Skip to end of metadata
Go to start of metadata

You are viewing an old version of this page. View the current version.

Compare with Current View Page History

« Previous Version 12 Next »

eBig Project

Project

Project Manager

Post-comp fixed wing

Wing Design

Nathaniel Li

Task Description

Based upon current CAD of the wings and research completed, design ailerons for our wings to allow for the correct flight controls. Refer to Wings for the design decisions made for the wings. The CAD can be found in PDM at Fixed Wing → Fixed Wing Design → Wings.

Additionally, refer to Aileron Sizing for a starting point. A lot of the research and calculations were based on Sizing Control Surfaces which can also be used for reference. The fixed wing calculator has lots of working info as well.

I suggest brainstorming a few ideas and asking for feedback as there are many factors at play. This task may require more research into aileron shapes. Some thought into linkage/servo connection would also be good.

Constraints

Constraints

Written By

Append Date

1 aileron per wing

Nathaniel Li

Adheres to sizing found in Aileron Sizing

Nathaniel Li

Relevant Contacts

Subteam

Contact

Contact Description

Subteam collaborating with

@ of contact

what is the contact responsible for?

Assignees

Task Progression/Updates

Author: @ person updating Date: 2024/09/25

Design Progression #1

Initial Ideas:

  • The initial idea is to take the existing rib and create a cut, splitting it into two parts.

    • The more extensive section of the rib towards the leading edge will form the profile for the main wing.

    • The smaller section of the rib towards the trailing edge will form the rib of the aileron flap.

      WingAileronCut.png

  • The aileron and the rest of the wing will be covered in the same singular piece of fabric.

    • The fabric will cover gaps between the aileron and wing. This is thought to improve aerodynamics.

  • The aileron will be attached to the wing by a hinge at the top edge of the rib.

    • Top placement reduces adverse yaw.

    • The servo will control the aileron movement using a horn and torque rod.

Progress:

Initial Ideas

  • The idea was to overlap the aileron cutout with the total aerofoil and connect them with a spar or pin.

    • Concern → weakness of a balsa joint with a metal pin passed through

  • Idea 1: use a sheet metal plate on either side of the balsa rib to reinforce the joint → whether we want to use

    • Concerns →

      • Lack of vertical constraint and twisting resistance with the balsa for the rest of the rib that is not covered by the sheet metal.

      • Use an aileron leading edge spacer across the entire design → weight concern

  • The result was to instead use frame to strengthen the ribs and constrain them from movement as shown in Design #1:

Design #1: Embedded mounts with Sheet Metal Rib Frames

image-20241003-224357.png

Dimensions:

  • Aileron Cord:

    • In line with the suggestions for the cord length

      • Total cord length: 230mm

      • Aileron Cord: 57.5mm → 25% of the cord (upper end of 15-25%)

  • Aileron Span

    • Total semi span: 750mm

    • Aileron span: 250mm

    • Aileron Span Ratio: 33.3% → 35% of the cord (below lower end by 2%) → concern of increasing since the design needs the ribs to line up.

    • Concern → syncing up with the existing rib spacing and the wing's trailing edge with a potential cutout and wall to mount the wing hinge

Current Mass

  • Mass: 22.53 grams

    • → excludes integration mechanism and corresponding changes.

Suggestions for Servo Horn Mount:

  • Place holder depending on the servo used:

image-20241002-004842.png

Author: Nathaniel Li Updating Date:

Aileron Sync

  • Confirm using the updated ribs

  • CAD the overlap design

  • Required materials → Manufacturing

    • Try everything to be a 3D print

  • Make a weight comparison

  • TBD servo placement (need to get from Smile?)

  • No labels