F01D 11/08
Preventing or minimising internal leakage of working-fluid: for sealing space between rotor
Official title: for sealing space between rotor blade tips and stator (specially-shaped blade tips therefor F01D5/20)
F01D11/08 (Preventing or minimising internal leakage of working-fluid: for sealing space between rotor) appears on 3,793 US grants and 3,753 published applications in this corpus.
Search patents in F01D- Granted patents
- 3,793
- Published applications
- 3,753
- Assignees
- 375
- Inventors
- 5,475
- Latest grant
- 6 Oct 2026
Filings by year
| Year | Granted patents | Published applications |
|---|---|---|
| 1976 | 12 | 0 |
| 1977 | 16 | 0 |
| 1978 | 11 | 0 |
| 1979 | 11 | 0 |
| 1980 | 14 | 0 |
| 1981 | 27 | 0 |
| 1982 | 21 | 0 |
| 1983 | 22 | 0 |
| 1984 | 19 | 0 |
| 1985 | 23 | 0 |
| 1986 | 19 | 0 |
| 1987 | 32 | 0 |
| 1988 | 20 | 0 |
| 1989 | 22 | 0 |
| 1990 | 8 | 0 |
| 1991 | 33 | 0 |
| 1992 | 32 | 0 |
| 1993 | 28 | 0 |
| 1994 | 32 | 0 |
| 1995 | 17 | 0 |
| 1996 | 21 | 0 |
| 1997 | 27 | 0 |
| 1998 | 27 | 0 |
| 1999 | 27 | 0 |
| 2000 | 41 | 0 |
| 2001 | 36 | 14 |
| 2002 | 46 | 32 |
| 2003 | 45 | 37 |
| 2004 | 33 | 57 |
| 2005 | 46 | 73 |
| 2006 | 46 | 56 |
| 2007 | 44 | 72 |
| 2008 | 32 | 84 |
| 2009 | 44 | 105 |
| 2010 | 61 | 112 |
| 2011 | 60 | 93 |
| 2012 | 98 | 114 |
| 2013 | 82 | 171 |
| 2014 | 105 | 178 |
| 2015 | 109 | 209 |
| 2016 | 117 | 392 |
| 2017 | 177 | 304 |
| 2018 | 239 | 274 |
| 2019 | 371 | 262 |
| 2020 | 351 | 295 |
| 2021 | 308 | 196 |
| 2022 | 232 | 149 |
| 2023 | 163 | 137 |
| 2024 | 148 | 124 |
| 2025 | 154 | 93 |
| 2026 | 84 | 120 |
By publication year. Applications have been published since 2001. 2026 runs to 8 Oct.
Subgroups
Granted patents
Recent patents
- Method for producing an abradable coating, abradable coating and coated part6 Oct 2026US 12,753,704 B2Centre National De La Recherche Scientifique
- Gas turbine engines having self-cooling seals and methods of operating the same29 Sep 2026US 12,747,672 B1Honeywell Aerospace US LLC
- CMC component with structure for directing cooling air flow22 Sep 2026US 12,742,398 B2Rtx Corporation
- Blade tip clearance sensor and gas turbine including same22 Sep 2026US 12,742,399 B2Doosan Enerbility Co., Ltd.
- Compressor shroud with swept grooves22 Sep 2026US 12,742,459 B2Pratt & Whitney Canada Corp.
- Hot gas path segment with seal slot cooling groove8 Oct 2026US 2026/0309040 A1GE Vernova Infrastructure Technology LLC
- Ceramic matrix composite seal repair8 Oct 2026US 2026/0309044 A1Rtx Corporation
- Turbine engine tip clearance control utilizing electric machine8 Oct 2026US 2026/0309046 A1Rtx Corporation
- Turbine engine rotor shroud8 Oct 2026US 2026/0309053 A1Rtx Corporation
- Assembly clip for gas engine components1 Oct 2026US 2026/0298103 A1Rtx Corporation
Most cited
By later US patents
- Segmented abradable ceramic coating133US 6,102,656 AUnited Technologies Corporation · 2000
- Use of high temperature insulation for ceramic matrix composites in gas turbines123US 6,197,424 B1Siemens Westinghouse Power Corporation · 2001
- Ceramic turbine shroud assembly117US 4,087,199 AGeneral Electric Company · 1978
- Method of producing a segmented abradable ceramic coating system113US 5,705,231 AUnited Technologies Corporation · 1998
- Ceramic matrix composite component for a gas turbine engine113US 6,758,653 B2Siemens Westinghouse Power Corporation · 2004