F05D 2300/502
Thermal properties
F05D2300/502 (Thermal properties) appears on 636 US grants and 735 published applications in this corpus.
Search patents in F05D- Granted patents
- 636
- Published applications
- 735
- Assignees
- 223
- Inventors
- 1,696
- Latest grant
- 4 Aug 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1987 | 1 | 0 |
| 1988 | 3 | 0 |
| 1989 | 1 | 0 |
| 1990 | 0 | 0 |
| 1991 | 3 | 0 |
| 1992 | 3 | 0 |
| 1993 | 0 | 0 |
| 1994 | 1 | 0 |
| 1995 | 0 | 0 |
| 1996 | 0 | 0 |
| 1997 | 2 | 0 |
| 1998 | 4 | 0 |
| 1999 | 1 | 0 |
| 2000 | 4 | 0 |
| 2001 | 8 | 2 |
| 2002 | 4 | 4 |
| 2003 | 12 | 12 |
| 2004 | 6 | 10 |
| 2005 | 10 | 15 |
| 2006 | 11 | 16 |
| 2007 | 7 | 15 |
| 2008 | 11 | 15 |
| 2009 | 10 | 19 |
| 2010 | 10 | 29 |
| 2011 | 15 | 29 |
| 2012 | 26 | 20 |
| 2013 | 22 | 19 |
| 2014 | 14 | 34 |
| 2015 | 16 | 33 |
| 2016 | 22 | 83 |
| 2017 | 39 | 60 |
| 2018 | 39 | 66 |
| 2019 | 69 | 51 |
| 2020 | 66 | 48 |
| 2021 | 39 | 30 |
| 2022 | 49 | 23 |
| 2023 | 34 | 38 |
| 2024 | 26 | 22 |
| 2025 | 31 | 26 |
| 2026 | 17 | 16 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
Recent patents
- Air turbine starter4 Aug 2026US 12,698,725 B2Unison Industries, LLC
- Turbine engine assembly with nut device and thermal expansion compensation14 Jul 2026US 12,680,520 B2Safran Ceramics
- Aircraft component with fiber-reinforced elastic expansion section16 Jun 2026US 12,654,421 B2Rohr, Inc.
- Slurry-based methods for forming a bond coat and articles formed by the methods2 Jun 2026US 12,643,831 B2General Electric Company
- Material systems for repair of thermal barrier coating and methods thereof26 May 2026US 12,637,947 B2General Electric Company
- Slurry-based methods for forming a bond coat and articles formed by the methods17 Sep 2026US 2026/0274760 A1General Electric Company
- Expander and thermodynamic cycle using the expander17 Sep 2026US 2026/0275871 A1Nuovo Pignone Tecnologie Srl
- A ring segment for a gas turbine, a method to operate a gas turbine and computer-implemented method to design and/or manufacture said ring segments30 Jul 2026US 2026/0218630 A1Siemens Energy Global GmbH & Co. KG
- Cmc component with cover plate16 Jul 2026US 2026/0201815 A1Rtx Corporation
- Turbine engine seal for turbine engines18 Jun 2026US 2026/0168386 A1General Electric Company
Most cited
By later US patents
- Ceramic matrix composite gas turbine vane132US 6,709,230 B2Siemens Westinghouse Power Corporation · 2004
- Blade clearance control using high-CTE and low-CTE ring members109US 8,790,067 B2United Technologies Corporation · 2014
- Passive clearance control85US 6,877,952 B2Florida Turbine Technologies, Inc. · 2005
- Method for producing a titanium metallic composition having titanium boride particles dispersed therein75US 7,410,610 B2General Electric Company · 2008
- Passive clearance control60US 7,210,899 B22007