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Boeing and Airbus have explored designs for blended wing aircraft – now California-based JetZero aims to put one into service by 2030. Boeing and Airbus have explored designs for blended wing ...
Blended-wing planes have already been flying for years in the military. The B-21 Raider is among the blended-in wing planes bought by the USAF. US Air Force via AP
The Boeing X-48 is an American experimental unmanned aerial vehicle (UAV) built to investigate the characteristics of blended wing body (BWB) aircraft. Boeing designed the X-48 and two examples were built by Cranfield Aerospace in the UK. Boeing began flight testing the X-48B version for NASA in 2007. The X-48B was later modified into the X-48C ...
Illustration of the Boeing SUGAR Volt concept aircraft. SUGAR Volt is the hybrid aircraft concept proposed by a team led by Boeing's Research & Technology division. It is one of a series of concepts put forward in response to a request for proposals for future aircraft issued by NASA.
The Boeing X-66 is an experimental airliner under development by Boeing. It is part of the X-plane series, and is being developed in collaboration with NASA and its Sustainable Flight Demonstrator program. It will use an extra-long and thin wing design stabilized by diagonal bracing struts, which is known as a Transonic Truss-Braced Wing.
Natilus' design for a "blended-wing" concept combines the wing and fuselage to increase efficiency. Imagine a B-21 bomber with passenger windows.
A blended wing body (BWB), also known as blended body, hybrid wing body (HWB) or a lifting aerofoil fuselage, [1] is a fixed-wing aircraft having no clear dividing line between the wings and the main body of the craft. [2] The aircraft has distinct wing and body structures, which are smoothly blended together with no clear dividing line. [3]
silhouettes of Boeing NMA concept at right between 787-8 on top and 737 MAX 10 on bottom, as presented at Paris Air Show 2017. At the June 2017 Paris Air Show, Boeing's aircraft development manager Mike Delaney confirmed the use of composites for the whole airframe, which would have a hybrid cross-section and bypass ratios above 10:1. [23]