Nothing Special   »   [go: up one dir, main page]

Hoyt Haight et al., 2006 - Google Patents

Design and fabrication of light rigidizable inflatable wings

Hoyt Haight et al., 2006

Document ID
8322255372144923354
Author
Hoyt Haight A
Allred R
Harrah L
McElroy P
Scarborough S
Smith T
Publication year
Publication venue
47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 14th AIAA/ASME/AHS Adaptive Structures Conference 7th

External Links

Snippet

The overall objective of this ongoing study is to develop light-curing resins and lighting systems to rigidize an inflatable wing for terrestrial and space applications. Rigidization of inflatable wings provides several potential advantages over current continuous pressure …
Continue reading at arc.aiaa.org (other versions)

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06—Frames; Stringers; Longerons; Fuselage sections
    • B64C1/12—Construction or attachment of skin panels
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces and the like
    • B64C1/06—Frames; Stringers; Longerons; Fuselage sections
    • B64C1/064—Stringers; Longerons
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/18—Spars; Ribs; Stringers

Similar Documents

Publication Publication Date Title
Ghori et al. The role of advanced polymer materials in aerospace
Takahashi et al. Development of variable camber wing with morphing leading and trailing sections using corrugated structures
Umamaheswar et al. Modelling of a patch repair to a thin cracked sheet
Thill et al. Composite corrugated structures for morphing wing skin applications
EP2084057B1 (en) Composite aircraft structures with hat stiffeners
US9352822B2 (en) Bonded composite airfoil
ES2646587T3 (en) Fixing ribs of an aircraft to stringers that have a variable geometry
EP2844555B1 (en) Morphing aerofoil
ES2770020T3 (en) Structural bonded patching element with tapered adhesive design
BRPI0721604A2 (en) integrated multi-purpose composite material twist box
JP6352187B2 (en) Integrated surface thermal management system
BR102017001471A2 (en) AERODYNAMIC BODY
Basri et al. Performance analysis of composite ply orientation in aeronautical application of unmanned aerial vehicle (UAV) NACA4415 wing
WO2015130985A1 (en) Composite sandwich panel having curable composite skins with asymmetrical resin distributions
WO2008053052A1 (en) Method for optimising the structural design of a composite stiffened panel
WO2010112644A1 (en) Structure for assembly of the pressure bulkhead of an aircraft
ES2596555T3 (en) Aircraft structure with means of reducing the risk of detachment in different deformation areas
TW201437031A (en) Triaxial fiber-reinforced composite laminate
KR20160019040A (en) Folded composite filler
EP3546200B1 (en) Methods for forming bonded structures
US20140377500A1 (en) Composite structure, aircraft wing and aircraft fuselage including composite structure, and method of manufacturing composite structure
Fielding et al. Design and manufacture of the DEMON unmanned air vehicle demonstrator vehicle
Hoyt Haight et al. Design and fabrication of light rigidizable inflatable wings
US10573772B2 (en) Composite vehicle skin co-cured with solar-cell array
US11319052B2 (en) Leading-edge arrangement for a flow body of a vehicle