Inventor
Daniel N. Miller
Inventor
Bainbridge Island, WA, US
Overview
Patents· 42 as inventor
Public. Assignee & technology derived from the patent record. Each patent links to its LexDana page.
Y02Tprimary
Y02TClimate change mitigation technologies related to transportation19%
B64CAeroplanes16%
F02KJet-propulsion plants9%
F05DIndexing scheme for aspects relating to non-positive-displacement machines or engines, gas-turbines or jet-propulsion plants7%
F15DFluid dynamics, i.e. methods or means for influencing the flow of gases or liquids6%
F02CGas-turbine plants5%
A61BDiagnosis4%
B64DEquipment for fitting in or to aircraft4%
F01DNon-positive displacement machines or engines, e.g. steam turbines4%
B25JManipulators3%
PatentTitleYear
10,794,329Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices202010,752,340Adhesive panels of microvane arrays for reducing effects of wingtip vortices202010,449,008System and method for breakaway clutching in an articulated arm201910,421,533Panels comprising uneven edge patterns for reducing boundary layer separation201910,410,502Method and apparatus for providing environmental management using smart alarms201910,405,944Medical device with active brake release control201910,272,569System and method for instrument disturbance compensation201910,226,306System and method for integrated surgical table201910,054,048Suprression of shock-induced airflow separation201810,034,717System and method for breakaway clutching in an articulated arm20189,995,181Exhaust impingement cooling20189,896,192'Minimally intrusive wingtip vortex wake mitigation using microvane arrays'20189,898,917'Method and apparatus for providing environmental management using smart alarms'20189,875,081Device selection for providing a response20189,868,516'Adhesive panels of microvane arrays for reducing effects of wingtip vortices'20189,551,297'Jet exhaust noise reduction'20179,541,030'Exhaust plume cooling using periodic interruption of exhaust gas flow to form ambient air entraining vortices'20179,512,821'Active bleed for airfoils'20169,261,047'Jet exhaust noise reduction'20168,960,609'Minimally intrusive wingtip vortex wake mitigation using inside-mold-line surface modifications'20158,408,281'System, method, and apparatus for pulsed-jet-enhanced heat exchanger'20138,403,271'Passive robust flow control micro device'20138,402,738'Flow control redistribution to mitigate high cycle fatigue'20138,353,482'System for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation'20138,316,631'Exhaust plume heat effect reducing method and apparatus'20128,240,616'Method and system for global flow field management using distributed, surface-embedded, nano-scale boundary layer actuation'20128,242,404'Systems and methods for plasma jets'20128,210,482'Prismatic-shaped vortex generators'20128,065,868'System, method, and apparatus for control input prediction and state verification of fluidic vectoring exhaust in high performance aircraft'20118,038,102'System and method to control flowfield vortices with micro-jet arrays'20117,874,525'Method and system for fully fixed vehicle control surfaces'20117,686,256'Conformal aero-adaptive nozzle/aftbody'20107,617,670'Flow control redistribution to mitigate high cycle fatigue'20097,510,149'System and method to control flowfield vortices with micro-jet arrays'20097,183,515'Systems and methods for plasma jets'20076,962,044'Method and apparatus of asymmetric injection into subsonic flow of a high aspect ratio/complex geometry nozzle'20056,758,032'System of pulsed detonation injection for fluid flow control of inlets, nozzles, and lift fans'20046,682,021'System and method for actively manipulating and controlling fluid flow over a surface'20046,371,414'System and method for manipulating and controlling fluid flow over a surface'20026,308,740'Method and system of pulsed or unsteady ejector'20016,112,513'Method and apparatus of asymmetric injection at the subsonic portion of a nozzle flow'20006,112,512'Method and apparatus of pulsed injection for improved nozzle flow control'2000Career & activity timeline
Assembled from patent assignee/location history and declaration credentials.
2000–2020Patents assigned to LOCKHEED CORP (32)· patent assignee history
2000–2004Based in Fort Worth, TX, US· patent location history
2004–2020Based in Bainbridge Island, WA, US· patent location history
2011–2018Patents assigned to MILLER DANIEL N (14)· patent assignee history
2012–2018Patents assigned to DOMEL NEAL D (5)· patent assignee history
2012–2018Patents assigned to BARUZZINI DAN J (3)· patent assignee history
2018–2019Patents assigned to INTUITIVE SURGICAL OPERATIONS (5)· patent assignee history
2018Based in Sunnyvale, CA, US· patent location history
2018Based in El Cerrito, CA, US· patent location history
2019Based in Fremont, CA, US· patent location history
Inventor activity
Assignee and location history derived from the patent record.
Assignees
| Assignee | Patents | Span |
|---|---|---|
| LOCKHEED CORP | 32 | 2000–2020 |
| MILLER DANIEL Nself | 14 | 2011–2018 |
| DOMEL NEAL D | 5 | 2012–2018 |
| INTUITIVE SURGICAL OPERATIONS | 5 | 2018–2019 |
| BARUZZINI DAN J | 3 | 2012–2018 |
Locations
| Location | Patents | Span |
|---|---|---|
| Bainbridge Island, Washington, US | 28 | 2004–2020 |
| Fremont, California, US | 5 | 2019 |
| Fort Worth, Texas, US | 5 | 2000–2004 |
| Sunnyvale, California, US | 2 | 2018 |
| El Cerrito, California, US | 1 | 2018 |