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Miniature Modular Rack Launcher Combo Senior Design Group 3 Casey Brown Cyril John Keith Kirkpatrick Bryan Rickards.

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Presentation on theme: "Miniature Modular Rack Launcher Combo Senior Design Group 3 Casey Brown Cyril John Keith Kirkpatrick Bryan Rickards."— Presentation transcript:

1 Miniature Modular Rack Launcher Combo Senior Design Group 3 Casey Brown Cyril John Keith Kirkpatrick Bryan Rickards

2 Overview Problem Statement Product Specifications Final Design Project Status Parts Received Potential Issues Testing Gantt Chart 1

3 Problem Statement Design and develop a Bomb Rack Unit (BRU) that is attached to the Tigershark UAV capable of housing and launching a cylindrical payload. BRU must contain an electrical box which will allow space for an electrical team to design and integrate an electrical interface to control in-flight operation of the BRU. Provide budget analysis for BRU Design and construction of a prototype 2

4 Tigershark UAV Platform Specifications: Wing span 21 feet Propulsion - 372cc two stroke 20 gallon fuel tank Empty airframe weight - 150 lbs. Gross take off weight - 300 lbs. Payload capacity – 50 lbs. One hard-point location per wing for launcher attachment 3

5 Constraints BRU must not exceed 5 lbs. Capable of holding a payload that is 10lbs Operation in temperature range -20 to 60 degrees C and during rain exposure Retain payload during aircraft maneuvers up to 2GS lateral load and 1G landing shock. 4

6 Final Design 5

7 6

8 7 Input RegulatorStorage TankExhaust Valve Solenoid Valve Piston

9 8 Final Design Ejector PistonLimit Switch Roller Bearing Slider Block Lanyard Attachment

10 9 Final Design

11 10 Final Design Safety Block Engaged

12 11 Final Design Safety Block Disengaged

13 Project Status All parts have been received Raw materials are currently being machined (31 parts) – Hook Assembly – Brackets – Delrin Spacers – Bearing and Slide Assembly As machined parts are completed assembly will begin Purchase Items PartVenderPart NumberPriceQuantityTotal Price Air CylinderMcMaster6498K211$33.421 Air TankClippardAVT-24-4$16.821 Check ValveMcMaster3208K22$14.741 RegulatorMcMaster99045K48$34.801 SolenoidcylvalSA31NC$40.801 Exhaust ValveMcMaster4149T41$35.551 Guide_rollerGrainger1ZGT7$48.254$193.00 Ejector_bushingMcMaster6377K114$20.272$40.54 Ejector_springGrainger1NCT2$7.691 PushspringMcMaster9657K48$6.291 ServoFutabaFUTM0513$1251$124.98 Limit SwitchMcMaster7090K37$7.911 RBF PINMcMaster90293A139$17.981 6-32 lock nutGrainger3HDT6$2.831 6-32x 1/2 screwGrainger1MU14$2.291 6-32x 1 1/2 screwMcMaster91251A157$6.981 Leveling FootMcMaster2531k61$7.304$29.20 air connectoromega OM-AIR- C24250418- 5PK$5.502$11.00 air hoseomega TYUTH95- 1418-50-TRBL$21.001 female connectoromega OM-AIR- C24260418- 5PK$11.501 90deg elbowomega OM-AIR- C24470418- 5PK$8.251 Raw Materialonlinemetals $102.54 Total $770.11 12

14 Parts Received Pneumatic System Servo Motor Roller Bearing Sway Brace 13

15 Potential Issues Proper machining BRU overweight Pneumatic system failure – Hook Release – Ejector Safety System – Servo Motor Time constraint Material Weight AssemblyTotal Hook Eject1.0191 Mech Safety0.0944 Ejector0.1606 Pylon Attach0.0574 BRU Casing0.9515 Push Spring0.0156 Pneumatic System0.4213 Sway Brace0.8803 Other1.2808 Total4.881 14

16 Testing Currently testing Pneumatic System/Servomotor Once assembled – Proper integration – Ejection Velocity – Load – Safety Systems 15

17 16

18 Questions ???? 17


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