Category:Paul R. Hanrahan of Sedona AZ (US)
Paul R. Hanrahan of Sedona AZ (US)
Executive Summary
Paul R. Hanrahan of Sedona AZ (US) is an inventor who has filed 1 patents. Their primary areas of innovation include GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines (1 patents), Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se (1 patents), NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids (1 patents), and they have worked with companies such as Raytheon Technologies Corporation (1 patents). Their most frequent collaborators include .
Patent Filing Activity
Technology Areas
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List of Technology Areas
- F02C7/06 (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines): 1 patents
- F01D25/16 (Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se): 1 patents
- F01D25/22 (NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids): 1 patents
- F01D25/162 ({Bearing supports}): 1 patents
- F02C3/04 (GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines): 1 patents
- F05D2240/50 (No explanation available): 1 patents
- F16C17/024 (SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS): 1 patents
- F16C2360/23 (SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS): 1 patents
Companies
List of Companies
- Raytheon Technologies Corporation: 1 patents
Collaborators
Subcategories
This category has only the following subcategory.
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Pages in category "Paul R. Hanrahan of Sedona AZ (US)"
The following 7 pages are in this category, out of 7 total.
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- US Patent Application 18202709. THRUST VECTORING EXHAUST NOZZLE FOR AIRCRAFT PROPULSION SYSTEM simplified abstract
- US Patent Application 18202727. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract
- US Patent Application 18202731. AIRCRAFT PROPULSION SYSTEM WITH VARIABLE SPEED ROTATING STRUCTURE simplified abstract
- US Patent Application 18202733. AIRCRAFT PROPULSION SYSTEM WITH ADJUSTABLE THRUST PROPULSOR simplified abstract
- US Patent Application 18202734. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract
- US Patent Application 18202736. SELECTIVE POWER DISTRIBUTION FOR AN AIRCRAFT PROPULSION SYSTEM simplified abstract