Patents by Inventor Raymond George Carreker

Raymond George Carreker has filed for patents to protect the following inventions. This listing includes patent applications that are pending as well as patents that have already been granted by the United States Patent and Trademark Office (USPTO).

  • Direct orientation vector rotor
    Patent number: 10183742
    Abstract: A direct orientation vector rotor (DOVER) for use on rotary wing aircraft includes a gear set for multidirectional rotor orientation based on the spherical coordinate system; an inclination mechanism, wherein the rotor is moved from the 0° horizontal position to an inclined position; a rotational turret, wherein the rotor is moved along the azimuth and wherein the inclination mechanism is housed; and a motion-adapted gear lubrication housing.
    Type: Grant
    Filed: October 6, 2015
    Date of Patent: January 22, 2019
    Inventor: Raymond George Carreker
  • MOBILE BASE ANCHORING DEVICE (MOBAD)
    Publication number: 20160318633
    Abstract: A mobile base anchoring device (MOBAD) is activated to infix a component projectile into a substrate as a method to affix the base onto the substrate.
    Type: Application
    Filed: November 5, 2014
    Publication date: November 3, 2016
    Inventor: Raymond George CARREKER
  • DIRECT ORIENTATION VECTOR ROTOR
    Publication number: 20160023756
    Abstract: A direct orientation vector rotor (DOVER) for use on rotary wing aircraft includes a gear set for multidirectional rotor orientation based on the spherical coordinate system; an inclination mechanism, wherein the rotor is moved from the 0° horizontal position to an inclined position; a rotational turret, wherein the rotor is moved along the azimuth and wherein the inclination mechanism is housed; and a motion-adapted gear lubrication housing.
    Type: Application
    Filed: October 6, 2015
    Publication date: January 28, 2016
    Inventor: Raymond George Carreker
  • Direct orientation vector rotor
    Patent number: 9193452
    Abstract: A direct orientation vector rotor (DOVER) for use on rotary wing aircraft includes a gear set for multidirectional rotor orientation based on the spherical coordinate system; an inclination mechanism, wherein the rotor is moved from the 0° horizontal position to an inclined position; a rotational turret, wherein the rotor is moved along the azimuth and wherein the inclination mechanism is housed; and a motion-adapted gear lubrication housing.
    Type: Grant
    Filed: December 14, 2012
    Date of Patent: November 24, 2015
    Inventor: Raymond George Carreker
  • Variable surface landing platform (VARSLAP)
    Patent number: 9174750
    Abstract: In one embodiment, a variable surface landing platform (VARSLAP) includes a base for contacting a landing surface; at least 3 adjustable struts interconnected with the base, wherein each strut is bisected by a strut actuator-housing, and wherein the at least 3 adjustable struts are interconnected to a main body aerospace craft (MAC); a sensor array on the base; and an attitude determination and control system (ADCS).
    Type: Grant
    Filed: February 23, 2015
    Date of Patent: November 3, 2015
    Inventor: Raymond George Carreker
  • VARIABLE SURFACE LANDING PLATFORM (VARSLAP)
    Publication number: 20150166201
    Abstract: In one embodiment, a variable surface landing platform (VARSLAP) includes a base for contacting a landing surface; at least 3 adjustable struts interconnected with the base, wherein each strut is bisected by a strut actuator-housing, and wherein the at least 3 adjustable struts are interconnected to a main body aerospace craft (MAC); a sensor array on the base; and an attitude determination and control system (ADCS).
    Type: Application
    Filed: February 23, 2015
    Publication date: June 18, 2015
    Inventor: Raymond George Carreker
  • Variable surface landing platform (VARSLAP)
    Patent number: 8960600
    Abstract: In one embodiment, a variable surface landing platform (VARSLAP) includes a base for contacting a landing surface; at least 3 adjustable struts interconnected with the base, wherein each strut is bisected by a strut actuator-housing, and wherein the at least 3 adjustable struts are interconnected to a main body aerospace craft (MAC); a sensor array on the base; and an attitude determination and control system (ADCS).
    Type: Grant
    Filed: February 8, 2010
    Date of Patent: February 24, 2015
    Inventor: Raymond George Carreker
  • DIRECT ORIENTATION VECTOR ROTOR
    Publication number: 20140169963
    Abstract: A direct orientation vector rotor (DOVER) for use on rotary wing aircraft includes a gear set for multidirectional rotor orientation based on the spherical coordinate system; an inclination mechanism, wherein the rotor is moved from the 0° horizontal position to an inclined position; a rotational turret, wherein the rotor is moved along the azimuth and wherein the inclination mechanism is housed; and a motion-adapted gear lubrication housing.
    Type: Application
    Filed: December 14, 2012
    Publication date: June 19, 2014
    Inventor: Raymond George Carreker
  • VARIABLE SURFACE LANDING PLATFORM (VARSLAP)
    Publication number: 20120298796
    Abstract: In one embodiment, a variable surface landing platform (VARSLAP) includes a base for contacting a landing surface; at least 3 adjustable struts interconnected with the base, wherein each strut is bisected by a strut actuator-housing, and wherein the at least 3 adjustable struts are interconnected to a main body aerospace craft (MAC); a sensor array on the base; and an attitude determination and control system (ADCS).
    Type: Application
    Filed: February 8, 2010
    Publication date: November 29, 2012
    Inventor: Raymond George Carreker