Gas turbine engine mounted above wing and with camber
US-12441475-B2 · Oct 14, 2025 · US
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Malecki Robert E patents
Malecki Robert E is listed as an inventor on 52 patents in our database. Major assignees and classification codes are summarized below.
| Metric | Value |
|---|---|
| Inventor | Malecki Robert E |
| Total patents | 52 |
| First publication | Feb 12, 2015 |
| Latest publication | Oct 14, 2025 |
Notable patents
Publications ranked by popularity score, then publication date.
Gas turbine engine mounted above wing and with camber
US-11970974-B2 · Apr 30, 2024 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-11781447-B2 · Oct 10, 2023 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-11781505-B2 · Oct 10, 2023 · US
Elongated geared turbofan with high bypass ratio
US-11391216-B2 · Jul 19, 2022 · US
Gas turbine engine mounted above wing and with camber
US-2022136441-A1 · May 5, 2022 · US
Gas turbine engine mounted above wing and with camber
US-2022136440-A1 · May 5, 2022 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-11286811-B2 · Mar 29, 2022 · US
Convergent divergent exit nozzle for a gas turbine engine
US-11236701-B2 · Feb 1, 2022 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-2022010689-A1 · Jan 13, 2022 · US
Recent patents
Latest publications not already listed above.
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-2021285403-A1 · Sep 16, 2021 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-11015550-B2 · May 25, 2021 · US
Nacelle short inlet
US-10724541-B2 · Jul 28, 2020 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-2020063603-A1 · Feb 27, 2020 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-2020025036-A1 · Jan 23, 2020 · US
Nacelle short inlet for fan blade removal
US-10479519-B2 · Nov 19, 2019 · US
Track fairing assembly for a turbine engine nacelle
US-10450898-B2 · Oct 22, 2019 · US
Elongated geared turbofan with high bypass ratio
US-10436121-B2 · Oct 8, 2019 · US
Exhaust nozzle for an elongated gear turbofan with high bypass ratio
US-10436120-B2 · Oct 8, 2019 · US
Elongated geared turbofan with high bypass ratio
US-2019271269-A1 · Sep 5, 2019 · US
Convergent divergent exit nozzle for a gas turbine engine
US-10371092-B2 · Aug 6, 2019 · US
Asymmetric fan nozzle in high-BPR separate-flow nacelle
US-10330047-B2 · Jun 25, 2019 · US
Exhaust nozzle arrangement for geared turbofan
US-10316757-B2 · Jun 11, 2019 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-10301971-B2 · May 28, 2019 · US
Exhaust nozzle arrangement for geared turbofan
US-10294871-B2 · May 21, 2019 · US
Nacelle deflection measurement assembly
US-10295420-B2 · May 21, 2019 · US
Convergent divergent exit nozzle for a gas turbine engine
US-2019017470-A1 · Jan 17, 2019 · US
Turbomachine thrust reverser
US-10145335-B2 · Dec 4, 2018 · US
Nacelle and compressor inlet arrangements
US-10054059-B2 · Aug 21, 2018 · US
Low pressure ratio fan engine having a dimensional relationship between inlet and fan size
US-2018209379-A1 · Jul 26, 2018 · US
Major assignees
Companies most often associated with this inventor's publications.
| Assignee | Patents |
|---|---|
| United Technologies Corp | 43 |
| Raytheon Tech Corp | 12 |
| Rtx Corp | 4 |
| Malecki Robert E | 3 |
| Murphy Michael Joseph | 1 |
Top CPC classifications
Most common classification codes across this inventor's patents.
| CPC | Patents |
|---|---|
| F02K3/06 | 31 |
| F01D25/24 | 27 |
| Y02T50/60 | 26 |
| F02C7/04 | 20 |
| F05D2220/36 | 16 |