LEAP 71 (@leap_71) 's Twitter Profile
LEAP 71

@leap_71

We create computational models for engineering to build the world's most advanced machines.

ID: 1589262417128824833

linkhttps://leap71.com calendar_today06-11-2022 14:24:31

260 Tweet

752 Followers

2 Following

Lin Kayser (@linkayser) 's Twitter Profile Photo

"AI in engineering" - or not?. I wrote an article about our work at LEAP 71 for Metal AM in which I describe our tech stack, why LLMs are (mostly) a bad idea for engineering, and how we finally get J.A.R.V.I.S.

"AI in engineering" - or not?. I wrote an article about our work at <a href="/leap_71/">LEAP 71</a> for <a href="/MetalAMMag/">Metal AM</a> in which I describe our tech stack, why LLMs are (mostly) a bad idea for engineering, and how we finally get J.A.R.V.I.S.
LEAP 71 (@leap_71) 's Twitter Profile Photo

Rocket engines that donโ€™t fly: We use Noyron to build advanced heat exchangers for our clients in the aerospace, energy, and A/C cooling industries - and beyond.

Rocket engines that donโ€™t fly: We use Noyron to build advanced heat exchangers for our clients in the aerospace, energy, and A/C cooling industries - and beyond.
LEAP 71 (@leap_71) 's Twitter Profile Photo

A lightweight high-performance customizable and stackable water/water heat exchanger for the energy sector designed using the Noyron Large Computational Engineering Model. The inside structure consists of checkerboard-interleaved cooling channels, oriented to be 3D printable.

A lightweight high-performance customizable and stackable water/water heat exchanger for the energy sector designed using the Noyron Large Computational Engineering Model. The inside structure consists of checkerboard-interleaved cooling channels, oriented to be 3D printable.
LEAP 71 (@leap_71) 's Twitter Profile Photo

A look from above our 2000 kN reference engine shows the injector head optimized for the inflow of hot gaseous methane and oxygen at the mass flows required to feed the engine. The twin methane inlets are on the side, the GOX inlet in the center. Created by Noyron without CAD.

A look from above our 2000 kN reference engine shows the injector head optimized for the inflow of hot gaseous methane and oxygen at the mass flows required to feed the engine. The twin methane inlets are on the side, the GOX inlet in the center. Created by Noyron without CAD.
LEAP 71 (@leap_71) 's Twitter Profile Photo

Assembling a 1.5kN thruster at the test stand. Like all of our rocket engines, this one was created from the same shared DNA, encoded in the Noyron Large Computational Engineering Model. The regen-cooled Kerolox engine was generated without human intervention and 3D printed.

Assembling a 1.5kN thruster at the test stand. Like all of our rocket engines, this one was created from the same shared DNA, encoded in the Noyron Large Computational Engineering Model. The regen-cooled Kerolox engine was generated without human intervention and 3D printed.
LEAP 71 (@leap_71) 's Twitter Profile Photo

A compact 2kN KeroLOX rocket engine with a Pintle injector. Pintle injectors have advantages for small engines, especially for the deep throttling required for lunar landers. Generated autonomously by the Noyron Large Computational Engineering Model.

A compact 2kN KeroLOX rocket engine with a Pintle injector. Pintle injectors have advantages for small engines, especially for the deep throttling required for lunar landers. Generated autonomously by the Noyron Large Computational Engineering Model.