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 number | Title of the application | Filing Date | Status |
---|---|---|---|
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
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[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
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[patent_no_of_words] => 2079
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[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
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[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
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[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
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[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
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[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 |