There is currently no text in this page. You can search for this page title in other pages, or search the related logs, but you do not have permission to create this page.
Category:G01M15/14
Subcategories
This category has the following 19 subcategories, out of 19 total.
A
D
G
J
M
P
R
S
T
W
Z
Pages in category "G01M15/14"
The following 34 pages are in this category, out of 34 total.
1
- 17971183. METHOD AND INTEGRALLY BLADED ROTOR FOR BLADE OFF TESTING simplified abstract (Pratt & Whitney Canada Corp.)
- 17972834. SEAL MONITORING APPARATUS simplified abstract (GENERAL ELECTRIC COMPANY)
- 18121430. MULTI-MEASUREMENT PROBE ASSEMBLY simplified abstract (Raytheon Technologies Corporation)
- 18238051. OPTICAL DEFECT DETECTION SYSTEM (RTX Corporation)
- 18238196. APPARATUS AND METHOD FOR PARTIALLY BLADED ROTOR TEST (RTX Corporation)
- 18371910. COMBUSTION TEST RIG (PRATT & WHITNEY CANADA CORP.)
- 18372485. SYSTEM AND METHOD FOR IDENTIFYING RUBBING CONDITIONS FOR ENGINE ROTATIONAL EQUIPMENT (PRATT & WHITNEY CANADA CORP.)
- 18377434. ENGINE COMPONENT TEST SYSTEM WITH CRYOGENIC COOLING SYSTEM (Pratt & Whitney Canada Corp.)
- 18406310. STEAM TURBINE NOZZLE DEFORMATION AMOUNT MANAGING APPARATUS simplified abstract (TOSHIBA ENERGY SYSTEMS & SOLUTIONS CORPORATION)
- 18420402. SYSTEM AND METHOD OF USING A TOOL ASSEMBLY simplified abstract (General Electric Company)
- 18442200. ELECTRONIC DEVICE FOR A MEASURING RAKE FACILITATING DATA LOADING simplified abstract (Airbus Operations SAS)
- 18442497. ANTISTATIC PRESSURE MEASURING RAKE, IN PARTICULAR FOR AN ENGINE OF AN AIRCRAFT, AND MORE PARTICULARLY FOR A BYPASS TURBOJET ENGINE simplified abstract (Airbus Operations SAS)
- 18454316. ACCRETION DETECTION SYSTEMS AND ASSOCIATED METHODS FOR GAS TURBINE ENGINES (RTX Corporation)
- 18466508. BUILT-IN TEST OF ACTIVELY CONTROLLED FUEL NOZZLES (RTX CORPORATION)
- 18472694. DETECTING GAS OR FUEL LEAKS IN A GAS TURBINE ENGINE (PRATT & WHITNEY CANADA CORP.)
- 18483722. INSPECTION SYSTEM FOR A GAS TURBINE ENGINE (RTX Corporation)
- 18678449. FIXTURE FOR COMPONENTS (ROLLS-ROYCE PLC)
B
P
R
- Raytheon technologies corporation (20240310246). MULTI-MEASUREMENT PROBE ASSEMBLY simplified abstract
- Raytheon technologies corporation (20240410787). MULTI INSTRUMENT EGRESS FOR GAS TURBINE ENGINE
- RAYTHEON TECHNOLOGIES CORPORATION patent applications on December 12th, 2024
- Raytheon Technologies Corporation patent applications on September 19th, 2024
- ROLLS-ROYCE plc (20250003826). METHOD OF DETERMINING A LOCATION OF A FAILURE EVENT IN A PRESSURISED FLUID DUCT
- Rtx corporation (20250067613). APPARATUS AND METHOD FOR PARTIALLY BLADED ROTOR TEST
- Rtx corporation (20250067625). OPTICAL DEFECT DETECTION SYSTEM
- Rtx corporation (20250067627). ACCRETION DETECTION SYSTEMS AND ASSOCIATED METHODS FOR GAS TURBINE ENGINES
- RTX Corporation patent applications on February 27th, 2025