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] => 9542161
[patent_doc_number] => 20140166808
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-19
[patent_title] => 'Convertible cabin attendant seat'
[patent_app_type] => utility
[patent_app_number] => 14/107219
[patent_app_country] => US
[patent_app_date] => 2013-12-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 7449
[patent_no_of_claims] => 15
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14107219
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/107219 | Convertible cabin attendant seat | Dec 15, 2013 | Issued |
Array
(
[id] => 11634803
[patent_doc_number] => 09656760
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-05-23
[patent_title] => 'Variable geometry helicopter engine inlet'
[patent_app_type] => utility
[patent_app_number] => 14/074265
[patent_app_country] => US
[patent_app_date] => 2013-11-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 14
[patent_no_of_words] => 3486
[patent_no_of_claims] => 4
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 184
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 14074265
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/074265 | Variable geometry helicopter engine inlet | Nov 6, 2013 | Issued |
Array
(
[id] => 10070380
[patent_doc_number] => 09108719
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-08-18
[patent_title] => 'Aircraft with AFT split-level multi-deck fusealge'
[patent_app_type] => utility
[patent_app_number] => 13/973843
[patent_app_country] => US
[patent_app_date] => 2013-08-22
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 17
[patent_figures_cnt] => 33
[patent_no_of_words] => 12058
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 214
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13973843
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/973843 | Aircraft with AFT split-level multi-deck fusealge | Aug 21, 2013 | Issued |
Array
(
[id] => 9809490
[patent_doc_number] => 20150021435
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-01-22
[patent_title] => 'Apparatus for causing an aircraft wheel to rotate'
[patent_app_type] => utility
[patent_app_number] => 13/945762
[patent_app_country] => US
[patent_app_date] => 2013-07-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2274
[patent_no_of_claims] => 1
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13945762
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/945762 | Apparatus for causing an aircraft wheel to rotate | Jul 17, 2013 | Abandoned |
Array
(
[id] => 9104363
[patent_doc_number] => 20130277494
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-10-24
[patent_title] => 'Very Low Power Actuation Devices'
[patent_app_type] => utility
[patent_app_number] => 13/869934
[patent_app_country] => US
[patent_app_date] => 2013-04-24
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 29
[patent_figures_cnt] => 29
[patent_no_of_words] => 10031
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13869934
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/869934 | Very low power actuation devices | Apr 23, 2013 | Issued |
Array
(
[id] => 10587369
[patent_doc_number] => 09308970
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2016-04-12
[patent_title] => 'Net engagement with parachute slowdown (NEPS) system'
[patent_app_type] => utility
[patent_app_number] => 13/852832
[patent_app_country] => US
[patent_app_date] => 2013-03-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 20
[patent_no_of_words] => 5320
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 2
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[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13852832
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/852832 | Net engagement with parachute slowdown (NEPS) system | Mar 27, 2013 | Issued |
Array
(
[id] => 9000041
[patent_doc_number] => 20130221165
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-29
[patent_title] => 'OBLIQUE BLENDED WING BODY AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/784438
[patent_app_country] => US
[patent_app_date] => 2013-03-04
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 8368
[patent_no_of_claims] => 64
[patent_no_of_ind_claims] => 7
[patent_words_short_claim] => 0
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13784438
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/784438 | Oblique blended wing body aircraft | Mar 3, 2013 | Issued |
Array
(
[id] => 9854755
[patent_doc_number] => 20150034771
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2015-02-05
[patent_title] => 'DEVICE FOR SUPPLYING AIR TO AN AUXILIARY POWER UNIT OF AN AIRCRAFT AND ASSOCIATED AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 14/378065
[patent_app_country] => US
[patent_app_date] => 2013-02-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3036
[patent_no_of_claims] => 6
[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] =>[firstpage_image] =>[orig_patent_app_number] => 14378065
[rel_patent_id] =>[rel_patent_doc_number] =>) 14/378065 | DEVICE FOR SUPPLYING AIR TO AN AUXILIARY POWER UNIT OF AN AIRCRAFT AND ASSOCIATED AIRCRAFT | Feb 11, 2013 | Abandoned |
Array
(
[id] => 11894907
[patent_doc_number] => 09764830
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-09-19
[patent_title] => 'Pilot control system with adjustable pedals'
[patent_app_type] => utility
[patent_app_number] => 13/736169
[patent_app_country] => US
[patent_app_date] => 2013-01-08
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 23
[patent_no_of_words] => 10598
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13736169
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/736169 | Pilot control system with adjustable pedals | Jan 7, 2013 | Issued |
Array
(
[id] => 8838635
[patent_doc_number] => 20130134263
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-30
[patent_title] => 'WINGLESS HOVERING OF MICRO AIR VEHICLE'
[patent_app_type] => utility
[patent_app_number] => 13/720773
[patent_app_country] => US
[patent_app_date] => 2012-12-19
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 22
[patent_figures_cnt] => 22
[patent_no_of_words] => 7188
[patent_no_of_claims] => 43
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13720773
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/720773 | Wingless hovering of micro air vehicle | Dec 18, 2012 | Issued |
Array
(
[id] => 9517592
[patent_doc_number] => 20140154084
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-06-05
[patent_title] => 'NON-UNIFORM BLADE DISTRIBUTION FOR ROTARY WING AIRCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/689941
[patent_app_country] => US
[patent_app_date] => 2012-11-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2356
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
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[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13689941
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/689941 | Non-uniform blade distribution for rotary wing aircraft | Nov 29, 2012 | Issued |
Array
(
[id] => 9508535
[patent_doc_number] => 20140145026
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-29
[patent_title] => 'Unmanned Aerial Device'
[patent_app_type] => utility
[patent_app_number] => 13/687155
[patent_app_country] => US
[patent_app_date] => 2012-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2873
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13687155
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/687155 | Unmanned Aerial Device | Nov 27, 2012 | Abandoned |
Array
(
[id] => 9508542
[patent_doc_number] => 20140145033
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-05-29
[patent_title] => 'TENSIONING DEVICE FOR AIRCRAFT REFUELING BOOM HOIST'
[patent_app_type] => utility
[patent_app_number] => 13/687484
[patent_app_country] => US
[patent_app_date] => 2012-11-28
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 6
[patent_no_of_words] => 2277
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13687484
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/687484 | TENSIONING DEVICE FOR AIRCRAFT REFUELING BOOM HOIST | Nov 27, 2012 | Abandoned |
Array
(
[id] => 9013689
[patent_doc_number] => 20130228653
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-09-05
[patent_title] => 'ELECTROTHERMAL AND ELECTRO EXPULSIVE HYBRID ICE PROTECTION SYSTEM FOR ENGINE INLET'
[patent_app_type] => utility
[patent_app_number] => 13/678906
[patent_app_country] => US
[patent_app_date] => 2012-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13678906
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/678906 | ELECTROTHERMAL AND ELECTRO EXPULSIVE HYBRID ICE PROTECTION SYSTEM FOR ENGINE INLET | Nov 15, 2012 | Abandoned |
Array
(
[id] => 8838628
[patent_doc_number] => 20130134256
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-30
[patent_title] => 'ANTI-TORQUE DEVICE WITH LONGITUDINAL THRUST FOR A ROTORCRAFT'
[patent_app_type] => utility
[patent_app_number] => 13/678648
[patent_app_country] => US
[patent_app_date] => 2012-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 9817
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13678648
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/678648 | Anti-torque device with longitudinal thrust for a rotorcraft | Nov 15, 2012 | Issued |
Array
(
[id] => 12171810
[patent_doc_number] => 09889936
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2018-02-13
[patent_title] => 'Curved seating layout'
[patent_app_type] => utility
[patent_app_number] => 13/664361
[patent_app_country] => US
[patent_app_date] => 2012-10-30
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13664361
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/664361 | Curved seating layout | Oct 29, 2012 | Issued |
Array
(
[id] => 10554560
[patent_doc_number] => 09278757
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2016-03-08
[patent_title] => 'Aircraft cabin enabling passengers to be received on several levels and corresponding aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/655843
[patent_app_country] => US
[patent_app_date] => 2012-10-19
[patent_effective_date] => 0000-00-00
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13655843
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/655843 | Aircraft cabin enabling passengers to be received on several levels and corresponding aircraft | Oct 18, 2012 | Issued |
Array
(
[id] => 8825627
[patent_doc_number] => 20130126672
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-23
[patent_title] => 'ROTATABLE CABIN ATTENDANT SEAT AND AIRCRAFT MONUMENT ARRANGEMENT WITH A ROTATABLE CABIN ATTENDANT SEAT'
[patent_app_type] => utility
[patent_app_number] => 13/655076
[patent_app_country] => US
[patent_app_date] => 2012-10-18
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/655076 | Rotatable cabin attendant seat and aircraft monument arrangement with a rotatable cabin attendant seat | Oct 17, 2012 | Issued |
Array
(
[id] => 10083222
[patent_doc_number] => 09120560
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2015-09-01
[patent_title] => 'Vertical take-off and landing aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/648706
[patent_app_country] => US
[patent_app_date] => 2012-10-10
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13648706
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/648706 | Vertical take-off and landing aircraft | Oct 9, 2012 | Issued |
Array
(
[id] => 11698478
[patent_doc_number] => 09688379
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2017-06-27
[patent_title] => 'Actuation device for opening an emergency exit flap of a cockpit door'
[patent_app_type] => utility
[patent_app_number] => 13/630287
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13630287
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/630287 | Actuation device for opening an emergency exit flap of a cockpit door | Sep 27, 2012 | Issued |