Rtx Corporation
Farmington, CT, US· latest recorded location
RTX CORPORATION is named on 1,605 US grants and 1,262 published applications in this corpus. Its most frequent classification is F05D (Indexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or).
- Granted patents
- 1,605
- Published applications
- 1,262
- Inventors
- 1,492
- Granted in 2026 so far
- 438
- Most recent grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 2018 | 0 | 1 |
| 2019 | 0 | 0 |
| 2020 | 0 | 2 |
| 2021 | 0 | 7 |
| 2022 | 0 | 8 |
| 2023 | 151 | 32 |
| 2024 | 510 | 204 |
| 2025 | 506 | 504 |
| 2026 | 438 | 504 |
By publication year. 2026 runs to 8 Oct.
Technology areas
Share of 2,867 documents
- F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or2,036
- F01DNon-positive displacement machines or engines1,608
- F02CGas-turbine plants1,206
- Y02TLow-carbon transport548
- F02KJet-propulsion plants427
- B64DEquipment for fitting in or to aircraft385
- C04BLime, magnesia346
- F23RGenerating combustion products of high pressure or high velocity287
- C23CCoating metallic material193
- B33YAdditive manufacturing, i.e. manufacturing of three-dimensional [3d] objects by additive deposition, additive177
Recent patents
- Cooling features for a component of a gas turbine engine6 Oct 2026US 12,753,697 B2
- Turbine engine vane baffle6 Oct 2026US 12,753,698 B1
- Vane with pin mount and anti-rotation6 Oct 2026US 12,753,703 B2
- Turbine engine fuel injector with non-circular nozzle passage6 Oct 2026US 12,753,922 B2
- Optical inspection of waterjet drilled holes6 Oct 2026US 12,754,139 B1
- Aircraft with symmetric propulsion system rotating patterns8 Oct 2026US 2026/0307812 A1
- Aircraft powerplant with shielded control system component(s)8 Oct 2026US 2026/0307815 A1
- Environmental barrier coating8 Oct 2026US 2026/0308075 A1
- Turbine engine rotor blade with tip shelf8 Oct 2026US 2026/0309032 A1
- Internal baffle for a gas turbine engine vane8 Oct 2026US 2026/0309033 A1
Most cited
By later US patents
- Component with feather seal slots for a gas turbine engine21US 11,840,930 B22023
- Scalloped mateface seal arrangement for CMC platforms18US 11,781,440 B22023
- Aftercooler exhaust duct protection12US 11,808,209 B12023
- Fuel-air mixer for turbine engine combustion section9US 12,007,117 B12024
- Inter-cooled preheat of steam injected turbine engine6US 11,920,526 B12024