Voting Results

Votes: 105
Voting Result: 2.08557055336953

Overview for DroneX

Hello, this is my design for Airbus Cargo Drone Challenge. DroneX was designed with efficiency in mind. My major concern is the fact, that having big wings while the craft is hovering will make it very sensible to the smallest winds. One of the requisites is hover 5 min, with winds up to 10m/s. For that, some simple form to reduce the wing surface is needed. After dealing with different concepts to reduce the wing surface, I concluded that a retractable wings are needed. A simple design combining a telescopic spar (pneumatically actuated) with ribs, and flexible skin (parachute fabric), is enought light and resistant to do the job. - DroneX can travel 100km with 5kg cargo. - Designed with FLZ_Vortex and XFLR5 1. “Keep it super simple”: a) Quad configuration: Most simple configuration, less elements, less prone to failure, less weight, extensively tested. b) Flying wing configuration: One body, one wing, and four tail elements.  Minimal elements with simple and symetrical shapes. c) Tail sitter configuration: No transition flight mecanisms requiered. Less  weight, less prone to failure, less elements to program and control. d) Shared function elements:  i. Forward flight propulsion is achieved with the same motors/propellers  used in multicopter mode. In aircraft mode the inferior motors are stopped, and propellers retracted. ii. Inferior tail landing gear are used for land and takeoff in multicopter  mode and aircraft mode. e) Low parts count: The main body structure and skin are built with less  than 15 parts. 2. Keep in mind: An optimized design contains the following: a) Ease of maintenance:  i. All parts are easily accesible removing the superior and inferior skin parts (less than 20 screws) ii. Ease of acces: The internal space is big, all internal parts are easy to  acces and well spaced. No problem for those technicians with big hands. iii. Elements with most decay are packed in the external nacelles. These  nacelles are atatched to main body throught two screws, So replacing  motor, ESC, battery, or propeller is as easy as swaping the nacelle with  failure or TBO exahusted for one new, and send the old to overhaul. b) 20 minutes turnaround between max-distance missions: less than 15 min i. Land, propellers stopped, disarmed: <10s ii. Aproximation to the Drone X with 4 fresh charged nacelles, and new  cargo (15kg max): 60s iii. Visual inspection: 240s iv. Proceed to unload the arrived cargo (push demagnetitzation button  while holding the cargo): 60s v. Proceed to load the new cargo (Hold the cargo in their place and push  magnetitzation button): 60s vi. Remove the screw protection of nacelle 0 and remove the two screws  that attatch him to tail 0. Swap the exhausted nacelle with a fresh one, plug in in their position and tighten the screws. Finally put the screws protection again: 90s vii. Remove the screw protection of nacelle 1 and remove the two screws  that attatch him to tail 1. Swap the exhausted nacelle with a fresh one, plug in in their position and tighten the screws. Finally put the screws protection again: 90s viii. Remove the screw protection of nacelle 2 and remove the two screws that attatch him to tail 2. Swap the exhausted nacelle with a fresh one, plug in in their position and tighten the screws. Finally put the screws protection again: 90s ix. Remove the screw protection of nacelle 3 and remove the two screws  that attatch him to tail 3. Swap the exhausted nacelle with a fresh one, plug in in their position and tighten the screws. Finally put the screws protection again: 90s x. Preflight check: 60s xi. Arm, propellers start spinning, takeoff: <15s c) Swappable batteries: The batteries are included in the external nacelles. d) Consider the following conditions: i. -30 to 50: Yes (Electronics included in the ignition kit must be capable of  sustain these conditions). ii. Moderate rain: Yes (The skin makes contact with the structure and vapour seals, creating watertight zones to all neded parts. The cargo is watertight  too). e) Safe operation in all flight states: 3. Human factors and safety provisions: a) Transportable by two average size pople: It can be transported by one  person as a backpack of 25kg. b) Limit time on ground with rotors spinning: Automatic takeoff and landig will be programed to stay the minimal time in the ground with the propellers spining.  i. Takeoff: <15s ii. Landing: <10s c) Modular design for ease of transport: i. Modular wings (easily atatched with 4 screws for half wing). There will be two versions attatchable. Conventional wings, and retractable wings. ii. Modular nacelles (easily atached with 2 screws for each one) d) The aircraft shall be able to be disassembled and transportable.  Consider different scenarios of shipping to perhaps even remote places     ( van, vessel, aircraft, truck, ISO container etc.). i. Van: Capable ii. Vessel: Capable iii. Aircraft: Capable iv. Truck: Capable v. ISO container: Capable 4. Design guideline for your design: i. May consider a disc loading between 10 kg/m^2 and 50 kg/m^2: Disc  loading of 25 kg/m^2. ii. May consider a wing loading between 10 kg/m^2 and 30 kg/m^2: Wing  loading of 10 kg/m^2. 5. Mitigate consequences of failure: i. Flight termination parachute system included. ii. Redundant battery system. 6. May consider a landing gear for conventional fixed-wing take-off and landing: This is a working progress. Space and weight reserved for it.  7. Ease of handling: The stability factor is >10% at cruise speed (80km/h). The stall point is 45km/h. 8. Components: 4x Motors: KDE7215XF-135 (565g)  2260g 4x ESC: KDEXF-UAS95HVC (86g) 344g 4x Battery: 16s3p Samsung INR 18650-35E 3500mah (2256g) 9024g 4x Electromagnetic cargo holding: OpenGrab EPM V3 (40g) 160g 24x Propeller Blade: Aeronaut CAM-CARB 18.5x15 (12g) 288g 1x Pneumatic System: Custom brushless radial turbine, with valve system for deliver pressure/vaccumm (inflate/deflate telescopic main spar and other actuators) 350g 1x Structure: Custom made structure with lasercut plates of CF-Nomex, and some mechanized aluminium parts. 1x Skin top: Vacuum formed 1x Skin bottom: Vacuum formed 2x Ventral cargo doors: Vacuum formed 2x Tail doors: Vacuum formed 2x Flight termination system doors: Vacuum formed 4x Tail nacelles: Vacum formed skin / CF tube and plates structure
Entry file list for DroneX

Results for DroneX

Voter Score
nkatsirou 5.0
Tana 5.0
gdshreedu141 5.0
kyriakicharalambous 5.0
noeliaytal 5.0
Team_82zero24 4.0
echatzigeo 4.0
viktorvildovic 4.0
crodrf01 4.0
Barbaros 4.0
silviomaccarrone1974 4.0
maximelafeuille 4.0
AdrienK 3.0
pedroouton 3.0
GPD 3.0
setiawan 3.0
prishtina 3.0
eddie_mauro 3.0
ACDesign 3.0
Phil_Airbus 3.0
VTOL 3.0
christoph 3.0
paulfaugeras 3.0
lucashernanlopez81 3.0
Alexis_K 3.0
jeademange 3.0
mkBoom 3.0
joernlutter 3.0
fesan3 3.0
gabriel_r 3.0
phill_scott 3.0
Cristian_F 3.0
CharlieFournier 2.0
vanessamariaramirez 2.0
MarkWatney 2.0
alexiel 2.0
Ramarryo 2.0
migl187 2.0
albertbuzafdz 2.0
amarkler 2.0
lulu 2.0
DavidCavaDesign 2.0
savtek 2.0
Pivotwing 2.0
jjsanchezrico 2.0
oemlegoem 2.0
evansmazarakos 2.0
fabiocastillione 2.0
jrsalter1 2.0
PeterKutz 2.0
TechFish 2.0
PhilS 2.0
steve4oven 2.0
mblair 2.0
michele.cantatore 2.0
DesignerMec 2.0
arre1954 2.0
warmonger 2.0
Andika 2.0
artapakidna 2.0
fernadinhoalvarodiaz 2.0
arthurmenezesmurcia 2.0
_alex 2.0
onter1965 2.0
Davded 2.0
tram 2.0
DesignMechanix 2.0
samuellevy 2.0
luismontenegroferrel 2.0
jhoholis 2.0
harvestzhang 2.0
Bialas 2.0
zamri 2.0
GeorgeP 2.0
stefanofortunati 2.0
iamyourman 2.0
vpastrikakis 1.0
vgc90 1.0
Franze 1.0
aeronaut4195 1.0
jimyjackal 1.0
angelicamary18 1.0
Falk90 1.0
engand42 1.0
kaltrina 1.0
francosalza 1.0
david5f18j90 1.0
nesman 1.0
gmech 1.0
pablofigueroamariavfaya 1.0
vasilatos_ianis 1.0
konelek 1.0
Mekiso 1.0
Lude 1.0
ypervoreios 1.0
karakalakis 1.0
LameContest 1.0
depi91 1.0
adw.wong 1.0
apalmer 1.0
ralonso 1.0
seeck1942 1.0
minvertedm 1.0
sonsoleslopezdebustos 1.0