Search

David M Gray

Supervisory Patent Examiner (ID: 13237, Phone: (571)272-2119 , Office: P/2852 )

Most Active Art Unit
2851
Art Unit(s)
2851, 2101, 2602, 2853, 2852
Total Applications
2033
Issued Applications
1687
Pending Applications
28
Abandoned Applications
298

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 9374065 [patent_doc_number] => 08678316 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-03-25 [patent_title] => 'Amorphous metal riblets' [patent_app_type] => utility [patent_app_number] => 12/361918 [patent_app_country] => US [patent_app_date] => 2009-01-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 18 [patent_no_of_words] => 6211 [patent_no_of_claims] => 4 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 71 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12361918 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/361918
Amorphous metal riblets Jan 28, 2009 Issued
Array ( [id] => 6430636 [patent_doc_number] => 20100187365 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'CRYOGENIC PROPELLANT DEPOT AND DEPLOYABLE SUNSHIELD' [patent_app_type] => utility [patent_app_number] => 12/359033 [patent_app_country] => US [patent_app_date] => 2009-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 5841 [patent_no_of_claims] => 22 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0187/20100187365.pdf [firstpage_image] =>[orig_patent_app_number] => 12359033 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/359033
CRYOGENIC PROPELLANT DEPOT AND DEPLOYABLE SUNSHIELD Jan 22, 2009 Abandoned
Array ( [id] => 6430629 [patent_doc_number] => 20100187364 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-07-29 [patent_title] => 'CRYOGENIC PROPELLANT DEPOT AND INTEGRAL SUNSHIELD' [patent_app_type] => utility [patent_app_number] => 12/359015 [patent_app_country] => US [patent_app_date] => 2009-01-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 17 [patent_no_of_words] => 5841 [patent_no_of_claims] => 14 [patent_no_of_ind_claims] => 5 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0187/20100187364.pdf [firstpage_image] =>[orig_patent_app_number] => 12359015 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/359015
CRYOGENIC PROPELLANT DEPOT AND INTEGRAL SUNSHIELD Jan 22, 2009 Abandoned
Array ( [id] => 8894975 [patent_doc_number] => 08474486 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-07-02 [patent_title] => 'Actuator system' [patent_app_type] => utility [patent_app_number] => 12/350479 [patent_app_country] => US [patent_app_date] => 2009-01-08 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 18 [patent_no_of_words] => 3549 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 145 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12350479 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/350479
Actuator system Jan 7, 2009 Issued
Array ( [id] => 5352864 [patent_doc_number] => 20090184208 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-07-23 [patent_title] => 'AERODYNAMIC SEALING MEMBER FOR AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/349054 [patent_app_country] => US [patent_app_date] => 2009-01-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2305 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0184/20090184208.pdf [firstpage_image] =>[orig_patent_app_number] => 12349054 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/349054
Aerodynamic sealing member for aircraft Jan 5, 2009 Issued
Array ( [id] => 7659149 [patent_doc_number] => 20110308418 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-12-22 [patent_title] => 'Projectile Having Deployable Fin' [patent_app_type] => utility [patent_app_number] => 12/344245 [patent_app_country] => US [patent_app_date] => 2008-12-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4377 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0308/20110308418.pdf [firstpage_image] =>[orig_patent_app_number] => 12344245 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/344245
Projectile having deployable fin Dec 24, 2008 Issued
Array ( [id] => 6421043 [patent_doc_number] => 20100102174 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-04-29 [patent_title] => 'Wingless Hovering Of Micro Air Vehicle' [patent_app_type] => utility [patent_app_number] => 12/342583 [patent_app_country] => US [patent_app_date] => 2008-12-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 22 [patent_figures_cnt] => 22 [patent_no_of_words] => 7174 [patent_no_of_claims] => 42 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0102/20100102174.pdf [firstpage_image] =>[orig_patent_app_number] => 12342583 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/342583
Wingless hovering of micro air vehicle Dec 22, 2008 Issued
Array ( [id] => 5499065 [patent_doc_number] => 20090159753 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-06-25 [patent_title] => 'MOMENTUM MANAGEMENT SYSTEM FOR REACTION WHEEL BY USING NULL SPACE VECTOR AND METHOD' [patent_app_type] => utility [patent_app_number] => 12/341393 [patent_app_country] => US [patent_app_date] => 2008-12-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 2596 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0159/20090159753.pdf [firstpage_image] =>[orig_patent_app_number] => 12341393 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/341393
MOMENTUM MANAGEMENT SYSTEM FOR REACTION WHEEL BY USING NULL SPACE VECTOR AND METHOD Dec 21, 2008 Abandoned
Array ( [id] => 8576239 [patent_doc_number] => 08342444 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2013-01-01 [patent_title] => 'Fail safe extended torque box strut-to-wing mount' [patent_app_type] => utility [patent_app_number] => 12/336213 [patent_app_country] => US [patent_app_date] => 2008-12-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 11 [patent_figures_cnt] => 13 [patent_no_of_words] => 5504 [patent_no_of_claims] => 21 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 207 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12336213 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/336213
Fail safe extended torque box strut-to-wing mount Dec 15, 2008 Issued
Array ( [id] => 6090462 [patent_doc_number] => 20110001002 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2011-01-06 [patent_title] => 'SUSPENSION FOR MOUNTING A TURBOJET ENGINE ON AN AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/329136 [patent_app_country] => US [patent_app_date] => 2008-12-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 3794 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0001/20110001002.pdf [firstpage_image] =>[orig_patent_app_number] => 12329136 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/329136
Suspension for mounting a turbojet engine on an aircraft Dec 4, 2008 Issued
Array ( [id] => 9284667 [patent_doc_number] => 08640986 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-04 [patent_title] => 'Turbojet nacelle and method for controlling separation in a turbojet nacelle' [patent_app_type] => utility [patent_app_number] => 12/326604 [patent_app_country] => US [patent_app_date] => 2008-12-02 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 15 [patent_no_of_words] => 3604 [patent_no_of_claims] => 13 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 87 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12326604 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/326604
Turbojet nacelle and method for controlling separation in a turbojet nacelle Dec 1, 2008 Issued
Array ( [id] => 6546356 [patent_doc_number] => 20100127116 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-05-27 [patent_title] => 'NACELLE AND METHOD OF ASSEMBLING THE SAME' [patent_app_type] => utility [patent_app_number] => 12/324429 [patent_app_country] => US [patent_app_date] => 2008-11-26 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 9 [patent_no_of_words] => 5358 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0127/20100127116.pdf [firstpage_image] =>[orig_patent_app_number] => 12324429 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/324429
Nacelle and method of assembling the same Nov 25, 2008 Issued
Array ( [id] => 6445163 [patent_doc_number] => 20100038471 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'Suspension system for aircraft auxiliary power unit with elastomeric member' [patent_app_type] => utility [patent_app_number] => 12/288434 [patent_app_country] => US [patent_app_date] => 2008-10-20 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 15 [patent_no_of_words] => 40614 [patent_no_of_claims] => 44 [patent_no_of_ind_claims] => 6 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038471.pdf [firstpage_image] =>[orig_patent_app_number] => 12288434 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/288434
Suspension system for aircraft auxiliary power unit with elastomeric member Oct 19, 2008 Issued
Array ( [id] => 7549317 [patent_doc_number] => 08061646 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2011-11-22 [patent_title] => 'Wing tip docking system for aircraft' [patent_app_type] => utility [patent_app_number] => 12/210711 [patent_app_country] => US [patent_app_date] => 2008-09-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 6630 [patent_no_of_claims] => 12 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 218 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] => patents/08/061/08061646.pdf [firstpage_image] =>[orig_patent_app_number] => 12210711 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/210711
Wing tip docking system for aircraft Sep 14, 2008 Issued
Array ( [id] => 5461375 [patent_doc_number] => 20090321575 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2009-12-31 [patent_title] => 'STRUCTURE OF AN AIRCRAFT AEROFOIL' [patent_app_type] => utility [patent_app_number] => 12/201310 [patent_app_country] => US [patent_app_date] => 2008-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 5 [patent_figures_cnt] => 5 [patent_no_of_words] => 2079 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0321/20090321575.pdf [firstpage_image] =>[orig_patent_app_number] => 12201310 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/201310
STRUCTURE OF AN AIRCRAFT AEROFOIL Aug 28, 2008 Abandoned
Array ( [id] => 6319836 [patent_doc_number] => 20100243795 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-09-30 [patent_title] => 'OBLIQUE BLENDED WING BODY AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/675165 [patent_app_country] => US [patent_app_date] => 2008-08-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 8297 [patent_no_of_claims] => 26 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0243/20100243795.pdf [firstpage_image] =>[orig_patent_app_number] => 12675165 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/675165
Oblique blended wing body aircraft Aug 28, 2008 Issued
Array ( [id] => 6215401 [patent_doc_number] => 20100051749 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-03-04 [patent_title] => 'AIRCRAFT SPILLOVER FUEL TANK' [patent_app_type] => utility [patent_app_number] => 12/199069 [patent_app_country] => US [patent_app_date] => 2008-08-27 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 7 [patent_no_of_words] => 4908 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0051/20100051749.pdf [firstpage_image] =>[orig_patent_app_number] => 12199069 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/199069
Aircraft spillover fuel tank Aug 26, 2008 Issued
Array ( [id] => 6541675 [patent_doc_number] => 20100044515 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-25 [patent_title] => 'CONTINUAL TRANSFERENCE OF FUEL BETWEEN FUEL TANKS AT A RATE COMMENSURATE WITH FUEL BURN DURING CRUISE FLIGHT OPERATION TO MAINTAIN THE AIRCRAFT CENTER OF GRAVITY WITHIN A PRE-SELECTED AFT CENTER OF GRAVITY ENVELOPE' [patent_app_type] => utility [patent_app_number] => 12/197737 [patent_app_country] => US [patent_app_date] => 2008-08-25 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 4172 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0044/20100044515.pdf [firstpage_image] =>[orig_patent_app_number] => 12197737 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/197737
Continuous fuel management system for automatic control of aircraft center of gravity Aug 24, 2008 Issued
Array ( [id] => 6445334 [patent_doc_number] => 20100038492 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'RETRACTABLE NACELLE CHINE' [patent_app_type] => utility [patent_app_number] => 12/192407 [patent_app_country] => US [patent_app_date] => 2008-08-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 8 [patent_figures_cnt] => 8 [patent_no_of_words] => 5878 [patent_no_of_claims] => 20 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038492.pdf [firstpage_image] =>[orig_patent_app_number] => 12192407 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/192407
Retractable nacelle chine Aug 14, 2008 Issued
Array ( [id] => 6445240 [patent_doc_number] => 20100038480 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2010-02-18 [patent_title] => 'JET/EFFLUX OUTWASH BARRIER SYSTEM FOR STOVL, TILTROTOR, AND HELICOPTER AIRCRAFT' [patent_app_type] => utility [patent_app_number] => 12/191914 [patent_app_country] => US [patent_app_date] => 2008-08-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 6 [patent_figures_cnt] => 6 [patent_no_of_words] => 5153 [patent_no_of_claims] => 45 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 0 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => publication [pdf_file] => publications/A1/0038/20100038480.pdf [firstpage_image] =>[orig_patent_app_number] => 12191914 [rel_patent_id] =>[rel_patent_doc_number] =>)
12/191914
JET/EFFLUX OUTWASH BARRIER SYSTEM FOR STOVL, TILTROTOR, AND HELICOPTER AIRCRAFT Aug 13, 2008 Abandoned
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