Award search
Awards for “boeing”
25 awards on this page · sorted by amount · page 327
| Award ID | Recipient | Awarding agency | Amount | Start | End | NAICS | Description |
|---|---|---|---|---|---|---|---|
| TYAH | BELL BOEING JOINT PROJECT OFFICE | Department of Defense | $1.01M | 2015-03-26 | 2016-06-23 | 336411 | 8501942991!PIN ASSEMBLY,SHEAR, |
| 5395 | BELL BOEING JOINT PROJECT OFFICE | Department of Defense | $1.01M | 2010-08-30 | 2012-03-12 | 336413 | NAVAL AVIATION |
| FA820718F0015 | THE BOEING COMPANY | Department of Defense | $1.01M | 2018-06-26 | 2022-09-19 | 541330 | PURCHASE RADIOGRAPHIC X-RAY MACHINE |
| 0010 | ARGON ST, INC. | Department of Defense | $1.01M | 2017-04-10 | 2018-04-19 | 541330 | 6 CHANNEL D/A VME CCA IGE::CL::IGE |
| NNL12AA55P | THE BOEING COMPANY | National Aeronautics and Space Administration | $1.01M | 2011-12-12 | 2015-09-30 | 541511 | FLIGHT TRAINING SIMULATOR DATA LICENSE AND BOEING 737-800W SIMULATION DATA PACKAGE |
| 0002 | BOEING DISTRIBUTION SERVICES, INC. | Department of Defense | $1.01M | 2017-07-28 | 2018-06-30 | 332722 | HARDWARE - VENDOR MANAGED INVENTORY AMB. |
| NNA16BD84C | THE BOEING COMPANY | National Aeronautics and Space Administration | $1.01M | 2016-08-17 | 2018-03-17 | 541712 | IGF::OT::IGF NRA SUBTOPIC 2.4, SASO1 "REVOLUTIONARY AND ADVANCED UNIVERSAL, RELIABLE, ALWAYS AVAILABLE, CYBER SECURE AND AFFORDABLE COMMUNICATION, NAVIGATION, SURVEILLANCE (CNS) OPTIONS FOR ALL ALTITUDES OF UAS OPERATIONS." THE SCOPE OF THE THIS WORK IS TO IDENTIFY REVOLUTIONARY AND ADVANCED INTEGRATED CNS SYSTEMS AND TECHNOLOGY OPTIONS THAT CAN SUPPORT UAS OPERATING AT ALL ALTITUDES AND IN ALL AIRSPACE. THE SYSTEM IS REQUIRED TO INCLUDE AIR-AIR AND AIR-GROUND CAPABILITIES. THESE CNS ALTERNATIVES MUST BE RELIABLE, REDUNDANT, ALWAYS AVAILABLE, CYBER-SECURE, AND AFFORDABLE FOR ALL TYPES OF VEHICLES INCLUDING SMALL UAS TO LARGE TRANSPORT CATEGORY AIRCRAFT. THE VEHICLES MUST BE TRACKED, AND IN COMMUNICATION, ALL THE WAY TO THE DOOR-STEP OR TO ANY ALTITUDE, ANYWHERE IN THE WORLD, BE ABLE TO SENSE OBSTACLES AT ALL ALTITUDES AND ACCURATELY NAVIGATE IN THE ABSENCE OF NAVIGATIONAL AIDS. |
| DTFAWA10D00019CALL0001 | BOEING AEROSPACE OPERATIONS, INC. | Department of Transportation | $1.01M | 2010-05-26 | 2012-01-31 | 541330 | THIS TASK ORDER IS FOR PROGRAM MANAGEMENT AND TECHNICAL SUPPORT FOR THE SE-2020 PROGRAM. TAS::69 1301::TAS |
| N0001918F2447 | THE BOEING COMPANY | Department of Defense | $1.01M | 2018-02-06 | 2019-02-06 | 541512 | FLEET SUPPORT SERVICES |
| N0001417C2009 | THE BOEING COMPANY | Department of Defense | $1.01M | 2016-11-07 | 2019-11-09 | 541712 | IGF::CL::IGF ROBUST ROUTING IN DYNAMIC NETWORKS (R2DN) |
| Z544 | THE BOEING COMPANY | Department of Defense | $1.01M | 2009-04-10 | 2013-04-10 | 541330 | TOUCH LABOR |
| N0001921F0326 | THE BOEING COMPANY | Department of Defense | $1.01M | 2021-05-12 | 2023-04-28 | 336412 | NAVSUP EMBEDDED GPS RECEIVERS (EGR) FFP |
| 0046 | THE BOEING COMPANY | Department of Defense | $1.01M | 2006-09-08 | 2010-09-30 | 336411 | 200612!000039!5700!FA8628!ASC/YDK !F3365701D2050 !A!N! !N!0046 ! !20060908!20070604!076200344!076200344!009256819!N!MCDONNELL DOUGLAS CORPORATION !2401 E WARDLOW ROAD !LONG BEACH !CA!90807!43000!037!06!LONG BEACH !LOS ANGELES !CALIFORNIA!+000001027798!N!N!000000000000!1510!AIRCRAFT FIXED WING !A1A!AIRFRAMES AND SPARES !000 !NOT DISCERNABLE !336411!E! !5!B!S! ! ! !99990909!B! ! !N!Z!D!N!J!1!001!N!1A!A!Y!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!C!N! ! ! !Y! ! !0001! ! |
| 70RSAT20C00000003 | THE BOEING COMPANY | Department of Homeland Security | $1.01M | 2020-03-04 | 2024-03-08 | 541715 | NEW CONTRACT $809,781.15 FOR BLAST EFFECTS ANALYSIS TOOLS DEVELOPMENT FOR COMMERCIAL COMPOSITE AIRCRAFT |
| 697DCK22F01593 | JEPPESEN FOREFLIGHT, INC. | Department of Transportation | $1.01M | 2022-08-10 | 2023-09-25 | 511210 | FUNDING DTFACT-16-D-00010 BOEING (JEPPESEN SUBSCRIPTIONS) ORDERING YEAR 2 POP: 9-26-2022 THRU 9-25-2023. ASSIGNED CO: RICHARD PALSGROVE |
| 7012 | THE BOEING COMPANY | Department of Defense | $1M | 2007-04-19 | 2011-07-01 | 336411 | NAVAL AVIATION |
| NNL11AC32T | THE BOEING COMPANY | National Aeronautics and Space Administration | $1M | 2011-09-21 | 2015-02-27 | 541712 | THE BOEING TEAM PROPOSES A NOVEL VARIABLE GEOMETRY WINGTIP CONTROL EFFECTOR AIMED SPECIFICALLY AT VERY HIGH ASPECT RATIO/LOW SWEEP TRUSS BRACED WINGS (TBW). TWO BOEING N+3 SUBSONIC ULTRA GREEN AIRCRAFT RESEARCH (SUGAR) CONFIGURATIONS TAKE ADVANTAGE OF TBW'S. AT CRUISE FLIGHT CONDITIONS THE TBW MAY BE SUBJECT TO DESIGN REQUIREMENTS THAT DISTINGUISH THEM FROM MORE HIGHLY SWEPT WINGS. HIGH ASPECT RATIO, SHORT CHORD LENGTH AND RELATIVE THINNESS OF THE AIRFOIL SECTIONS ALL CONTRIBUTE TO RELATIVELY LOW WING TORSIONAL STIFFNESS. THIS MAY LEAD TO AEROELASTIC ISSUES SUCH AS AILERON REVERSAL AND LOW FLUTTER MARGINS. FURTHER, THE GEOMETRY OF A SWEPT WING NATURALLY PROVIDES STRONG STABILIZING AERODYNAMIC FORCES DUE TO WING BENDING DEFORMATION UNDER LOADS. LACKING THIS AERODYNAMIC STIFFENING, LOW SWEEP WINGS MAY EXHIBIT REDUCED DIVERGENCE MARGINS. IN ORDER TO COUNTERACT THESE ISSUES, HIGH ASPECT RATIO/LOW SWEEP WINGS MAY NEED TO CARRY ADDITIONAL STRUCTURAL WEIGHT TO PROVIDE HIGH TORSIONAL STIFFNESS. ONE VERY ATTRACTIVE OPTION TO PROVIDE ROLL CONTROL IS TO INTENTIONALLY CREATE WING TWIST. THE NASA X-53 ACTIVE AEROELASTIC WING (AAW) AIRCRAFT DEMONSTRATED THIS CONCEPT IN FLIGHT TESTING. BOEING WAS LEAD CONTRACTOR ON X-53 SO WE FULLY UNDERSTAND THAT THE PRIMARY ADVANTAGE OF AAW IS THAT ADDITIONAL STRUCTURAL WEIGHT IS NOT REQUIRED TO PROVIDE HIGH TORSIONAL STIFFNESS, IN FACT THE ADDITIONAL WEIGHT IS DETRIMENTAL TO THE AAW APPROACH. HOWEVER, ROLL CONTROL BY AAW WORKS BEST IN A FAIRLY NARROW RANGE OF DYNAMIC PRESSURE WHEN FORCES GENERATED BY THE CONTROL SURFACE ACT THROUGH A MOMENT ARM TO OVERCOME THE TWIST STIFFNESS OF THE WING. AT LOWER DYNAMIC PRESSURE, THE TWIST LOADS ARE NOT SUFFICIENT TO GENERATE ENOUGH TWIST AND AT THE AILERON REVERSAL SPEED, THE AILERONS PROVIDE NO ROLL CONTROL AT ALL. THE PROPOSED NOVEL CONTROL EFFECTOR IS A VARIABLE SWEEP RAKED WING TIP. AT HIGH SPEED THE WINGTIP IS IN THE RAKED (SWEPT BACK) POSITION PROVIDING DUAL, INDEPENDENT BENEFITS. THE DRAG REDUCTION BENEFIT OF A RAKED WINGTIP IS ACHIEVED, AND IN ADDITION THE CONTROL EFFECTOR(S) ARE MOVED WELL AFT OF THE WING TORSIONAL AXIS. THIS PROVIDES A MOMENT ARM FOR FORCES GENERATED BY THE CONTROL EFFECTOR TO APPLY WING TWIST AND ENABLE THE AAW EFFECT. AT LOW SPEED THE WINGTIP IS UNSWEPT. THIS MOVES THE AERODYNAMIC CENTER OF THE CONTROL SURFACE LOADS FORWARD TO LIE ON OR VERY NEAR THE WING TORSIONAL AXIS. THIS ALLOWS THE CONTROL SURFACE TO ACT VERY EFFECTIVELY AS A CONVENTIONAL AILERON BY PROVIDING ROLL CONTROL FORCES WHILE APPLYING MINIMAL TWIST LOADS TO THE WING. A KEY ASPECT OF OUR CONCEPT IS THAT HIGH RATES NECESSARY FOR ROLL CONTROL CAN BE PROVIDED BY A HIGH RATE CONTROL EFFECTOR SUCH AS LEADING OR TRAILING EDGE FLAPS, CONFORMAL CAMBER CHANGE OF THE WINGTIP, AND/OR TWIST OF THE WINGTIP ITSELF. THE LARGE SCALE VARIABLE GEOMETRY (SWEEP) WILL CHANGE WITH FLIGHT CONDITION AND NEED MUCH LOWER RATE. VARIABLE GEOMETRY WILL LIKELY INCLUDE SWEEP CHANGE, BUT OTHER SHAPE CHANGES SUCH AS WINGTIP DIHEDRAL (WINGLETS) AND TWIST WILL ALSO BE INVESTIGATED. BOEING HAS CAREFULLY SELECTED A SMALL, AGILE TEAM THAT INCLUDES VIRGINIA TECH FOR THEIR EXPERIENCE WITH TBW AIRCRAFT, AND NEXTGEN AERONAUTICS FOR THEIR EXPERIENCE WITH DEVELOPMENT OF MORPHING AIRCRAFT CONCEPTS. BOTH ARE TEAM MEMBERS ON THE BOEING SUGAR PHASE II PROGRAM. THIS PROGRAM WILL DRAW DIRECTLY ON THE DESIGNS AND DATA GENERATED IN SUGAR PHASES I AND II. EACH OF THE THREE TEAM MEMBERS WILL DEVELOP A CONCEPT FOR VARIABLE GEOMETRY RAKED WINGTIPS BASED ON THEIR UNIQUE EXPERIENCE. ONE OF THESE CONCEPTS WILL BE SELECTED FOR A DETAILED PERFORMANCE INVESTIGATION INCLUDING EXTENSIVE EVALUATION OF AEROELASTIC RESPONSE. ADDITIONAL BENEFITS WILL BE CONSIDERED SUCH AS ACTIVE GUST LOAD ALLEVIATION, RIDE QUALITY IMPROVEMENT AND ACTIVE BUFFET ALLEVIATION. BOEING IS EXCITED ABOUT THE BENEFITS OF THIS SYNERGISTIC APPLICATION OF AAW AND ADAPTIVE STRUCTURES/MORPHING TECHNOLOGY TO BENEFIT HIGH SPAN LOW WING SWEEP CONFIGURATIONS. |
| SPE4A520F2755 | THE BOEING COMPANY | Department of Defense | $1M | 2019-11-08 | 2023-01-31 | 336413 | 8506929239!PIN ASSEMBLY, TIE BAR (HEAD A |
| 0003 | THE BOEING COMPANY | Department of Defense | $1M | 2005-03-09 | 2011-03-18 | 336413 | 200506!000749!5700!FA8103!OC-ALC/LID !FA810304D0119 !A!N! !N!0003 ! !20050309!20050729!076200344!076200344!009256819!N!MCDONNELL DOUGLAS CORPORATION !2401 E WARDLOW ROAD !LONG BEACH !CA!90807!43000!037!06!LONG BEACH !LOS ANGELES !CALIFORNIA!+000001004292!N!N!000000000000!1650!ACFT HYDRAULIC, VACUUM & DE-ICING SYS COMP !A1C!OTHER AIRCRAFT EQUIPMENT !000 !* !336413!E! !5!A!S! ! ! !20200930!B! ! !N!Z!A!N!J!2!002!B! !A!N!Z! ! !N!C!N! ! ! !A!A!A!A!000!A!B!N! ! ! ! ! ! !0001! ! |
| 0009 | THE BOEING COMPANY | Department of Defense | $1M | 2015-09-25 | 2017-12-25 | 336413 | IGF::OT::IGF ENGINEERING SERVICES FOR FUEL TANK ACCESS DOOR SEAL REPLACEMENT DEVELOPMENT |
| SC07 | BOEING AEROSPACE OPERATIONS, INC. | Department of Defense | $1M | 2007-01-01 | 2008-06-30 | 541330 | ACC F-22 CETS |
| 0011 | THE BOEING COMPANY | Department of Defense | $1M | 2014-12-15 | 2016-01-31 | 336411 | KUWAIT ISS SUPPORT |
| Z5DW | THE BOEING COMPANY | Department of Defense | $1M | 2016-06-22 | 2021-08-31 | 336411 | F/A-18 A-D AND E/F MODIFICATIONS |
| NND11AQ73C | THE BOEING COMPANY | National Aeronautics and Space Administration | $1M | 2011-09-23 | 2013-04-01 | 541712 | UAS INTO THE NATIONAL AIRSPACE SYSTEM |
| 2001 | THE BOEING COMPANY | Department of Defense | $1M | 2007-05-22 | 2007-11-30 | 336411 | SLAM-ER (USN/FMS) |