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] => 9748592
[patent_doc_number] => 08840057
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-09-23
[patent_title] => 'Hybrid aircraft having a rotary wing'
[patent_app_type] => utility
[patent_app_number] => 13/628525
[patent_app_country] => US
[patent_app_date] => 2012-09-27
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
[patent_figures_cnt] => 1
[patent_no_of_words] => 4773
[patent_no_of_claims] => 19
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 283
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13628525
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/628525 | Hybrid aircraft having a rotary wing | Sep 26, 2012 | Issued |
Array
(
[id] => 8729969
[patent_doc_number] => 20130075538
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-03-28
[patent_title] => 'Transport Aircraft Hull Attachment System'
[patent_app_type] => utility
[patent_app_number] => 13/626036
[patent_app_country] => US
[patent_app_date] => 2012-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 10
[patent_figures_cnt] => 10
[patent_no_of_words] => 9152
[patent_no_of_claims] => 32
[patent_no_of_ind_claims] => 2
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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] => 13626036
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/626036 | Transport Aircraft Hull Attachment System | Sep 24, 2012 | Abandoned |
Array
(
[id] => 9380633
[patent_doc_number] => 20140084114
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-27
[patent_title] => 'VTOL Aircraft with Propeller tiltable around two Axes and a retractable Rotor'
[patent_app_type] => utility
[patent_app_number] => 13/626008
[patent_app_country] => US
[patent_app_date] => 2012-09-25
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 11
[patent_figures_cnt] => 11
[patent_no_of_words] => 3265
[patent_no_of_claims] => 8
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13626008
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/626008 | VTOL Aircraft with Propeller tiltable around two Axes and a retractable Rotor | Sep 24, 2012 | Abandoned |
Array
(
[id] => 11698483
[patent_doc_number] => 09688384
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2017-06-27
[patent_title] => 'Methods and apparatus to control a gap between movable aircraft wing components'
[patent_app_type] => utility
[patent_app_number] => 13/623597
[patent_app_country] => US
[patent_app_date] => 2012-09-20
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
[patent_figures_cnt] => 8
[patent_no_of_words] => 4183
[patent_no_of_claims] => 20
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 188
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13623597
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/623597 | Methods and apparatus to control a gap between movable aircraft wing components | Sep 19, 2012 | Issued |
Array
(
[id] => 9400059
[patent_doc_number] => 08690105
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-04-08
[patent_title] => 'Parachute'
[patent_app_type] => utility
[patent_app_number] => 13/619987
[patent_app_country] => US
[patent_app_date] => 2012-09-14
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 4
[patent_figures_cnt] => 4
[patent_no_of_words] => 1824
[patent_no_of_claims] => 6
[patent_no_of_ind_claims] => 1
[patent_words_short_claim] => 202
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13619987
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/619987 | Parachute | Sep 13, 2012 | Issued |
Array
(
[id] => 10862359
[patent_doc_number] => 08888043
[patent_country] => US
[patent_kind] => B1
[patent_issue_date] => 2014-11-18
[patent_title] => 'Crew bunk system and method'
[patent_app_type] => utility
[patent_app_number] => 13/610883
[patent_app_country] => US
[patent_app_date] => 2012-09-12
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 18
[patent_figures_cnt] => 20
[patent_no_of_words] => 7523
[patent_no_of_claims] => 18
[patent_no_of_ind_claims] => 3
[patent_words_short_claim] => 193
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13610883
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/610883 | Crew bunk system and method | Sep 11, 2012 | Issued |
Array
(
[id] => 8764751
[patent_doc_number] => 20130092788
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-18
[patent_title] => 'SUSPENSION SYSTEM FOR AIRCRAFT AUXILIARY POWER UNIT WITH ELASTOMERIC MEMBER'
[patent_app_type] => utility
[patent_app_number] => 13/606607
[patent_app_country] => US
[patent_app_date] => 2012-09-07
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 15
[patent_figures_cnt] => 15
[patent_no_of_words] => 40609
[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] =>[firstpage_image] =>[orig_patent_app_number] => 13606607
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/606607 | SUSPENSION SYSTEM FOR AIRCRAFT AUXILIARY POWER UNIT WITH ELASTOMERIC MEMBER | Sep 6, 2012 | Abandoned |
Array
(
[id] => 9334591
[patent_doc_number] => 20140061373
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-03-06
[patent_title] => 'CONTROLS FOR AIRCRAFT E-TAXI'
[patent_app_type] => utility
[patent_app_number] => 13/600343
[patent_app_country] => US
[patent_app_date] => 2012-08-31
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 2
[patent_figures_cnt] => 2
[patent_no_of_words] => 753
[patent_no_of_claims] => 14
[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] => 13600343
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/600343 | CONTROLS FOR AIRCRAFT E-TAXI | Aug 30, 2012 | Abandoned |
Array
(
[id] => 8741614
[patent_doc_number] => 20130081330
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-04-04
[patent_title] => 'AIRCRAFT INTERIOR DOOR ASSEMBLY'
[patent_app_type] => utility
[patent_app_number] => 13/588083
[patent_app_country] => US
[patent_app_date] => 2012-08-17
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 8
[patent_figures_cnt] => 8
[patent_no_of_words] => 3733
[patent_no_of_claims] => 18
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[patent_current_assignee] =>[type] => publication
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13588083
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/588083 | AIRCRAFT INTERIOR DOOR ASSEMBLY | Aug 16, 2012 | Abandoned |
Array
(
[id] => 9880782
[patent_doc_number] => 08967535
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-03-03
[patent_title] => 'Aircraft landing gear'
[patent_app_type] => utility
[patent_app_number] => 13/544674
[patent_app_country] => US
[patent_app_date] => 2012-07-09
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 5
[patent_figures_cnt] => 5
[patent_no_of_words] => 2411
[patent_no_of_claims] => 15
[patent_no_of_ind_claims] => 2
[patent_words_short_claim] => 132
[patent_maintenance] => 1
[patent_no_of_assignments] => 0
[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13544674
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/544674 | Aircraft landing gear | Jul 8, 2012 | Issued |
Array
(
[id] => 10891864
[patent_doc_number] => 08915469
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2014-12-23
[patent_title] => 'System for draining water condensation in an aircraft'
[patent_app_type] => utility
[patent_app_number] => 13/543379
[patent_app_country] => US
[patent_app_date] => 2012-07-06
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 1
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[patent_no_of_words] => 5585
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[patent_current_assignee] =>[type] => patent
[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13543379
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/543379 | System for draining water condensation in an aircraft | Jul 5, 2012 | Issued |
Array
(
[id] => 9209319
[patent_doc_number] => 20140008496
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2014-01-09
[patent_title] => 'USING HANDHELD DEVICE TO CONTROL FLYING OBJECT'
[patent_app_type] => utility
[patent_app_number] => 13/541766
[patent_app_country] => US
[patent_app_date] => 2012-07-05
[patent_effective_date] => 0000-00-00
[patent_drawing_sheets_cnt] => 7
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13541766
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/541766 | USING HANDHELD DEVICE TO CONTROL FLYING OBJECT | Jul 4, 2012 | Abandoned |
Array
(
[id] => 10183202
[patent_doc_number] => 09212877
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-12-15
[patent_title] => 'Retention system for a deployable projectile fin'
[patent_app_type] => utility
[patent_app_number] => 13/542041
[patent_app_country] => US
[patent_app_date] => 2012-07-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13542041
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/542041 | Retention system for a deployable projectile fin | Jul 4, 2012 | Issued |
Array
(
[id] => 8973467
[patent_doc_number] => 20130206897
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-08-15
[patent_title] => 'VERY LOW-POWER ACTUATION DEVICES'
[patent_app_type] => utility
[patent_app_number] => 13/542635
[patent_app_country] => US
[patent_app_date] => 2012-07-05
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13542635
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/542635 | Very low-power actuation devices | Jul 4, 2012 | Issued |
Array
(
[id] => 8825634
[patent_doc_number] => 20130126678
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-05-23
[patent_title] => 'SPACE VEHICLE RENDEZVOUS'
[patent_app_type] => utility
[patent_app_number] => 13/534761
[patent_app_country] => US
[patent_app_date] => 2012-06-27
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13534761
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/534761 | SPACE VEHICLE RENDEZVOUS | Jun 26, 2012 | Abandoned |
Array
(
[id] => 9963076
[patent_doc_number] => 09010679
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-04-21
[patent_title] => 'Hybrid spherical and thrust bearing'
[patent_app_type] => utility
[patent_app_number] => 13/532910
[patent_app_country] => US
[patent_app_date] => 2012-06-26
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/532910 | Hybrid spherical and thrust bearing | Jun 25, 2012 | Issued |
Array
(
[id] => 8863015
[patent_doc_number] => 20130146718
[patent_country] => US
[patent_kind] => A1
[patent_issue_date] => 2013-06-13
[patent_title] => 'ELEVON CONTROL SYSTEM'
[patent_app_type] => utility
[patent_app_number] => 13/524937
[patent_app_country] => US
[patent_app_date] => 2012-06-15
[patent_effective_date] => 0000-00-00
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[pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13524937
[rel_patent_id] =>[rel_patent_doc_number] =>) 13/524937 | Elevon control system | Jun 14, 2012 | Issued |
Array
(
[id] => 10156262
[patent_doc_number] => 09188025
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-11-17
[patent_title] => 'Apparatus for facilitating access to a nacelle interior'
[patent_app_type] => utility
[patent_app_number] => 13/524036
[patent_app_country] => US
[patent_app_date] => 2012-06-15
[patent_effective_date] => 0000-00-00
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/524036 | Apparatus for facilitating access to a nacelle interior | Jun 14, 2012 | Issued |
Array
(
[id] => 10156263
[patent_doc_number] => 09188026
[patent_country] => US
[patent_kind] => B2
[patent_issue_date] => 2015-11-17
[patent_title] => 'Apparatus for facilitating access to a nacelle interior and method of assembling the same'
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[patent_app_number] => 13/524127
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/524127 | Apparatus for facilitating access to a nacelle interior and method of assembling the same | Jun 14, 2012 | Issued |
Array
(
[id] => 10874734
[patent_doc_number] => 08899515
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[patent_issue_date] => 2014-12-02
[patent_title] => 'Folding configuration for air vehicle'
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[patent_app_number] => 13/475371
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[rel_patent_id] =>[rel_patent_doc_number] =>) 13/475371 | Folding configuration for air vehicle | May 17, 2012 | Issued |