 filers
-55%
3-yr filing growth (lag-adj.)
United States
Leading jurisdiction
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Published byPatSnap Insights Team··7 min readVerified by PatSnap Eureka data
Overview

RTX Corp leads a tightly held field dominated by five aerospace primes

RTX Corp holds the top position in the applicant ranking with 4,313 patent records, followed by General Electric Co at 2,952 and United Technologies Corp at 2,920—three entities that together account for the bulk of the field’s documented innovation.

The top five filers—RTX Corp, General Electric Co, United Technologies Corp, Rolls-Royce PLC, and Pratt & Whitney Canada Corp—collectively represent 78% of the hundred largest filers’ combined total, signaling a field where a handful of vertically integrated OEMs have erected substantial prior-art barriers.

Leading applicants
#ApplicantPatent recordsShare
1RTX Corp4,313
2General Electric Co2,952
3United Technologies Corp2,920
4Rolls-Royce PLC2,332
5PRATT & WHITNEY CANADA CORP816
6Rolls-Royce Corp513
7Rolls-Royce North American Technologies Inc390
8Honeywell International Inc319
9Siemens Energy Inc283
10Siemens AG227
#ApplicantPatent recordsShare
11Safran Aircraft Engines SAS178
12Solar Turbines Inc159
13IHI Corporation140
14Florida Turbine Technologies Inc116
15SIEMENS ENERGY GLOBAL GMBH & CO KG110
16SN DETUDE & DE CONSTR DE MOTEURS DAVIATION (S N E …90
17ROLLS ROYCE DEUT LTD & CO KG85
18MTU Aero Engines GmbH65
19General Electric Technology GmbH59
20GE Infrastructure Technology LLC49
↗ Hover a row · click a company to ask Eureka

This concentration means that new entrants or tier-2 suppliers face a dense thicket of overlapping claims across turbine structures, gas-turbine plant auxiliaries, and pumping systems before reaching open ground, and must differentiate on process chemistry, novel alloy systems, or highly specific component geometries.

Patent publication typically lags filing by 18–24 months, so figures for 20242026 undercount actual recent activity; trend reads for those years should be treated as provisional. Longer-window growth, applicant concentration, and technology-route coverage are therefore more reliable signals than the latest-year bar alone.

Source: PatSnap Eureka. Chart shows the top applicants ranked by patent records; the corpus total is measured in patent families. These figures use different units and should not be compared directly.Explore deeper in Eureka →
Trends & Structure

Filing volume peaked in 2018 and has moderated; turbine structures dominate the technology mix

The annual filing chart captures a decade-long arc that crested in 2018, while the IPC composition chart reveals that core turbine-structure classes dwarf the dedicated additive manufacturing classification, pointing to where OEMs have chosen to stake their claims.

Annual filing trend

Annual filings peaked in 2018 at 911 patent records before declining to 437 in 2021 and moderating further thereafter; 2024–2026 data are incomplete due to publication lag and should not be read as a continued structural decline. The field reached its lifecycle inflection point around 2018, and the multi-year moderation reflects both maturation of core process patents and consolidation among the leading filers.

Annual filing trendAnnual values from 2017 to 2026, peaking at 911 in 2018.86720179112018862201956920204372021298202228620232602024197202542026↗ Hover for values · click a bar to ask Eureka

Technology composition

F01D (Turbines and non-positive engines) accounts for by far the largest share of IPC classifications, with F02C (Gas-turbine plants) and F04D (Non-positive-displacement pumps) as secondary clusters. Notably, B33Y (Additive manufacturing / 3D printing) appears much further down the list, indicating that applicants have historically anchored claims in component-function classes rather than the process-method class—a strategic choice that broadens the scope of protection.

Technology compositionF01D · Turbines & non-positive engines leads with 16,985; F02C · Gas-turbine plants 4,261.F01D · Turbines & non-po…16,985F02C · Gas-turbine plants4,261F04D · Non-positive-disp…2,501F02K · Jet & reaction pr…1,332B23P · Metal working (ge…917C23C · Coating & surface…696F23R · Combustion chambers527B23K · Welding, solderin…452↗ Hover for values · click a bar to ask Eureka
Source: PatSnap Eureka. Technology-branch counts are measured in patent records; a single patent family can carry several IPC classes, so class totals can exceed the family total in scope.Explore deeper in Eureka →
Key Patents

Highly cited patent families surfaced by the query

Citation-heavy patent families returned by the query. Use this section as citation context, not as a curated list of the most topic-specific patents.

Featured patent
US20260117978A1Published 2026-04-30

Bimetallic hydrogen fuel nozzle with multiple flow…

Pratt & Whitney Canada CORP.

A hydrogen fuel nozzle for a gas turbine engine has a plurality of flow circuits, each of which is configured to flow one of a fuel or an oxidizer to a gas turbine engine combustor positioned downstream of the hydrogen fuel nozzle when the gas turbine engine is assembled. At least one of the plurality of flow circuits is a hydrogen flow circuit configured… (excerpt from the patent abstract)

Bimetallic hydrogen fuel nozzle with multiple flow… — patent drawingBimetallic hydrogen fuel nozzle with multiple flow… — patent drawing
Representative drawings from the patent document.
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Highly cited patent families surfaced by this query
#PatentCitations
1Counter rotating aircraft gas turbine engine with …387
2Impingement cooled transition duct385
3Chevron film cooled wall380
4Aircraft engine with inter-turbine engine frame364
5Evaporatively cooled rotor for a gas turbine engine353
6Microturbomachinery326
7Vane assembly and temperature control arrangement326
8High pressure gas generator rotor tie rod system f…296

Ranked by total forward citations. Citation counts favour older and broadly cited patent families, and broad or adjacent patents may appear when they match the search scope. Treat this section as citation context, not as a curated list of the most topic-specific patents. Some patent titles may be shown in their original, non-English language where an accurate translation could not be guaranteed.

Source: PatSnap Eureka. Citation-ranked patent families surfaced by this query.Open in Eureka →
Insights

What the patent structure means for R&D investment decisions

Four structural factors—lifecycle stage, competitive concentration, co-filing ecosystems, and geographic coverage—shape where incremental R&D spend is most likely to find differentiated space.

Decline

Field is past peak; core turbine-AM patents are largely staked

The lifecycle evidence indicates that annual filings have eased back from their 2018 peak, placing this field in a declining phase by annual-volume measures. Core process and component patents filed by the major OEMs from 2015–2020 are now maturing toward grant and enforcement, raising the cost of undifferentiated entry. R&D investment should target process gaps—novel alloy systems, post-processing integration, or digital-twin inspection methods—where the prior-art density is lower.

Lifecycle: Decline
Concentration

Five primes hold 78% of the top-100 filers’ combined records

The top five filers account for 78% of the hundred largest filers’ combined patent records, a level of concentration typical of regulated aerospace supply chains where qualification barriers amplify IP moats. The gap between Rolls-Royce PLC at rank four (2,332 patent records) and Pratt & Whitney Canada at rank five (816 patent records) marks a significant tier break. Challengers operating below that break—Rolls-Royce Corp (513), Rolls-Royce North American Technologies (390), Honeywell (319)—face a large absolute gap to the top tier.

High concentration
Collaboration

Rolls-Royce’s intra-group co-filing is the dominant collaboration signal

The most active co-filing pair is Rolls-Royce Corp and Rolls-Royce North American Technologies Inc with 197 joint records, reflecting coordinated IP strategy across the group’s North American entities. Siemens AG and Siemens Energy Inc account for 30 joint records, while United Technologies Corp and MTU Aero Engines have 19 joint records—one of the few cross-group collaborations visible in the data. General Electric Co and Oliver Crispin Robotics also appear with 12 joint records, signaling GE’s interest in robotic AM inspection or repair. These patterns suggest that cross-company collaboration outside existing corporate families remains limited.

Intra-group dominant
Geography

US and EPO filings dominate; China and Asia are thin

The United States leads jurisdiction coverage with 6,459 patent records, followed by Europe via the EPO at 5,267. The United Kingdom (936), Canada (704), and Japan (678) form a secondary tier consistent with the home markets of the leading OEMs. China holds only 296 patent records, and South Korea 76, indicating that the major Western aerospace primes have not prioritized Asia-Pacific protection at scale—a potential exposure point if Chinese or Korean manufacturers accelerate in this domain.

US/EPO concentrated
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Top collaboration links
ApplicantCollaboratorCo-filings
Rolls-Royce CorpRolls-Royce North American Technologies Inc197
Siemens AGSiemens Energy Inc30
United Technologies CorporationMTU Aero Engines GmbH19
Rolls-Royce PLCRolls-Royce North American Technologies Inc19
Rolls-Royce PLCRolls-Royce High Temperature Composites Inc19
Rolls-Royce CorpRolls-Royce High Temperature Composites Inc19
Rolls-Royce PLCRolls-Royce Corp15
Rolls-Royce North American Technologies IncRolls-Royce High Temperature Composites Inc14
General Electric CompanyOliver Crispin Robotics Ltd12
Siemens AGMikro Systems Inc12

Co-filing pairs, ranked by the number of jointly-filed patent families.

Source: PatSnap Eureka. Collaboration counts are based on co-applicant relationships within the patent-record corpus.Explore insights →
Leaders

RTX Corp leads on volume; Pratt & Whitney Canada is the only top-five filer showing positive recent momentum

The applicant ranking is anchored by two consolidated entities—RTX Corp and General Electric Co—whose portfolios span virtually every turbine sub-system. Recent filing trends reveal diverging trajectories within the top tier.

Leader · RTX Corp

RTX Corp

RTX Corp ranks first with 4,313 patent records, the largest position in the field by a wide margin. Its technology emphasis is concentrated in F01D 5 (turbine blade and vane structures), F02C 7 (gas-turbine plant auxiliaries), and F01D 25 (turbine casings and bearing supports)—a portfolio shaped by the integration of Pratt & Whitney and Collins Aerospace legacy assets. Recent filing trend is down 11%, consistent with the field-wide moderation from the 2018 peak but less severe than peers, suggesting RTX continues to file selectively in core areas.

patent records: 4,313
Challenger · Pratt & Whitney Canada Corp

Pratt & Whitney Canada Corp

Pratt & Whitney Canada Corp holds 816 patent records at rank five, but stands out as the only top-five filer with a positive recent filing trend at +33%, making it the most active upward mover among the large incumbents. Its technology focus mirrors the broader RTX group—F01D 5, F04D 29, and F01D 25—but its regional specialization in business and regional jet engines may be driving continued investment in additive-manufactured components for smaller, higher-cycle powerplants where AM economics are most favorable.

patent records: 816
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Rolls-Royce PLCHoneywell International Inc+ more
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Leading-applicant momentum (recent 3 yrs, lag-adjusted)
ApplicantRecent (3 yrs)Trend
General Electric Company118▼ -17%
Rolls-Royce PLC103▼ -66%
RTX Corporation395▼ -11%
Pratt & Whitney Canada Corp97▲ +33%
Rolls-Royce Corp12▼ -84%
Rolls-Royce North American Technologies Inc6▼ -81%
Honeywell International Inc12▼ -79%
Siemens Energy Inc2▲ new entrant
Source: PatSnap Eureka. Applicant momentum reflects recent three-year filing activity compared with the prior three-year period.Explore players →
Adjacent Branches

Under-served adjacent branches worth monitoring for white-space entry

Several IPC branches adjacent to the dominant turbine-structures cluster carry meaningful patent counts but remain small relative to the core, suggesting areas where the prior-art density may be lower and differentiated filing is more tractable.

C23C · Coating and surface deposition

C23C (Coating and surface deposition) holds 696 patent records—only 2% of the classified corpus—despite being directly relevant to thermal barrier coatings, environmental barrier coatings, and bond-coat systems applied in or after additive manufacturing of hot-section components. The sparse coverage relative to the scale of the underlying engineering problem suggests that process-integrated coating deposition (e.g., directed-energy deposition with in-situ coating) is an under-claimed area. Entry paths exist for materials specialists and coating OEMs not currently active in the top-20 applicant list.

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B22F · Powder metallurgy

B22F (Powder metallurgy) appears with 315 patent records, representing roughly 1% of the classified corpus despite powder-bed fusion and directed-energy deposition processes being foundational to metal AM for turbofan components. The low share relative to the structural turbine classes indicates that upstream powder characterization, powder recycling, and feedstock qualification—critical to AM part certification—are comparatively under-patented by the dominant OEMs. Powder suppliers, material qualification firms, and research institutions represent plausible entry vectors.

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F23R · Combustion chambersF02K · Jet and reaction propulsion+ more
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Source: PatSnap Eureka. Branch share figures are relative to the full classified patent-record corpus for this topic.Explore emerging →
Route Matrix

How leading applicants differ by technology route emphasis

Route coverage across the main technology branches in the current evidence set.

PlayerF01D 5 · Turbines & non-positive enginesF02C 7 · Gas-turbine plantsF01D 25 · Turbines & non-positive enginesF01D 9 · Turbines & non-positive enginesF04D 29 · Non-positive-displacement pumps
United Technologies CorporationStrong · 5,887Moderate · 1,619Moderate · 1,519Moderate · 1,387Emerging · 961
General Electric CompanyStrong · 2,976Moderate · 755Moderate · 668Emerging · 503Emerging · 423
Rolls-Royce PLCStrong · 2,260Emerging · 298Emerging · 354Emerging · 282Emerging · 340
RTX CorporationStrong · 1,069Emerging · 198Moderate · 253Moderate · 229Emerging · 111
Pratt & Whitney Canada CorpStrong · 775Emerging · 123Emerging · 136Emerging · 86Moderate · 159
Rolls-Royce CorpStrong · 487Emerging · 29Moderate · 111Emerging · 87Emerging · 50
Rolls-Royce North American Technologies IncStrong · 366AbsentModerate · 84Emerging · 50Emerging · 32
Source: PatSnap Eureka. Matrix values are measured in patent records and should not be compared directly with family-level applicant totals.Compare in Eureka →
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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.

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