-
公开(公告)号：US20240294256A1
公开(公告)日：2024-09-05
申请号：US18593719
申请日：2024-03-01
申请人： Joby Aero, Inc.
摘要： An oblique flying wing aircraft with internal ducting and airflow. The aircraft may have propulsion units within the wing body. The propulsion units may be off-axis internal to the wing to utilize locations with larger internal space available. In some aspects, the multi-segment oblique flying wing aircraft may have three distinct segments including two outer wing segments and a central wing segment. The central segment may be thicker in the vertical direction and adapted to hold pilots and passengers. The outer wing segments may be substantially thinner and may taper as they progress outboard from the wing center. The multi-segment oblique flying wing aircraft be adapted for rotating into a high-speed flight configuration, or may be adapted for take-off and cruise at a constant angle.
-
公开(公告)号：US20240253773A1
公开(公告)日：2024-08-01
申请号：US18375540
申请日：2023-10-01
申请人： JETZERO, INC.
发明人： Mark Allan Page
摘要： An apparatus for ingesting boundary layer flow on an aircraft, the apparatus includes a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and main body of the aircraft, wherein the blended wing body includes a nacelle located aft of a leading edge of the blended wing body, wherein the nacelle includes a propulsor configured to propel the aircraft, a primary duct, and a flow augmentation arrangement, wherein the flow augmentation arrangement is configured to accelerate a boundary layer flow in the airflow, wherein the flow augmentation arrangement further includes a secondary duct, wherein the secondary duct configured to ingest the boundary layer flow in the airflow from an inlet proximal to a forward portion of the nacelle to an outlet proximal to a rear portion of the nacelle and a tertiary duct between the primary duct and the secondary duct.
-
公开(公告)号：US20240253763A1
公开(公告)日：2024-08-01
申请号：US18101914
申请日：2023-01-26
申请人： JETZERO, INC.
发明人： John Vassberg , Blaine Rawdon
摘要： A system for providing favorable environment for propulsion system of a blended wing body aircraft, wherein the system comprises a blended wing body, wherein the blended wing body comprises a main body, wherein the main body comprises a main body shaping comprising an upper aft surface configured to provide a favorable environment for a propulsion system of the blended wing body aircraft, and the propulsion system mounted to the upper aft surface of the main body, wherein the propulsion system comprises one or more prime movers, and a nacelle covering the one or more prime movers.
-
公开(公告)号：US20240124122A1
公开(公告)日：2024-04-18
申请号：US18375542
申请日：2023-10-01
申请人： JETZERO, INC.
发明人： Mark A. Page
CPC分类号： B64C9/02 , B64C39/10 , B64C2039/105
摘要： Aspects relate to airplanes having a blended wing body. A blended wing body may include a fuselage and a port wing and a starboard wing continuously coupled to the fuselage and a nose section. A midship control surface may be disposed on a trailing edge of the blended wing body and centered between the port wing and the starboard wing.
-
公开(公告)号：US11905007B2
公开(公告)日：2024-02-20
申请号：US17340811
申请日：2021-06-07
发明人： Geoffrey C. Bower
CPC分类号： B64C29/0033 , B64C23/069 , B64C39/10 , B64D27/24
摘要： A passenger vertical take-off and landing aircraft includes a flying wing comprising a passenger compartment, a first set of rotors positioned at least partially forward of a leading edge of the flying wing, and a second set of rotors positioned at least partially rearward of a trailing edge of the flying wing. The first set of rotors may include at least four rotors and the second set of rotors may comprise at least two rotors. The first set of rotors, the second set of rotors, both, or neither may be tiltable between lift configurations for providing lift for vertical take-off and landing of the aircraft and propulsion configurations for providing forward thrust to the aircraft.
-
公开(公告)号：US11897601B2
公开(公告)日：2024-02-13
申请号：US17672860
申请日：2022-02-16
申请人： JETZERO, Inc.
CPC分类号： B64C23/076 , B64C9/06 , B64C39/10 , B64C13/24 , B64C2039/105
摘要： Aspects relate to aircraft and methods of use for aerodynamic control with winglet surfaces. In an aspect an exemplary aircraft includes a first wing having a first winglet at a distal end of the wing, wherein the first winglet comprises at least a first control surface at a first trailing edge of the first winglet and a second wing having a second winglet at a distal end of the wing, wherein the second winglet comprises at least a second control surface at a second trailing edge of the second winglet.
-
公开(公告)号：US11891178B2
公开(公告)日：2024-02-06
申请号：US17731622
申请日：2022-04-28
申请人： JETZERO, INC.
CPC分类号： B64C39/10 , B64D15/00 , B64D37/30 , B64C2039/105 , B64D2041/005 , B64D2221/00
摘要： A system for a blended wing body aircraft with a combustion engine is illustrated. The aircraft comprises a blended wing body, at least a fuel source located within the blended wing body and configured to store a fuel, wherein the fuel includes liquid hydrogen, and at least a propulsor configured to propel the blended wing body aircraft. The at least a propulsor comprises a combustion engine configured to burn the fuel from the fuel source and produce mechanical work to power the at least a propulsor.
-
公开(公告)号：US20230406504A1
公开(公告)日：2023-12-21
申请号：US18144601
申请日：2023-05-08
申请人： JETZERO, INC.
CPC分类号： B64D11/00 , B64C39/00 , B64C1/22 , B64C2039/105 , B64D25/14 , B64C39/10 , B64C1/10 , B64C1/1423
摘要： Technologies for providing emergency egress routes for a blended wing body aircraft are described herein. In some examples, the emergency egress routes are through a side cabin bulkhead and aft one or more cargo holds. In some examples, the blended wing body aircraft has wings that are high geometry wings. In these examples, the emergency egress routes do not penetrate an aft spar, reducing weight and increasing the integrity of the aircraft.
-
公开(公告)号：US11827355B2
公开(公告)日：2023-11-28
申请号：US17873679
申请日：2022-07-26
申请人： JETZERO, INC.
发明人： Mark A. Page
CPC分类号： B64C9/02 , B64C39/10 , B64C2039/105
摘要： Aspects relate to airplanes having a blended wing body. A blended wing body may include a fuselage and a port wing and a starboard wing continuously coupled to the fuselage and a nose section. A midship control surface may be disposed on a trailing edge of the blended wing body and centered between the port wing and the starboard wing.
-
公开(公告)号：US11827339B1
公开(公告)日：2023-11-28
申请号：US18102342
申请日：2023-01-27
申请人： JETZERO, INC.
发明人： Mark Allan Page
摘要： An apparatus for ingesting boundary layer flow on an aircraft, the apparatus includes a blended wing body, wherein the blended wing body is characterized by having no clear dividing line between wings and main body of the aircraft, wherein the blended wing body includes a nacelle located aft of a leading edge of the blended wing body, wherein the nacelle includes a propulsor configured to propel the aircraft, a primary duct, and a flow augmentation arrangement, wherein the flow augmentation arrangement is configured to accelerate a boundary layer flow in the airflow, wherein the flow augmentation arrangement further includes a secondary duct, wherein the secondary duct configured to ingest the boundary layer flow in the airflow from an inlet proximal to a forward portion of the nacelle to an outlet proximal to a rear portion of the nacelle and a tertiary duct between the primary duct and the secondary duct.
-
-
-
-
-
-
-
-
-
搜索结果
344 条记录 (耗时 0.02 秒)
