Prosecution Insights
Prosecution Insights
Tech Center 3700 • Art Units: 3741
This examiner grants 51% of resolved cases
Lorne Edward Meade is a patent examiner in Tech Center 3700, working within Art Unit 3741. The examiner has 584 resolved cases and an allowance rate of 51.4 percent. This 51.4 percent rate reflects the proportion of applications that reach a grant. For the 584 cases handled, this data provides a basis for understanding the probability of success during the examination process. The volume of resolved cases reflects the examiner's experience within Tech Center 3700.
The median days to allowance for this examiner is 1204. This 1204-day timeline represents the duration for an application to move from filing to a grant. Applicants should consider this period when planning their patent strategy and resource allocation. The volume of 584 resolved cases suggests that this duration is a consistent aspect of the examiner's workflow in Art Unit 3741. This median provides a specific metric for evaluating the expected length of prosecution.
The data shows an interview lift of 38.7 percent. This 38.7 percent lift represents the change in the likelihood of allowance when an interview is conducted. It suggests that direct communication is a method for addressing the probability of a grant. For practitioners, utilizing an interview is an option to navigate the prosecution process and achieve a positive outcome. Practitioners can use this lift to evaluate the potential benefits of direct engagement.
| App # | Title | Status | Assignee |
|---|---|---|---|
| 19128451 | AERO-PROPULSION SYSTEM WITH IMPROVED PROPULSION EFFICIENCY | Non-Final OA | SAFRAN AIRCRAFT ENGINES |
| 18839893 | SOUND ABSORPTION DEVICE | Non-Final OA | Safran Nacelles |
| 18377186 | CIRCUMFERENTIALLY TAILORED INLET GUARD FOR AN AIRCRAFT ENGINE INLET | Final Rejection | Pratt & Whitney Canada Corp. |
| 17866103 | AIRCRAFT PROPULSION SYSTEM WITH INTERMITTENT COMBUSTION ENGINE(S) | Final Rejection | Pratt & Whitney Canada Corp. |
| 19253191 | SYSTEMS AND APPARATUS TO LUBRICATE A GAS TURBINE ENGINE VIA AN EXTERNAL PRESSURE SOURCE | Non-Final OA | General Electric Company |
| 18541974 | TURBINE-POWERED SYSTEM WITH THERMOELECTRIC COOLING | Final Rejection | Rolls-Royce North American Technologies Inc. |
| 17792402 | SATELLITE CONSTELLATION FORMING SYSTEM, SATELLITE CONSTELLATION FORMING METHOD, GROUND FACILITY, BUSINESS DEVICE, AND OPEN ARCHITECTURE DATA REPOSITORY | Final Rejection | Mitsubishi Electric Corporation |
| 18228841 | FUEL SUPPLY METHOD, FUEL SUPPLY SYSTEM, FUEL COMBUSTION SYSTEM PROVIDED WITH FUEL SUPPLY SYSTEM, AND GAS TURBINE PLANT | Final Rejection | MITSUBISHI HEAVY INDUSTRIES, LTD. |
| 19237616 | TURBOMACHINE COOLING AND ALTERNATIVE FUEL SUPPLY | Non-Final OA | GE Vernova Infrastructure Technology LLC |
| 18919910 | GAS TURBINE ENGINE WITH ELECTRICALLY DRIVEN COMPRESSOR | Non-Final OA | RTX Corporation |
| 18546893 | DEVICE AND METHOD FOR DIRECT ENERGY DEPOSITION ADDITIVE MANUFACTURING (DED) | Final Rejection | Linde GmbH |
| 18234723 | DIGITAL TWIN FOR LASER MATERIAL PROCESSING | Final Rejection | Applied Materials, Inc. |
| 18451688 | Multiple Wire Additive Manufacturing | Final Rejection | Relativity Space, Inc. |
| 18169533 | HYBRID EASY TO CLEAN COATING FOR MICROWAVE APPLIANCE | Non-Final OA | Whirlpool Corporation |
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