AeroMorph Presentation (Initial)

8/10/2019 AeroMorph Presentation (Initial)

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ADAPTIVE LEADINGEDGE DROOP MECHANIS

CHRIS, REIDY


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PRIVATE AIRCRAFT

STALLING

ANGLEFIXEDWINGCUFF

ADAPTIVEWING CUFF

DESIGNPROCESS

2D DESIGN

3D DESIGN

INTERNALMECHANISM

MATERIALS

STALLING ANGLE

FUELCONSUMPTIONMONETARY

SAVINGSCARBONFOOTPRINT

P R O B

L E M

S O L U

T I O N

A D V A

N T A G E S

1 2 3 4


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PRIVATE AIRCRAFT

STALLING

ANGLEFIXEDWINGCUFF

P R O B

L E M

1


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At high angles of attack, privateaircraft undergo stalling caused byseparation of airflow.

Stalling causes sudden drop in lift,resulting in loss of pilot control.

Fixed leading edge droop malleviates airflow separationincreases stalling angle.

However, it increases drag angles of attack.

STALLING ANGLE PRIVATE AIRCRAFT


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ADAPTIVEWING CUFF

DESIGNPROCESS

2D DESIGN

3D DESIGN

INTERNALMECHANISM

MATERIALS

S O L U

T I O N

2


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RESEARCHFINALDESIG

N

MODELIN

ACCOMPLISHING THE FINAL DESIGN DESIGN PROCESS

THE IDEAFUEL

EFFICIENCYFLIGHT SAFETY

PRIVATE AIRCRAFTSPECIFICATIONS

FIXED LEADINGEDGE CUFFS

AIRFOIL AND WINGDESIGN AND ANALYSIS C


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FLIGHT ADAPTABILITY DROOP MECHANISM

The mechanism can modify angle of leading edge droop during flight. Alleviates stalling conditions Increases fuel efficiency


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CESSNA SKYCATCHER FLIGHT CONDITIONS


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FLIGHT CONDITION OPTIMAL DRAG AIRFOIL OPTIMAL STALLING AIRFOIL L/D

Climb #1 15 Cuff 15 Cuff 125.5

Climb #2 15 Cuff 20 Cuff 133.5

Cruise #1 15 Cuff 20 Cuff 133.0

Cruise #2 15 Cuff 20 Cuff 135.6

Descent #1 15 Cuff 20 Cuff 130.1

Descent #2 15 Cuff 20 Cuff 119.8

OPTIMAL AIRFOILS FOR CRUISE & STALLINGAIRFOIL SELECTION


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BASELINE MODELCESSNA SKYCATCHER

WING CUFF MODEL

3D GEOMETRY WING DESIGN

AUTODESK

INVENTOR

FUSION


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AIRFLOW CONTOURS WING CFD ANALYSIS

WITHOUTCUFF

WITH CUFF


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PARTICLE IMAGE VELOCIMETRYWIND TUNNEL ANALYSIS

CRUISE CONDITIONS STALLINGCONDITIONS

BASELINE

12.5 CUFF

20 CUFF


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MOTILE APPARATUS FOR DROOP MODIFICATIONINTERNAL MECHANISM DES

Force = 160 lb

Weight = 10.7 lb Factor of Safety = 2.5

LINEAR ACTUATOR

FINAL INTERNAL MECHANISMIS LINEAR ACTUATOR

BECAUSE IT HAS HIGHERFACTOR OF SAFETY FORAPPROXIMATELY SAME

WEIGHT.


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STALLING ANGLE

FUELCONSUMPTIONMONETARYSAVINGS

CARBONFOOTPRINT

A D V A

N T A G E S

3


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MONETARY SAVINGS AND CARBON FOOTPRINTGREEN TECHNOLOGY

COMPARED TOBASELINE

520 Th gal fuel $3.227 M 9.575 M lb CO 2 200 Th trees

COMPARED TOFIXED CUFF

630 Th gal fuel $3.902 M 11.577 M lb CO 2 240 Th trees

THE ADAPTIVE LEADING EDGE DROOPIS MORE FUEL EFFICIENT


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INCREASED STALLING ANGLEFLIGHT SAFETY


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4


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MAKINGOUR DESIGN A REALITYNEXT STEP PLAN

Step4

Step3

Step2

Step1

Obtain insurance andpatent for design

Propose design andbudget to major

funding organizations

Obtain requiredresources and

facilities to constructdesign

Perform flight tfinal aircraft

perform inspe

PROTECTION FUNDING DEVELOPMENT VERIFICATIO


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IDENTIFYING POTENTIAL INVESTORSTARGET MARKET

PRIVATE

PILOTS

Pre-Market

ManufacturingCessna, GKN Aerospace,

etc.

Private Aircraft Companies

Aviation and Aerospace Industry

1. Pitching the design to private aircrmanufacturers such as Cessna

2. Licensed to private manufacturersproduction

Governmenbe pursued, Departmenand of Ene

the Fe Ad


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INVESTMENT SOURCES FUNDING MECHANISMS

G

PRIVATE INVESTMENT

1. Major source of funding will be private aircraftcompanies who invest in our design in order toimplement it in their own aircraft and accrueincreased sales / profits in the future.

2. In recent years, government has been pushing forsafer and more fuel efficient transportation, whichis the goal of our project. Government grants will

be pursued from Departments of Energy andTransportation, and Federal Aviation Administration.


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COMPETITIVE REFERENCE


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ATTRIBUTE FIXED WING CUFFS VARIABLE SLATS STOL KITS

Flight Safety

Fuel Efficiency

Price

Ease of Usage

ASSESSMENT

PRODUCT ASSESSMENT COMPETITIVE REFERENCE

ENDORSEMENT


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INCREASING STALLING ANGLEENDORSEMENT

Professionals in the aeronauticalalready shown interest in our dethis endorsement from Pratt &Dr. Manoj Rahematpura .

We are also currently working toGKN Aerospace .


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AeroMorph Presentation (Initial)

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