ClassID:

72231

B64C39/066 - CPC Classification

Classification description:

Aircraft not otherwise provided for having disc- or ring-shaped wings having channel wings

Recent Application in this class:
#1
20260116538
2026-04-30

Adaptive Vertical Take-Off and Landing Propulsion System

#2
20250145286
2025-05-08

CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

#3
20240199205
2024-06-20

ADAPTIVE VERTICAL TAKE-OFF AND LANDING PROPULSION SYSTEM

#4
20240182167
2024-06-06

CONFIGURATION FOR VERTICAL TAKE-OFF AND LANDING SYSTEM FOR AERIAL VEHICLES

#5
20240067368
2024-02-29

Hybrid inflatable aircraft of the unmanned type

#6
20230022007
2023-01-26

Air mobility device using compressed air

#7
20220111957
2022-04-14

Configuration for vertical take-off and landing system for aerial vehicles

#8
20210086897
2021-03-25

Retractable duct channel wing

#9
20200324891
2020-10-15

ADAPTIVE VERTICAL TAKE-OFF AND LANDING PROPULSION SYSTEM

#10
20190193839
2019-06-27

Aircraft with a weight element controlling the center of gravity thereof

#11
20180370627
2018-12-27

Configuration for vertical take-off and landing system for aerial vehicles

#12
20180305007
2018-10-25

Configuration for vertical take-off and landing system for aerial vehicles

#13
20180086447
2018-03-29

Aircraft having independently variable incidence channel wings with independently variable incidence channel canards

#14
20170370227
2017-12-28

Lifting foil

#15
20160318606
2016-11-03

Extremely quiet short take-off and landing (STOL) aircraft

#16
20160121995
2016-05-05

Aircraft and convertible wing assembly

#17
20160009376
2016-01-14

Semi-open fluid jet VTOL aircraft

#18
20150232180
2015-08-20

Dual channel wing for an aerocar

#19
20140227098
2014-08-14

Lifting Foil

#20
20120156037
2012-06-21

Foil, utilized such as an airfoil or hydrofoil, characterized by a duct moving relative to a mass of fluid. A constriction within the duct increases the speed of the fluid flowing within the duct and thereby produces a pressure drop inducing a mass of fluid external to the duct to accelerate into the duct. The acceleration of the fluid into the duct generates a resultant force, which can be varied and controlled to improve performance and reduce drag

#21
20110108675
2011-05-12

Wing and a multiple propeller aircraft

#22
20110000802
2011-01-06

TACTILE PACKAGING FOR CONSUMER GOODS

#23
20100140389
2010-06-10

AIR VEHICLE

#24
20090261207
2009-10-22

Stable aircraft

#25
20070164147
2007-07-19

Aircraft internal wing and design

#26
20060202083
2006-09-14

VTOL personal aircraft

#27
20060091263
2006-05-04

Lifting foil

#28
20050173592
2005-08-11

Lifting foil

#29
20050029396
2005-02-10

Channel-wing system for thrust deflection and force/moment generation

#30
15342244
2017-07-25

Semi-open fluid jet VTOL aircraft