Search

Michael B. Kreiner

Examiner (ID: 12122, Phone: (571)270-5379 , Office: P/3644 )

Most Active Art Unit
3644
Art Unit(s)
3644, 3642, 4174
Total Applications
934
Issued Applications
777
Pending Applications
65
Abandoned Applications
125

Applications

Application numberTitle of the applicationFiling DateStatus
Array ( [id] => 10083245 [patent_doc_number] => 09120583 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-09-01 [patent_title] => 'Space solar array architecture for ultra-high power applications' [patent_app_type] => utility [patent_app_number] => 13/447166 [patent_app_country] => US [patent_app_date] => 2012-04-14 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 12 [patent_figures_cnt] => 12 [patent_no_of_words] => 11120 [patent_no_of_claims] => 2 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13447166 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/447166
Space solar array architecture for ultra-high power applications Apr 13, 2012 Issued
Array ( [id] => 9078885 [patent_doc_number] => 20130264415 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-10-10 [patent_title] => 'TRANSVERSE FLUX MACHINE UTILIZED AS PART OF A COMBINED LANDING GEAR SYSTEM' [patent_app_type] => utility [patent_app_number] => 13/442905 [patent_app_country] => US [patent_app_date] => 2012-04-10 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 3 [patent_figures_cnt] => 3 [patent_no_of_words] => 1752 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13442905 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/442905
Transverse flux machine utilized as part of a combined landing gear system Apr 9, 2012 Issued
Array ( [id] => 8563400 [patent_doc_number] => 20120325971 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-12-27 [patent_title] => 'Space vacuum propulsion system' [patent_app_type] => utility [patent_app_number] => 13/506619 [patent_app_country] => US [patent_app_date] => 2012-04-06 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 38 [patent_figures_cnt] => 38 [patent_no_of_words] => 2351 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 11 [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] => 13506619 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/506619
Space vacuum propulsion system Apr 5, 2012 Abandoned
Array ( [id] => 9830597 [patent_doc_number] => 08939404 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-01-27 [patent_title] => 'Pressure fuselage of an aircraft with dome-shaped pressure bulkhead' [patent_app_type] => utility [patent_app_number] => 13/440133 [patent_app_country] => US [patent_app_date] => 2012-04-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 3138 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 314 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13440133 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/440133
Pressure fuselage of an aircraft with dome-shaped pressure bulkhead Apr 4, 2012 Issued
Array ( [id] => 9942476 [patent_doc_number] => 08991765 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-31 [patent_title] => 'Satellite predictive avoidance system' [patent_app_type] => utility [patent_app_number] => 13/438176 [patent_app_country] => US [patent_app_date] => 2012-04-03 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 15 [patent_figures_cnt] => 19 [patent_no_of_words] => 11996 [patent_no_of_claims] => 25 [patent_no_of_ind_claims] => 4 [patent_words_short_claim] => 270 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13438176 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/438176
Satellite predictive avoidance system Apr 2, 2012 Issued
Array ( [id] => 9826997 [patent_doc_number] => 08936219 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-01-20 [patent_title] => 'Performance-enhancing winglet system and method' [patent_app_type] => utility [patent_app_number] => 13/436355 [patent_app_country] => US [patent_app_date] => 2012-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 16 [patent_no_of_words] => 9066 [patent_no_of_claims] => 18 [patent_no_of_ind_claims] => 3 [patent_words_short_claim] => 129 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13436355 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/436355
Performance-enhancing winglet system and method Mar 29, 2012 Issued
Array ( [id] => 9314358 [patent_doc_number] => 08655589 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-02-18 [patent_title] => 'System and method for controlling motion of spacecrafts' [patent_app_type] => utility [patent_app_number] => 13/435641 [patent_app_country] => US [patent_app_date] => 2012-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 5922 [patent_no_of_claims] => 11 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 237 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13435641 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/435641
System and method for controlling motion of spacecrafts Mar 29, 2012 Issued
Array ( [id] => 10175719 [patent_doc_number] => 09205908 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2015-12-08 [patent_title] => 'Locking mechanism for use in a decompression arrangement' [patent_app_type] => utility [patent_app_number] => 13/435013 [patent_app_country] => US [patent_app_date] => 2012-03-30 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 2 [patent_figures_cnt] => 3 [patent_no_of_words] => 4317 [patent_no_of_claims] => 10 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 196 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13435013 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/435013
Locking mechanism for use in a decompression arrangement Mar 29, 2012 Issued
Array ( [id] => 8486683 [patent_doc_number] => 20120286090 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-11-15 [patent_title] => 'CONNECTION OF A FUSELAGE TO AN AIRCRAFT WING' [patent_app_type] => utility [patent_app_number] => 13/428291 [patent_app_country] => US [patent_app_date] => 2012-03-23 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 4 [patent_no_of_words] => 1204 [patent_no_of_claims] => 8 [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] => 13428291 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/428291
Connection of a fuselage to an aircraft wing Mar 22, 2012 Issued
Array ( [id] => 8344565 [patent_doc_number] => 20120205489 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2012-08-16 [patent_title] => 'INITIATING FLIGHT OF A FLYING STRUCTURE' [patent_app_type] => utility [patent_app_number] => 13/426670 [patent_app_country] => US [patent_app_date] => 2012-03-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 20 [patent_figures_cnt] => 20 [patent_no_of_words] => 11091 [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] => 13426670 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/426670
INITIATING FLIGHT OF A FLYING STRUCTURE Mar 21, 2012 Abandoned
Array ( [id] => 9592179 [patent_doc_number] => 08781741 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-15 [patent_title] => 'Multi-body dynamics method of generating fuel efficient transfer orbits for spacecraft' [patent_app_type] => utility [patent_app_number] => 13/426746 [patent_app_country] => US [patent_app_date] => 2012-03-22 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 9 [patent_no_of_words] => 10205 [patent_no_of_claims] => 9 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 178 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13426746 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/426746
Multi-body dynamics method of generating fuel efficient transfer orbits for spacecraft Mar 21, 2012 Issued
Array ( [id] => 9050937 [patent_doc_number] => 20130248651 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-26 [patent_title] => 'Aircraft Class Divider' [patent_app_type] => utility [patent_app_number] => 13/426451 [patent_app_country] => US [patent_app_date] => 2012-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 10 [patent_figures_cnt] => 10 [patent_no_of_words] => 2259 [patent_no_of_claims] => 12 [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] => 13426451 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/426451
Aircraft class divider Mar 20, 2012 Issued
Array ( [id] => 9050934 [patent_doc_number] => 20130248648 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-26 [patent_title] => 'Portable Control System For Rotary-Wing Aircraft Load Management' [patent_app_type] => utility [patent_app_number] => 13/425546 [patent_app_country] => US [patent_app_date] => 2012-03-21 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 3926 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13425546 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/425546
Portable control system for rotary-wing aircraft load management Mar 20, 2012 Issued
Array ( [id] => 9880775 [patent_doc_number] => 08967529 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-03 [patent_title] => 'Battery-structure' [patent_app_type] => utility [patent_app_number] => 13/422204 [patent_app_country] => US [patent_app_date] => 2012-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 16 [patent_no_of_words] => 3355 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13422204 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/422204
Battery-structure Mar 15, 2012 Issued
Array ( [id] => 9880775 [patent_doc_number] => 08967529 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2015-03-03 [patent_title] => 'Battery-structure' [patent_app_type] => utility [patent_app_number] => 13/422204 [patent_app_country] => US [patent_app_date] => 2012-03-16 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 9 [patent_figures_cnt] => 16 [patent_no_of_words] => 3355 [patent_no_of_claims] => 8 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 186 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13422204 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/422204
Battery-structure Mar 15, 2012 Issued
Array ( [id] => 9031332 [patent_doc_number] => 20130233970 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-09-12 [patent_title] => 'Method and Apparatus for Changing a Deployed Position for a Tail Skid Assembly' [patent_app_type] => utility [patent_app_number] => 13/416914 [patent_app_country] => US [patent_app_date] => 2012-03-09 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 14 [patent_figures_cnt] => 14 [patent_no_of_words] => 7957 [patent_no_of_claims] => 24 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13416914 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/416914
Method and apparatus for changing a deployed position for a tail skid assembly Mar 8, 2012 Issued
Array ( [id] => 9310216 [patent_doc_number] => 08651427 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-02-18 [patent_title] => 'Wing tip device with recess in surface' [patent_app_type] => utility [patent_app_number] => 13/411941 [patent_app_country] => US [patent_app_date] => 2012-03-05 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 7 [patent_figures_cnt] => 17 [patent_no_of_words] => 2787 [patent_no_of_claims] => 16 [patent_no_of_ind_claims] => 2 [patent_words_short_claim] => 69 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13411941 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/411941
Wing tip device with recess in surface Mar 4, 2012 Issued
Array ( [id] => 9272327 [patent_doc_number] => 08636253 [patent_country] => US [patent_kind] => B1 [patent_issue_date] => 2014-01-28 [patent_title] => 'Rollable and accordian foldable refractive concentrator space solar array panel' [patent_app_type] => utility [patent_app_number] => 13/410278 [patent_app_country] => US [patent_app_date] => 2012-03-01 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 17 [patent_figures_cnt] => 19 [patent_no_of_words] => 9550 [patent_no_of_claims] => 6 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 266 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13410278 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/410278
Rollable and accordian foldable refractive concentrator space solar array panel Feb 29, 2012 Issued
Array ( [id] => 9619624 [patent_doc_number] => 08789790 [patent_country] => US [patent_kind] => B2 [patent_issue_date] => 2014-07-29 [patent_title] => 'Aircraft engine attachment pylon' [patent_app_type] => utility [patent_app_number] => 13/408323 [patent_app_country] => US [patent_app_date] => 2012-02-29 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 4 [patent_figures_cnt] => 5 [patent_no_of_words] => 4045 [patent_no_of_claims] => 15 [patent_no_of_ind_claims] => 1 [patent_words_short_claim] => 170 [patent_maintenance] => 1 [patent_no_of_assignments] => 0 [patent_current_assignee] =>[type] => patent [pdf_file] =>[firstpage_image] =>[orig_patent_app_number] => 13408323 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/408323
Aircraft engine attachment pylon Feb 28, 2012 Issued
Array ( [id] => 8973491 [patent_doc_number] => 20130206921 [patent_country] => US [patent_kind] => A1 [patent_issue_date] => 2013-08-15 [patent_title] => 'SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE' [patent_app_type] => utility [patent_app_number] => 13/397569 [patent_app_country] => US [patent_app_date] => 2012-02-15 [patent_effective_date] => 0000-00-00 [patent_drawing_sheets_cnt] => 16 [patent_figures_cnt] => 16 [patent_no_of_words] => 8748 [patent_no_of_claims] => 24 [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] =>[firstpage_image] =>[orig_patent_app_number] => 13397569 [rel_patent_id] =>[rel_patent_doc_number] =>)
13/397569
SYSTEM, APPARATUS AND METHOD FOR LONG ENDURANCE VERTICAL TAKEOFF AND LANDING VEHICLE Feb 14, 2012 Abandoned
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