Propeller Type Patents (Class 180/7.4)
  • Patent number: 11845548
    Abstract: A jet powered personal flying machine composed of a customizable framework consisting of separate bolt-on parts or sections that can be swapped out or switched, including a base frame containing a plurality of mini jet engines, a shell or fuselage, a fuel tank, a flight computer, a plurality of electronic buttons and controls, a parachute, footstands on both sides for the user to place their feet and a single control stick consisting of a metal or carbon fiber tube attached at the front and center of the base, and protruding upwards and slightly forward from the base frame, of which contains electronic buttons and controls for the user to use in flying the machine.
    Type: Grant
    Filed: June 29, 2021
    Date of Patent: December 19, 2023
    Inventor: Nazareno Cruzada
  • Patent number: 11827350
    Abstract: A flying robot executing predetermined work, the flying robot comprising: a body unit; and a propulsion portion comprising a plurality of propulsion units configured to cause propulsion to occur by driving rotor blades, the plurality of propulsion units being provided on the body unit; the flying robot further comprising: a contact support unit configured to contact a predetermined contact surface to be capable of supporting at least a part of the body unit; a sensor configured to detect an inclination of the body unit; and a control unit configured to, when the contact support unit contacts the predetermined contact surface, and the predetermined work is being performed, execute posture control to drive at least one of the plurality of propulsion units based on the inclination of the body unit detected by the sensor so that the inclination of the body unit is kept within a predetermined angle range.
    Type: Grant
    Filed: March 5, 2019
    Date of Patent: November 28, 2023
    Assignee: THK CO., LTD.
    Inventor: Kaoru Hoshide
  • Patent number: 11760478
    Abstract: A flying robot comprising: a flying body unit; a propulsion portion comprising a plurality of propulsion units configured to cause propulsion to occur by driving rotor blades, the plurality of propulsion units being provided on the flying body unit; a working body unit; a manipulator unit configured to be capable of executing predetermined work and comprising one or more work manipulators provided on the working body unit; and connection units provided on the working body unit and the flying body unit so as to enable the flying body unit to be connected with and disconnected from the working body unit; wherein the flying robot executes the predetermined work by the work manipulators in a state in which the working body unit and the flying body unit are connected at the connection units. The flying robot is caused to execute a wide range of content of work as far as possible.
    Type: Grant
    Filed: March 5, 2019
    Date of Patent: September 19, 2023
    Assignee: THK CO., LTD.
    Inventor: Kaoru Hoshide
  • Patent number: 11535073
    Abstract: An air and land multimodal vehicle comprises a frame, a propeller engine attached to a first location of the frame supplying power and torque to a propeller, a ground engine attached to a second location of the frame supplying power and torque to one or more ground traction elements, and a flexible wing releasably connectable to the frame, wherein the propeller engine is vertically and horizontally spaced from the ground engine.
    Type: Grant
    Filed: February 5, 2018
    Date of Patent: December 27, 2022
    Assignee: SkyRunner, LLC
    Inventor: Stewart Hamel
  • Patent number: 11524780
    Abstract: A fan powered folding wing bicycle apparatus for novelty and transportation includes a frame and a rear wheel coupled between a pair of lower horizontal tubes. A stem is pivotably coupled within a head tube. A handle bar is coupled to the stem. A pair of forks is coupled to the stem and a front wheel is coupled to the pair of forks. A pair of engine straps is coupled between a pair of top horizontal tubes. A duct is coupled to the pair of engine straps and a turbine is coupled within the duct. A seat is coupled to the duct. A battery is in operational communication with the turbine. A pair of wings is pivotably coupled to the pair of top horizontal tubes.
    Type: Grant
    Filed: January 7, 2021
    Date of Patent: December 13, 2022
    Inventor: Faruk Hossain
  • Patent number: 11485451
    Abstract: A jet-powered sled has a body having a control cockpit with control apparatus for an operator to control the jet sled, a set of surface runners adapted to engage a surface upon which the sled is operated, the surface runners removably engaged to spindles coupled to swing arms coupled to the jet sled, and an engine compartment having a jet engine removably mounted in a manner to direct thrust to a rear of the jet sled to propel the jet sled. The jet sled is characterized in that the sled may be adapted specifically to run on water, ice or snow by installing runners adapted for water, ice or snow on the spindles of the swing arms.
    Type: Grant
    Filed: September 20, 2021
    Date of Patent: November 1, 2022
    Assignee: JETTS, LLC
    Inventor: Eric Oliver
  • Patent number: 11008053
    Abstract: An aerodynamic component disposed on a side face of an upper rear part of an automobile vehicle body and reduces a lift coefficient of a vehicle body rear part, includes a plate-shaped base part and a fin projectingly provided on a front face of the base part, wherein the base part gently increases in thickness from a front edge side to a rear edge side, and has at the rear edge a shape that rises steeply with respect to the side face of the upper rear part of the vehicle body.
    Type: Grant
    Filed: November 27, 2017
    Date of Patent: May 18, 2021
    Assignee: HONDA ACCESS CORP.
    Inventors: Ryo Shiogai, Takashi Yuzawa, Seiko Fukuda
  • Patent number: 9364766
    Abstract: A propulsion system for a vehicle or toy vehicle is disclosed. The system comprises rotary drive means for driving the vehicle along ground, the rotary drive means operating in a plane and having a peripheral ground-engagement part. The system further comprises a rotor comprising one or more rotor blades rotatable about a rotor axis for producing thrust, wherein the rotary drive means and the rotor are positioned relative to each other so that during rotation of the rotor, the rotor blades pass through the plane of the rotary drive means, inside the peripheral ground-engagement part. In this way, the rotor blades are protected by the peripheral ground-engagement part.
    Type: Grant
    Filed: June 7, 2013
    Date of Patent: June 14, 2016
    Inventor: Witold Mielniczek
  • Patent number: 7546190
    Abstract: A method for compensating a steering system exhibiting dead-zone characteristics estimates the dead-zone parameters of the steering system and establishes a dead-zone inverse function utilizing the estimated parameters. The dead-zone inverse is utilized to transform steering orders in the dead-zone. Parameters of the dead-zone inverse are continuously up-dated with the utilization of the transformed steering order, the existing dead-zone parameters, and the present heading.
    Type: Grant
    Filed: August 31, 2005
    Date of Patent: June 9, 2009
    Assignee: Northrop Grumman Systems Corp.
    Inventor: Jason O. Burkholder
  • Patent number: 7267530
    Abstract: A windmill apparatus has multiple pairs of blades to enhance power output and lift performance. The apparatus has multiple double acting piston/cylinders actuated by the windmill, which includes several clutches that are used to engage and disengage the windmill from the motor.
    Type: Grant
    Filed: February 21, 2004
    Date of Patent: September 11, 2007
    Inventor: Francis J. McCabe
  • Publication number: 20020060267
    Abstract: A remotely-controlled unmanned mobile device (UMD) adapted to function as a robot scout to enter and reconnoiter the site of a disaster and to communicate to a rescue mission information regarding conditions prevailing at the site, making it possible for the mission to decide on rescue measures appropriate to these conditions. The UMD is operable in either of two modes. In its air-mobility mode the UMD is able to vertically take off and land, to fly to the site and then hover thereover. In its ground-mobility mode, the UMD can walk on legs over difficult terrain and through wrecked structures and ruins. The UMD is provided with condition-sensitive sensors for gathering data regarding conditions prevailing at the site, and position-sensitive sensors for avoiding obstacles in the path of the walking UMD, thereby assuring safe mobility. Other sensors govern geo-referenced navigation and flight control functions.
    Type: Application
    Filed: September 25, 2001
    Publication date: May 23, 2002
    Inventor: Arie Yavnai