CRP Technology Used SLS 3D Printing and Windform XT 2.0 to Make Aircraft Model for Wind Tunnel Testing

The new AW609 wind tunnel model designed for Leonardo HD by Metaltech S.r.l. and 3D printed by CRP Technology

CRP Technology, part of the larger CRP Group, is well-known for its 3D printing applications in the automotive sector, but lest we forget that it is also accomplished in aerospace 3D printing, the company has come out with a new case study about its work creating a new 3D printed wind tunnel model (1:8.5 scale) of the Leonardo TiltRotor AW609 for the Leonardo Helicopter Division (Leonardo HD, formerly known as AgustaWestland).

According to the case study, CRP Technology was able to “highlight the perfect union” between its advanced SLS 3D printing technology and high-performance, composite Windform materials – particularly its Windform XT 2.0, a polyamide-based carbon fiber reinforced composite. Metaltech S.r.l. designed the model.

The goals of Leonardo HD’s project included:

• design and manufacture an internal main structure out of aluminum alloy that can easily have new geometries added
• complete the work in a very short timetable, but with an extremely high level of commonality and reliability
• make components out of materials with high mechanical and aerodynamic characteristics

3D printed aircraft propeller spinners

These goals are why Leonardo HD was referred to CRP Technology – it would be able to meet these goals while 3D printing the external parts for the wind tunnel model, which was designed, manufactured, and assembled in order to complete a series of dedicated low-speed wind tunnel tests. Some of the parts that were 3D printed for the wind tunnel model include nose and cockpit components, fairings, external fuel tanks, rear fuselage, wings, and nacelles.

The level of detail that went into these 3D printed parts “is crucial to the applied loads to be sustainable,” as the wind’s aerodynamic loads in the tunnel are high. So load resistance was one of the more important project aspects, along with maintaining good dimensional tolerances, under load, of large components.

“It is important to remember that the performance of these components affects the final performance of the entire project, especially because the external fairings have to transfer the aerodynamic loads generated by the fuselage to the internal frame,” CRP Technology wrote in the case study.

3D printed tail fairing

The tests needed to cover the standard range of flight attitudes at Leonardo HD’s Michigan wind tunnel facility, in addition to Politecnico di Milano, and varying external geometries were changed during testing, so that technicians would be able to gain a better understanding of “aerodynamic phenomena.”

Today, the CAD-CAM approach is used to design models for wind tunnel testing, before an internal structural frame of aluminum and steel is milled and assembled. Then, 3D printing is used to obtain all external geometries. Because Leonardo HD used CRP Technology’s advanced 3D printing and Windform XT 2.0 material the project was completed much more quickly, with “excellent results and with high-performing mechanical and aerodynamic properties.”

CRP analyzed the dimensional designs that Leonardo HD had sent in order to make the best composite material recommendation: its Windform XT 2.0, with high heat deflection, increased tensile strength and modulus, superior stiffness, and excellent detail reproduction.

“The choice of the Windform XT 2.0 composite material was not casual, all the goals required by Leonardo HD were considered, such as the importance of a short realization time, good mechanical performances and also good dimensional characteristics,” CRP Technology wrote in the case study.

It was necessary to 3D print the single parts separately, as “some components were dimensionally superior to the construction volume of the 3D printing machines,” but CRP Technology was able to complete the project with no time delays. The company used CAD to evaluate the working volume’s functional measures in order to determine which parts to split, and to figure out how to maximize contact surface where structural adhesive would be added to the model.

3D printed aircraft nose and cockpit

It only took four days to 3D print the various parts of the components.

The case study noted, “Different confidential efficiencies, which are an integral part of CRP Technology’s specific know-how, allowed the reduction of the delivery lead time and allowed CRP to minimize the normal tolerances of this technology, and eradicate any potential problem of deformation or out of tolerance.”

The completed model underwent surface finishing, before it was assembled by Metaltech S.r.l. and mounted directly onto a rig assembly, so any small imperfections resulting from single components being put together could be optimized. Thanks to CRP Technology, this step was finished very quickly, and Leonardo HD was able to efficiently flatten the model’s surface and treat it with a special liquid to both prepare for painting and make the model waterproof.

Leonardo HD needed to review the behavior of the aircraft, and so completed a high-speed wind tunnel test campaign, which encompassed speeds Mach 0.2-Mach 0.6, on a new 1:6 scale model at NASA Ames Unitary Plan 11′ x 11′ transonic wind tunnel. The company called on CRP USA, based in North Carolina, to speed up the process, using its partner company’s SLS 3D printing and Windform XT 2.0 composite material to make the external fuselage and some additional components.

3D printed model installed in the 11’x 11’ test section at NASA Ames

While the architecture of the new 3D printed model, which spanned nearly 2 meters, is similar to the original AW609 version, some improvements were made so remote controls could be used for the wing flaperons and elevator surfaces. Additionally, by using four different 6-component strain gauge balances, all the loads were able to act on the complete model, the nacelle, the tail surfaces, and the wing alone.

The model was constructed in such a way as to be mounted in the transonic wind tunnel on a single strut straight sting support system.

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