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] => 6602577
[patent_doc_number] => 20100170986
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-07-08
[patent_title] => 'AIRCRAFT STRUCTURAL ELEMENT LOCATED AT THE INTERFACE BETWEEN A WING AND THE FUSELAGE'
[patent_app_type] => utility
[patent_app_number] => 12/601170
[patent_app_country] => US
[patent_app_date] => 2008-05-13
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 3646
[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] => publications/A1/0170/20100170986.pdf
[firstpage_image] =>[orig_patent_app_number] => 12601170
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/601170 | Aircraft structural element located at the interface between a wing and the fuselage | May 12, 2008 | Issued |
Array
(
[id] => 4633168
[patent_doc_number] => 08011613
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-06
[patent_title] => 'Aircraft with reduced environmental impact'
[patent_app_type] => utility
[patent_app_number] => 12/106485
[patent_app_country] => US
[patent_app_date] => 2008-04-21
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 7
[patent_no_of_words] => 2602
[patent_no_of_claims] => 9
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 155
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/011/08011613.pdf
[firstpage_image] =>[orig_patent_app_number] => 12106485
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/106485 | Aircraft with reduced environmental impact | Apr 20, 2008 | Issued |
Array
(
[id] => 6398618
[patent_doc_number] => 20100147997
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2010-06-17
[patent_title] => 'AIRCRAFT ENGINE ATTACHMENT PYLON HAVING A REAR ENGINE ATTACHMENT PROVIDED WITH A SELF-LOCKING NUT'
[patent_app_type] => utility
[patent_app_number] => 12/596085
[patent_app_country] => US
[patent_app_date] => 2008-04-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 4870
[patent_no_of_claims] => 11
[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/A1/0147/20100147997.pdf
[firstpage_image] =>[orig_patent_app_number] => 12596085
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/596085 | Aircraft engine attachment pylon having a rear engine attachment provided with a self-locking nut | Apr 17, 2008 | Issued |
Array
(
[id] => 4633169
[patent_doc_number] => 08011614
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-09-06
[patent_title] => 'Bird vortex flying machine'
[patent_app_type] => utility
[patent_app_number] => 12/100901
[patent_app_country] => US
[patent_app_date] => 2008-04-10
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 3286
[patent_no_of_claims] => 16
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 198
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/011/08011614.pdf
[firstpage_image] =>[orig_patent_app_number] => 12100901
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/100901 | Bird vortex flying machine | Apr 9, 2008 | Issued |
Array
(
[id] => 8919549
[patent_doc_number] => 08485473
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2013-07-16
[patent_title] => 'Method and device for detecting rime and/or rime conditions on a flying aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/594822
[patent_app_country] => US
[patent_app_date] => 2008-04-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 6
[patent_no_of_words] => 8510
[patent_no_of_claims] => 12
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 216
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12594822
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/594822 | Method and device for detecting rime and/or rime conditions on a flying aircraft | Apr 8, 2008 | Issued |
Array
(
[id] => 4594068
[patent_doc_number] => 07980514
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-07-19
[patent_title] => 'Solar array momentum control'
[patent_app_type] => utility
[patent_app_number] => 12/048981
[patent_app_country] => US
[patent_app_date] => 2008-03-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 6
[patent_figures_cnt] => 7
[patent_no_of_words] => 7236
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 82
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/07/980/07980514.pdf
[firstpage_image] =>[orig_patent_app_number] => 12048981
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/048981 | Solar array momentum control | Mar 13, 2008 | Issued |
Array
(
[id] => 10896492
[patent_doc_number] => 08919693
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-30
[patent_title] => 'Lockable guiding system for a mobile part of a nacelle'
[patent_app_type] => utility
[patent_app_number] => 12/531526
[patent_app_country] => US
[patent_app_date] => 2008-03-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 8
[patent_no_of_words] => 3611
[patent_no_of_claims] => 11
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 173
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 12531526
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/531526 | Lockable guiding system for a mobile part of a nacelle | Mar 6, 2008 | Issued |
Array
(
[id] => 5431887
[patent_doc_number] => 20090166473
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-02
[patent_title] => 'Optimized aircraft manhole'
[patent_app_type] => utility
[patent_app_number] => 12/072691
[patent_app_country] => US
[patent_app_date] => 2008-02-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 1670
[patent_no_of_claims] => 10
[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/A1/0166/20090166473.pdf
[firstpage_image] =>[orig_patent_app_number] => 12072691
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/072691 | Optimized aircraft manhole | Feb 26, 2008 | Issued |
Array
(
[id] => 5352168
[patent_doc_number] => 20090183512
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-07-23
[patent_title] => 'MOUNTING SYSTEM FOR A GAS TURBINE ENGINE'
[patent_app_type] => utility
[patent_app_number] => 12/016337
[patent_app_country] => US
[patent_app_date] => 2008-01-18
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2789
[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/A1/0183/20090183512.pdf
[firstpage_image] =>[orig_patent_app_number] => 12016337
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/016337 | Mounting system for a gas turbine engine | Jan 17, 2008 | Issued |
Array
(
[id] => 7709191
[patent_doc_number] => 08091827
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-01-10
[patent_title] => 'Thrust reverser door'
[patent_app_type] => utility
[patent_app_number] => 11/941360
[patent_app_country] => US
[patent_app_date] => 2007-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 12
[patent_no_of_words] => 3296
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 95
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/091/08091827.pdf
[firstpage_image] =>[orig_patent_app_number] => 11941360
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/941360 | Thrust reverser door | Nov 15, 2007 | Issued |
Array
(
[id] => 7544122
[patent_doc_number] => 08052086
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2011-11-08
[patent_title] => 'Thrust reverser door'
[patent_app_type] => utility
[patent_app_number] => 11/941391
[patent_app_country] => US
[patent_app_date] => 2007-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 10
[patent_no_of_words] => 3125
[patent_no_of_claims] => 28
[patent_no_of_ind_claims] => 5
[patent_words_short_claim] => 103
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/052/08052086.pdf
[firstpage_image] =>[orig_patent_app_number] => 11941391
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/941391 | Thrust reverser door | Nov 15, 2007 | Issued |
Array
(
[id] => 8161113
[patent_doc_number] => 08172175
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2012-05-08
[patent_title] => 'Pivoting door thrust reverser for a turbofan gas turbine engine'
[patent_app_type] => utility
[patent_app_number] => 11/941371
[patent_app_country] => US
[patent_app_date] => 2007-11-16
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 9
[patent_no_of_words] => 3263
[patent_no_of_claims] => 27
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 91
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] => patents/08/172/08172175.pdf
[firstpage_image] =>[orig_patent_app_number] => 11941371
[rel_patent_id] =>[rel_patent_doc_number] =>) 11/941371 | Pivoting door thrust reverser for a turbofan gas turbine engine | Nov 15, 2007 | Issued |
Array
(
[id] => 4775663
[patent_doc_number] => 20080283661
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-11-20
[patent_title] => 'Remote Controlled Mobile Platform'
[patent_app_type] => utility
[patent_app_number] => 12/092078
[patent_app_country] => US
[patent_app_date] => 2007-07-30
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 6583
[patent_no_of_claims] => 66
[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/A1/0283/20080283661.pdf
[firstpage_image] =>[orig_patent_app_number] => 12092078
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/092078 | Remote Controlled Mobile Platform | Jul 29, 2007 | Abandoned |
Array
(
[id] => 5549650
[patent_doc_number] => 20090283636
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2009-11-19
[patent_title] => 'Module for an Aircraft'
[patent_app_type] => utility
[patent_app_number] => 12/087328
[patent_app_country] => US
[patent_app_date] => 2006-12-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 16
[patent_figures_cnt] => 16
[patent_no_of_words] => 6230
[patent_no_of_claims] => 29
[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/A1/0283/20090283636.pdf
[firstpage_image] =>[orig_patent_app_number] => 12087328
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/087328 | Module for an aircraft | Dec 26, 2006 | Issued |
Array
(
[id] => 4883673
[patent_doc_number] => 20080258005
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2008-10-23
[patent_title] => 'Aircraft Having a Reduced Environmental Impact'
[patent_app_type] => utility
[patent_app_number] => 12/091286
[patent_app_country] => US
[patent_app_date] => 2006-10-23
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 7
[patent_no_of_words] => 2084
[patent_no_of_claims] => 11
[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/A1/0258/20080258005.pdf
[firstpage_image] =>[orig_patent_app_number] => 12091286
[rel_patent_id] =>[rel_patent_doc_number] =>) 12/091286 | Aircraft having a reduced environmental impact | Oct 22, 2006 | Issued |