CARBON FIBER WING - Proof Load Test Setup! (Wing Load Test)
For more DarkAero action check out: https://www.youtube.com/darkaeroinc/join
(Exclusive members only content including photos, videos, live Q&A and more!)
Wing Proof Load Test Tool: https://www.darkaero.com/knowledge/aircraft-design/
DarkAero 1 - https://www.darkaero.com/aircraft
DarkAero Apparel - https://www.darkaero.com/shop
The DarkAero 1 utilizes a carbon fiber wing that is constructed using a unique structural approach called Hollow Grid. Before flying this wing, we needed to prove it can handle the stresses generated by aerodynamic loads in flight. In this video, Ryan talks through some of the hardware and other details of the setup for the positive G proof load test.
We had to built a test fixture to support the wing in an inverted position and then level it in the roll direction. The inverted orientation allowed us to use the weight of sand bags to simulate aerodynamic lift loads. The support fixture was designed to hold the wing at a specific pitch attitude to replicate worst case loads for the wing structure. We chose to build the test stand out of wood because it is easy to work with and cost effective. However, we had to install some localized aluminum and steel reinforcements into the test stand where the wing attach bolts interfaced.
Mechanical scissor jacks were positioned under the wings to help control the wing load and wing deflection during the test. We had to make pads to distribute the reaction forces from the jacks into the wing. The pads were made from sections of CNC cut foam.
We also made foam pads to sit on top of the wing in between the sand/concrete bags and the wing skin. The foam pads were marked to guide the position of sand bags that were stacked on the wing. The sand bag distribution was generated and tracked with a spreadsheet tool we created.
Around the perimeter of the wing was an aluminum frame with rulers attached to it to measure the deflection and the twist of the wing. FAR Part 23 states that the wing must sustain limit loads without detrimental or permanent deformation. While the wing was deflected, we confirmed that the ailerons were able to still move freely.
For the next test we plan to add station labels on the wing to more clearly organize the position of weights.
Thank you for watching!
00:00 - Intro
00:29 - Test Fixture
02:15 - Load Control
03:34 - Load Pads
06:28 - Measurements
08:20 - Lessons Learned
If you enjoyed this video and would like to see more of this type of content, follow along as we work to create the fastest, longest range aircraft you can build in your garage.
More information on DarkAero can be found on our website and other social media accounts:
https://www.darkaero.com
https://www.facebook.com/darkaeroinc
https://www.instagram.com/darkaeroinc
https://www.linkedin.com/company/darkaero-inc
Видео CARBON FIBER WING - Proof Load Test Setup! (Wing Load Test) канала DarkAero, Inc
(Exclusive members only content including photos, videos, live Q&A and more!)
Wing Proof Load Test Tool: https://www.darkaero.com/knowledge/aircraft-design/
DarkAero 1 - https://www.darkaero.com/aircraft
DarkAero Apparel - https://www.darkaero.com/shop
The DarkAero 1 utilizes a carbon fiber wing that is constructed using a unique structural approach called Hollow Grid. Before flying this wing, we needed to prove it can handle the stresses generated by aerodynamic loads in flight. In this video, Ryan talks through some of the hardware and other details of the setup for the positive G proof load test.
We had to built a test fixture to support the wing in an inverted position and then level it in the roll direction. The inverted orientation allowed us to use the weight of sand bags to simulate aerodynamic lift loads. The support fixture was designed to hold the wing at a specific pitch attitude to replicate worst case loads for the wing structure. We chose to build the test stand out of wood because it is easy to work with and cost effective. However, we had to install some localized aluminum and steel reinforcements into the test stand where the wing attach bolts interfaced.
Mechanical scissor jacks were positioned under the wings to help control the wing load and wing deflection during the test. We had to make pads to distribute the reaction forces from the jacks into the wing. The pads were made from sections of CNC cut foam.
We also made foam pads to sit on top of the wing in between the sand/concrete bags and the wing skin. The foam pads were marked to guide the position of sand bags that were stacked on the wing. The sand bag distribution was generated and tracked with a spreadsheet tool we created.
Around the perimeter of the wing was an aluminum frame with rulers attached to it to measure the deflection and the twist of the wing. FAR Part 23 states that the wing must sustain limit loads without detrimental or permanent deformation. While the wing was deflected, we confirmed that the ailerons were able to still move freely.
For the next test we plan to add station labels on the wing to more clearly organize the position of weights.
Thank you for watching!
00:00 - Intro
00:29 - Test Fixture
02:15 - Load Control
03:34 - Load Pads
06:28 - Measurements
08:20 - Lessons Learned
If you enjoyed this video and would like to see more of this type of content, follow along as we work to create the fastest, longest range aircraft you can build in your garage.
More information on DarkAero can be found on our website and other social media accounts:
https://www.darkaero.com
https://www.facebook.com/darkaeroinc
https://www.instagram.com/darkaeroinc
https://www.linkedin.com/company/darkaero-inc
Видео CARBON FIBER WING - Proof Load Test Setup! (Wing Load Test) канала DarkAero, Inc
Показать
Комментарии отсутствуют
Информация о видео
Другие видео канала
We Load Tested the Wing! - DarkAero Progress Update - August 31, 2020How we set up the NEGATIVE G proof load test for the DarkAero 1 wing!BUILDING AEROBATIC CARBON WINGElixir's Molded Carbon AircraftMaking a Carbon Fiber Rear Wing with DRSCARBON FIBER + Honeycomb Sandwich Panels in the DarkAero 1 EXPLAINED!Manufacturing Carbonfiber Wing SkinsCo-Cured Wing Structure Using Dry Carbon Fiber Application/Overbraiding & Resin Transfer MoldingHow Diamond Builds Composite AircraftWhy this propeller is different: Airmaster Propeller on the DarkAero 1Simulating Stall of the DarkAero 1 Using SimScale Cloud-Based CFDDarkAero Shop Life 7 - Firewall Hardpoints, Electrical Grounds, Machining Fixtures - Mar 12-13, 2020How to Make a Carbon Fiber Wing [DIY] (with 3D Printed Molds)UL Power UL520iS Engine Install on the DarkAero 1 - Part 1Carbon Fiber - 5 Things You (probably) DON'T KnowSecrets to Machining an Aerospace Part on a Tormach CNC MillCarbon fiber aircraft prototype wing ribsDarkAero 1 Progress Update (Feb 2021)Why We Use Different Types of Carbon Fiber in the DarkAero 1