WO2026102403A1 - Procédés d'assemblage de structures de support métalliques pour véhicules - Google Patents

Procédés d'assemblage de structures de support métalliques pour véhicules

Info

Publication number
WO2026102403A1
WO2026102403A1 PCT/US2025/054830 US2025054830W WO2026102403A1 WO 2026102403 A1 WO2026102403 A1 WO 2026102403A1 US 2025054830 W US2025054830 W US 2025054830W WO 2026102403 A1 WO2026102403 A1 WO 2026102403A1
Authority
WO
WIPO (PCT)
Prior art keywords
metallic
panel
vehicle
support structure
structures
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
PCT/US2025/054830
Other languages
English (en)
Inventor
Luis Leon
Gary Coleman
Samantha VERONESE
Todd Morton
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Supernal LLC
Original Assignee
Supernal LLC
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Supernal LLC filed Critical Supernal LLC
Publication of WO2026102403A1 publication Critical patent/WO2026102403A1/fr
Pending legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B32—LAYERED PRODUCTS
    • B32B—LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT OR NON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
    • B32B3/00—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form
    • B32B3/10—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material
    • B32B3/12—Layered products comprising a layer with external or internal discontinuities or unevennesses, or a layer of non-planar shape; Layered products comprising a layer having particular features of form characterised by a discontinuous layer, i.e. formed of separate pieces of material characterised by a layer of regularly- arranged cells, e.g. a honeycomb structure
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0054—Fuselage structures substantially made from particular materials
    • B64C2001/0081—Fuselage structures substantially made from particular materials from metallic materials

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)

Abstract

L'invention concerne un procédé d'assemblage de structures métalliques d'un véhicule. Le procédé consiste à agencer la pluralité de structures métalliques et à assembler la pluralité de structures métalliques. L'invention concerne également une structure de support pour un véhicule. Le véhicule comprend un panneau, et la structure de support comprend un panneau métallique comportant une partie surélevée présentant une forme géométrique formée d'une seule pièce avec une surface et faisant saillie de celle-ci, et une partie renfoncée adjacente à la partie surélevée. Un adhésif non métallique est appliqué à la partie surélevée ou à la partie renfoncée, et une soudure est appliquée à une distance prédéterminée de l'adhésif au niveau d'un emplacement d'accouplement.
PCT/US2025/054830 2024-11-11 2025-11-10 Procédés d'assemblage de structures de support métalliques pour véhicules Pending WO2026102403A1 (fr)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US202463718949P 2024-11-11 2024-11-11
US202463718943P 2024-11-11 2024-11-11
US63/718,943 2024-11-11
US63/718,949 2024-11-11

Publications (1)

Publication Number Publication Date
WO2026102403A1 true WO2026102403A1 (fr) 2026-05-15

Family

ID=99765912

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2025/054830 Pending WO2026102403A1 (fr) 2024-11-11 2025-11-10 Procédés d'assemblage de structures de support métalliques pour véhicules

Country Status (1)

Country Link
WO (1) WO2026102403A1 (fr)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130251510A1 (en) * 2012-03-01 2013-09-26 The Boeing Company Spf/db structure for attenuation of noise from air flow
US20140008144A1 (en) * 2012-07-06 2014-01-09 C&D Zodiac, Inc. Aircraft interior panel with acoustic materials
US20200086624A1 (en) * 2016-12-22 2020-03-19 Agency For Science, Technology And Research Method and system of manufacturing a load-bearing structure and a load-bearing structure manufactured thereof
US20220048131A1 (en) * 2020-08-14 2022-02-17 Lincoln Global, Inc. Refill friction stir spot welding tool and end effector
US20240083603A1 (en) * 2023-11-17 2024-03-14 Daniel Keith Schlak Bladeless eVTOL Passenger Aircraft with Fixed-Wing Forward Flight Travel, and Method and Power Plant Therefor

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20130251510A1 (en) * 2012-03-01 2013-09-26 The Boeing Company Spf/db structure for attenuation of noise from air flow
US20140008144A1 (en) * 2012-07-06 2014-01-09 C&D Zodiac, Inc. Aircraft interior panel with acoustic materials
US20200086624A1 (en) * 2016-12-22 2020-03-19 Agency For Science, Technology And Research Method and system of manufacturing a load-bearing structure and a load-bearing structure manufactured thereof
US20220048131A1 (en) * 2020-08-14 2022-02-17 Lincoln Global, Inc. Refill friction stir spot welding tool and end effector
US20240083603A1 (en) * 2023-11-17 2024-03-14 Daniel Keith Schlak Bladeless eVTOL Passenger Aircraft with Fixed-Wing Forward Flight Travel, and Method and Power Plant Therefor

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