Description
Category: Technology Licenses
Created On: 2022-04-28
Record Count: 7
Primary Industries
- Transportation
- Engines
- Machinery
- Automotive
- Scientific & Technical Instruments
- Tool
- Energy Resources & Svcs
IPSCIO Report Record List
Below you will find the records curated into this collection. This summary includes the complete licensed property description so that you can review and determine if this collection covers the topics, technology or transaction type that is relevant for your needs. The full report will include all relevant deal data such as the royalty base, agreement date, term description, royalty rates and other deal terms. For reference, here is a sample of a full IPSCIO curated royalty rate report: Sample Report
IPSCIO Record ID: 1784
The Orbital Vane Compressor technology is based on a circular, non-contact sealing rotary mechanism with an integral lubricant management system and can be sized and configured to operate over a wide range of capacities and applications. These compressors are initially intended to supply air to fuel cells and to circulate hydrogen fuel through them.
IPSCIO Record ID: 26521
'Rand Cam TM Diesel Engine Technology' means a positive displacement, compression ignition, machine, which consists of a rotor with multiple axial vanes forming combustion chambers as a rotor and vanes rotate in a cam shaped housing. This cam housing is referred to as a stator, which contains a toroidal trough of varying depth machined into each stator.
'Rand Cam TM Compressor Technology' means a positive displacement machine whose purpose is to compress a compressible fluid such as air from a lower pressure to a higher pressure, which consists of a rotor with multiple axial vanes forming compression chambers as a rotor and vanes rotate in a cam shaped housing. This cam housing is referred to as a stator, which contains a toroidal trough of varying depth machined into each stator.
'Rand Cam TM' Expander Technology' means a positive displacement machine whose purpose is to expand a compressible fluid such as air from a higher pressure to a lower pressure thus generating positive power, which consists of a rotor with multiple axial vanes forming expansion chambers as a rotor and vanes rotate in a cam shaped housing. This cam housing is referred to as a stator, which contains a toroidal trough of varying depth machined into each stator.
'Rand Cam TM Cold Turbine Technology' means a Brayton Cycle (Gas Turbine Cycle) machine consisting of one or more 'Rand Cam TM Compressors' used as compressors in the Brayton Cycle and one or more 'Rand Cam TM Expanders' used as the expanders (turbines) in the Brayton Cycle machine.
'Radian Products' means equipment utilizing the various Rand CAMTM Technologies along with other technologies which Radian will use to design, manufacture and market UAV engines of over 10 horsepower maximum engine power utilizing 'Rand CAMTM Direct Charge Engine Technology' engines, 'Rand CAMTM Diesel Engine Technology' engines and 'Rand CAMTM Cold Turbine Technology' engines. Engines produced by Radian will be used exclusively for UAV equipment produced by Radian and replacement engines and parts for said equipment. 'The Technology' shall mean the Rand CAMTM', Direct Charge Engine Technology, Rand CAMTM Diesel Engine Technology, Rand CAMTM Compressor Technology, Rand CAMTM Expander Technology and Rand CAMTM Cold Turbine Technology as embodied in know-how, formulae, processes, designs, sketches, photographs, plans, drawings, specifications samples, models, reports, studies, findings, invention and ideas and other means of conveying information whether any of the foregoing is adapted to use in manufacture or not.
IPSCIO Record ID: 27717
Licensor hereby grants Licensee the non-exclusive right to use the registered trademark Dynacharger(TM). Licensee has no obligation to use this trademark on its motor assisted turbochargers.
The patents hereby licensed on a non-exclusive basis are all the patents issued or to be issued and effective in the Territories during the term of this License Agreement and corresponding to the following U.S. patents.
a. U.S. Patent No. 5,560,208 Issued 10/01/96
Motor Assisted Variable Geometry Turbocharging System
b. U.S. Patent No. 5,870,894 Issued 02/16/99
Motor Assisted Supercharging Devices For Internal Combustion Engines
c. U.S. Patent No. 5,605,045 Issued 02/25/97
Turbocharging System With Integral Assisting Electric Motor And Cooling System Therefore
d. U.S. Patent No. 5,025,629 Issued 06/25/91
High Pressure Ratio Turbocharger
e. U.S. Patent No. 5,094,587 Issued 03/10/99
'Turbine For Internal Combustion Engine Turbochargers'
f. U.S. Patent No. 5,906,098 Issued 05/25/99
Motor Generator Assisted Turbocharging System For Use With Internal
Combustion Engines, And Control Method Therefore
g. U.S. Patent No. 4,565,505 Issued 01/21/86
Combination Flow Turbine For Internal Combustion Engine
Turbochargers
h. U.S. Patent No. 5,857,332 Issued 01/12/99
Bearing System For Motor Assisted Turbochargers For Internal
Combustion Engines
IPSCIO Record ID: 240592
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manufacture the Licensee Manufactured Components;
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source the Licensee Sourced Components and the Optionally Sourced Components; and
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sell the Licensee Manufactured Components, Licensee Sourced Components and Optionally Sourced Components;
Licensor grants the manufacturing rights that are owned and available from Licensor or transferred from SYNERJECT to Licensor, for the Licensor Direct Fuel Injection System components (Licensee Manufactured Components).
During the Royalty Payment Period, Licensee agree not to grant to another supplier the right to sell the Licensor Direct Fuel Injection System to the Licensed Customers for use in Licensed Vehicles in the Licensed Sales Territory.
Licensee Manufactured Components shall mean Licensor Direct Fuel Injection System components identified
Air compressor; Piston fuel pump; Throttle body assembly (excluding the Throttle Position Sensor); Fuel rail assembly ( excluding the fuel injector and fuel .pressure
regulator); ECU Hardware, and ECU Software.
UCAL Sourced Components identified
ECU Hardware, Software, Direct Injector; Fuel Injector; Fuel pressure regulator (SYNERJECT type).
Optionally Sourced Components identified
Ignition coil; Engine temperature sensor; throttle Position Sensor; Oil pump.
Licensed Vehicle shall mean 2 and 3 wheeler motor vehicles incorporating a 2 stroke OCP technology engine and tested on the Indian Drive Cycle, but does not include 4 wheeled passenger car vehicles.
Licensor Direct Fuel Injection System shall mean the current Licensor air assisted direct fuel injection system components and including any Licensee improvements thereof.
IPSCIO Record ID: 27214
Electronic Control Module – electronic device used in the fuel injection system that coordinates the proper mixture of fuel and air; enhance the performance of fuel injection systems.
IPSCIO Record ID: 27404
'CSRV Valve Seal' shall mean a valve seal for use with a CSRV Rotary Valve Sphere (as hereinafter defined) in the Coates Spherical Rotary Valve System.
'CSRV Rotary Valve Sphere' shall mean a spherical rotary valve used in the CSRV Valve System in accordance with the Technical Specifications.
'CSRV Components' shall mean the parts that when assembled comprise the Licensed Product.
'Coates Co-Generation System' shall mean a device consisting of an Engine linked to a Coates Generator.
'Engine' or 'Engines' shall mean all Coates internal combustion engine(s) employing the Coates Spherical Rotary Valve System.
'Generator' shall mean a Coates patented device, which produces electricity having an Engine as its power source.
'Licensed Product' shall mean the Coates Co-Generation System incorporating the Engines, the Generators, Patent Rights and/or Technical Information in its design and manufacture incorporating the components.
US Patent No. Date Application Filed
4,989,579 (Mark I) July 26,1982 February 5,1991
4,953,527 Mark II) November 14,1998 September 4,1990
4,989,558 September 14,1998 February 5, 1991
4,944,261(Mark IIB) October 16,1989 July 31,1990
4,976,232 December 6,1989 December 11,1990
5,109,814 May 10,1991 May 5,1992
5,361,739(Mark III) May 12,1993 November 8,1994.
IPSCIO Record ID: 1305