Search

Raymond W. Addie

Examiner (ID: 17107)

Most Active Art Unit
3671
Art Unit(s)
3635, 3616, 3673, 3671
Total Applications
2996
Issued Applications
2368
Pending Applications
189
Abandoned Applications
481

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 18005749 [patent_doc_number] => 20220364515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-11-17 [patent_title] => ADAPTED PROCESS CONCEPT AND PERFORMANCE CONCEPT FOR ENGINES (E.G. ROCKETS), AIR-BREATHING PROPULSION SYSTEMS (E.G. SUBSONIC RAMJETS, RAMJETS, ROCKET RAMJETS), TURBOPUMPS OR NOZZLES (E.G. BELL NOZZLES, AEROSPIKES) [patent_app_type] => utility [patent_app_number] => 17/656459 [patent_app_country] => US [patent_app_date] => 2022-03-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6526 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -12 [patent_words_short_claim] => 132 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17656459 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/656459
ADAPTED PROCESS CONCEPT AND PERFORMANCE CONCEPT FOR ENGINES (E.G. ROCKETS), AIR-BREATHING PROPULSION SYSTEMS (E.G. SUBSONIC RAMJETS, RAMJETS, ROCKET RAMJETS), TURBOPUMPS OR NOZZLES (E.G. BELL NOZZLES, AEROSPIKES) Mar 24, 2022 Abandoned
Array ( [id] => 18583551 [patent_doc_number] => 20230265812 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-08-24 [patent_title] => Variable Area Fan Nozzle Actuation System [patent_app_type] => utility [patent_app_number] => 17/694479 [patent_app_country] => US [patent_app_date] => 2022-03-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5921 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17694479 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/694479
Variable area fan nozzle actuation system Mar 13, 2022 Issued
Array ( [id] => 19156658 [patent_doc_number] => 20240149365 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-05-09 [patent_title] => GAS-SHIELDED ARC WELDING METHOD, WELDED JOINT, AND WELDED JOINT PRODUCTION METHOD [patent_app_type] => utility [patent_app_number] => 18/279800 [patent_app_country] => US [patent_app_date] => 2022-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5778 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 85 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18279800 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/279800
GAS-SHIELDED ARC WELDING METHOD, WELDED JOINT, AND WELDED JOINT PRODUCTION METHOD Mar 10, 2022 Pending
Array ( [id] => 18613299 [patent_doc_number] => 20230280035 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-09-07 [patent_title] => BIMODAL COMBUSTION SYSTEM [patent_app_type] => utility [patent_app_number] => 17/687873 [patent_app_country] => US [patent_app_date] => 2022-03-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 22616 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 114 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17687873 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/687873
BIMODAL COMBUSTION SYSTEM Mar 6, 2022 Abandoned
Array ( [id] => 19232757 [patent_doc_number] => 20240189949 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2024-06-13 [patent_title] => WELDING ELECTRODE AND SPOT-WELDING DEVICE [patent_app_type] => utility [patent_app_number] => 18/279643 [patent_app_country] => US [patent_app_date] => 2022-02-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5888 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18279643 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/279643
WELDING ELECTRODE AND SPOT-WELDING DEVICE Feb 15, 2022 Pending
Array ( [id] => 17930768 [patent_doc_number] => 20220325893 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-13 [patent_title] => CHAMBER FOR ROTATING DETONATION ENGINE AND WALL OBSTACLES FOR SAME [patent_app_type] => utility [patent_app_number] => 17/670575 [patent_app_country] => US [patent_app_date] => 2022-02-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3673 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -17 [patent_words_short_claim] => 98 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17670575 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/670575
CHAMBER FOR ROTATING DETONATION ENGINE AND WALL OBSTACLES FOR SAME Feb 13, 2022 Abandoned
Array ( [id] => 17946532 [patent_doc_number] => 20220333550 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-20 [patent_title] => POSITION SENSOR FOR AIRCRAFT NACELLE THRUST REVERSER DOOR [patent_app_type] => utility [patent_app_number] => 17/666244 [patent_app_country] => US [patent_app_date] => 2022-02-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3646 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -19 [patent_words_short_claim] => 79 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17666244 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/666244
Position sensor for aircraft nacelle thrust reverser door Feb 6, 2022 Issued
Array ( [id] => 17762115 [patent_doc_number] => 20220235727 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-28 [patent_title] => ROTATING DETONATION ENGINE [patent_app_type] => utility [patent_app_number] => 17/582408 [patent_app_country] => US [patent_app_date] => 2022-01-24 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3962 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -26 [patent_words_short_claim] => 78 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17582408 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/582408
ROTATING DETONATION ENGINE Jan 23, 2022 Abandoned
Array ( [id] => 17750336 [patent_doc_number] => 20220228541 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-07-21 [patent_title] => TURBOFAN ENGINE COMPRISING A SYSTEM FOR BLOCKING THE FLOW PATH OF THE BYPASS STREAM COMPRISING VEILS [patent_app_type] => utility [patent_app_number] => 17/580110 [patent_app_country] => US [patent_app_date] => 2022-01-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 5744 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 411 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17580110 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/580110
Turbofan engine comprising a system for blocking the flow path of the bypass stream comprising veils Jan 19, 2022 Issued
Array ( [id] => 17483285 [patent_doc_number] => 20220090789 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-24 [patent_title] => ISOLATION SECTION SUPPRESSING SHOCK WAVE FORWARD TRANSMISSION STRUCTURE FOR WAVE ROTOR COMBUSTOR AND WAVE ROTOR COMBUSTOR [patent_app_type] => utility [patent_app_number] => 17/544315 [patent_app_country] => US [patent_app_date] => 2021-12-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3557 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -8 [patent_words_short_claim] => 150 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17544315 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/544315
Isolation section suppressing shock wave forward transmission structure for wave rotor combustor and wave rotor combustor Dec 6, 2021 Issued
Array ( [id] => 18420996 [patent_doc_number] => 20230175459 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-06-08 [patent_title] => PLURALITY OF AIRBREATHING AND NON-AIRBREATHING ENGINES [patent_app_type] => utility [patent_app_number] => 17/457653 [patent_app_country] => US [patent_app_date] => 2021-12-04 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3002 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -5 [patent_words_short_claim] => 62 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17457653 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/457653
PLURALITY OF AIRBREATHING AND NON-AIRBREATHING ENGINES Dec 3, 2021 Abandoned
Array ( [id] => 17474560 [patent_doc_number] => 20220082064 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-03-17 [patent_title] => AIRCRAFT PROPULSION UNIT [patent_app_type] => utility [patent_app_number] => 17/536480 [patent_app_country] => US [patent_app_date] => 2021-11-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4003 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -14 [patent_words_short_claim] => 113 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17536480 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/536480
Aircraft propulsion unit Nov 28, 2021 Issued
Array ( [id] => 19970169 [patent_doc_number] => 12338767 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-06-24 [patent_title] => Gas turbine inlet cooling for constant power output [patent_app_type] => utility [patent_app_number] => 18/037161 [patent_app_country] => US [patent_app_date] => 2021-10-13 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2243 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 658 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18037161 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/037161
Gas turbine inlet cooling for constant power output Oct 12, 2021 Issued
Array ( [id] => 18785771 [patent_doc_number] => 20230373645 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-11-23 [patent_title] => COOLING SYSTEM OF A COMPARTMENT OF PIECES OF EQUIPMENT IN A NACELLE OF AN AIRCRAFT PROPELLING ASSEMBLY [patent_app_type] => utility [patent_app_number] => 18/044958 [patent_app_country] => US [patent_app_date] => 2021-10-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 7634 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -11 [patent_words_short_claim] => 2 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18044958 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/044958
Cooling system of a compartment of pieces of equipment in a nacelle of an aircraft propelling assembly Sep 30, 2021 Issued
Array ( [id] => 18692189 [patent_doc_number] => 20230322418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-10-12 [patent_title] => PLANAR ELECTRIC MOTOR FOR AEROSPACE USE [patent_app_type] => utility [patent_app_number] => 18/043583 [patent_app_country] => US [patent_app_date] => 2021-09-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 4632 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -7 [patent_words_short_claim] => 205 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18043583 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/043583
PLANAR ELECTRIC MOTOR FOR AEROSPACE USE Sep 1, 2021 Pending
Array ( [id] => 18862718 [patent_doc_number] => 20230417154 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-28 [patent_title] => METHOD FOR CREATING MAXIMUM OUTPUT IN GAS TURBINE, METHOD FOR CREATING OUTPUT FOR CONTROLLING GAS TURBINE, METHOD FOR CONTROLLING GAS TURBINE, DEVICE FOR EXECUTING SAID METHODS, AND PROGRAM FOR CAUSING COMPUTER TO EXECUTE SAID METHODS [patent_app_type] => utility [patent_app_number] => 18/033700 [patent_app_country] => US [patent_app_date] => 2021-07-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 26772 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -24 [patent_words_short_claim] => 215 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18033700 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/033700
Method for creating maximum output in gas turbine, method for creating output for controlling gas turbine, method for controlling gas turbine, device for executing said methods, and program for causing computer to execute said methods Jul 25, 2021 Issued
Array ( [id] => 19731565 [patent_doc_number] => 12209556 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2025-01-28 [patent_title] => Thrust reverser provided with a lightweight thrust reverser flap [patent_app_type] => utility [patent_app_number] => 17/340533 [patent_app_country] => US [patent_app_date] => 2021-06-07 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 7 [patent_no_of_words] => 3716 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 271 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17340533 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/340533
Thrust reverser provided with a lightweight thrust reverser flap Jun 6, 2021 Issued
Array ( [id] => 18247218 [patent_doc_number] => 11603794 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2023-03-14 [patent_title] => Method and apparatus for increasing useful energy/thrust of a gas turbine engine by one or more rotating fluid moving (agitator) pieces due to formation of a defined steam region [patent_app_type] => utility [patent_app_number] => 17/233993 [patent_app_country] => US [patent_app_date] => 2021-04-19 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 17 [patent_no_of_words] => 8417 [patent_no_of_claims] => 19 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 286 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17233993 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/233993
Method and apparatus for increasing useful energy/thrust of a gas turbine engine by one or more rotating fluid moving (agitator) pieces due to formation of a defined steam region Apr 18, 2021 Issued
Array ( [id] => 17930552 [patent_doc_number] => 20220325677 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2022-10-13 [patent_title] => ADJUSTABLE EXHAUST NOZZLE FOR DETONATION ENGINES [patent_app_type] => utility [patent_app_number] => 17/228682 [patent_app_country] => US [patent_app_date] => 2021-04-12 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 6376 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -18 [patent_words_short_claim] => 183 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 17228682 [rel_patent_id] =>[rel_patent_doc_number] =>)
17/228682
ADJUSTABLE EXHAUST NOZZLE FOR DETONATION ENGINES Apr 11, 2021 Abandoned
Array ( [id] => 18831458 [patent_doc_number] => 20230399985 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2023-12-14 [patent_title] => METHOD FOR KEEPING COMBUSTION OF GAS TURBINE STABLE IN DYNAMIC PROCESS, COMPUTER READABLE MEDIUM, AND GAS TURBINE CONTROL SYSTEM [patent_app_type] => utility [patent_app_number] => 18/036162 [patent_app_country] => US [patent_app_date] => 2021-03-11 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 0 [patent_figures_cnt] => 0 [patent_no_of_words] => 3839 [patent_no_of_claims] => 0 [patent_no_of_ind_claims] => -9 [patent_words_short_claim] => 135 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 18036162 [rel_patent_id] =>[rel_patent_doc_number] =>)
18/036162
METHOD FOR KEEPING COMBUSTION OF GAS TURBINE STABLE IN DYNAMIC PROCESS, COMPUTER READABLE MEDIUM, AND GAS TURBINE CONTROL SYSTEM Mar 10, 2021 Abandoned
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