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GB2601835B - Apparatuses based on jet-effect and thermoelectric effect - Google Patents

Apparatuses based on jet-effect and thermoelectric effect Download PDF

Info

Publication number
GB2601835B
GB2601835B GB2019731.5A GB202019731A GB2601835B GB 2601835 B GB2601835 B GB 2601835B GB 202019731 A GB202019731 A GB 202019731A GB 2601835 B GB2601835 B GB 2601835B
Authority
GB
United Kingdom
Prior art keywords
effect
jet
apparatuses based
thermoelectric
thermoelectric effect
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Fee Related
Application number
GB2019731.5A
Other versions
GB2601835A (en
GB202019731D0 (en
Inventor
Abramov Yuri
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Soliton Holdings Corp
Original Assignee
Soliton Holdings Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Soliton Holdings Corp filed Critical Soliton Holdings Corp
Priority to GB2019731.5A priority Critical patent/GB2601835B/en
Publication of GB202019731D0 publication Critical patent/GB202019731D0/en
Publication of GB2601835A publication Critical patent/GB2601835A/en
Application granted granted Critical
Publication of GB2601835B publication Critical patent/GB2601835B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/025—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for simultaneous blowing and sucking
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/467—Aerodynamic features
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/141—Shape, i.e. outer, aerodynamic form
    • H—ELECTRICITY
    • H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
    • H10N10/00—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects
    • H10N10/10—Thermoelectric devices comprising a junction of dissimilar materials, i.e. devices exhibiting Seebeck or Peltier effects operating with only the Peltier or Seebeck effects
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C2003/143—Aerofoil profile comprising interior channels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2270/00—Control
    • F05D2270/01—Purpose of the control system
    • F05D2270/17—Purpose of the control system to control boundary layer
    • F05D2270/173—Purpose of the control system to control boundary layer by the Coanda effect
    • H—ELECTRICITY
    • H04—ELECTRIC COMMUNICATION TECHNIQUE
    • H04R—LOUDSPEAKERS, MICROPHONES, GRAMOPHONE PICK-UPS OR LIKE ACOUSTIC ELECTROMECHANICAL TRANSDUCERS; DEAF-AID SETS; PUBLIC ADDRESS SYSTEMS
    • H04R23/00—Transducers other than those covered by groups H04R9/00 - H04R21/00
    • H04R23/002—Transducers other than those covered by groups H04R9/00 - H04R21/00 using electrothermic-effect transducer

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Acoustics & Sound (AREA)
  • Signal Processing (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
GB2019731.5A 2020-12-14 2020-12-14 Apparatuses based on jet-effect and thermoelectric effect Expired - Fee Related GB2601835B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2019731.5A GB2601835B (en) 2020-12-14 2020-12-14 Apparatuses based on jet-effect and thermoelectric effect

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2019731.5A GB2601835B (en) 2020-12-14 2020-12-14 Apparatuses based on jet-effect and thermoelectric effect

Publications (3)

Publication Number Publication Date
GB202019731D0 GB202019731D0 (en) 2021-01-27
GB2601835A GB2601835A (en) 2022-06-15
GB2601835B true GB2601835B (en) 2023-01-25

Family

ID=74188931

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2019731.5A Expired - Fee Related GB2601835B (en) 2020-12-14 2020-12-14 Apparatuses based on jet-effect and thermoelectric effect

Country Status (1)

Country Link
GB (1) GB2601835B (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115421426B (en) * 2022-09-27 2023-07-11 兰州交通大学 Mounting arrangement and cooperative control method for high-speed train flank lift force regulating device
GB2625312A (en) * 2022-12-13 2024-06-19 Qinetiq Ltd Thermoacoustic system
CN118900614B (en) * 2024-10-09 2024-12-10 江苏锦立冷链科技有限公司 Semiconductor refrigeration module and preparation method, refrigeration equipment

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5367890A (en) * 1993-07-13 1994-11-29 Marlow Industries, Inc. Integrated thermoelectric system with full/half wave rectifier control
DE19946806A1 (en) * 1999-09-29 2001-04-05 Klaus Palme Generation of electrical energy from thermal energy by the Seebeck effect e.g. for use with a vehicle combustion engine, involves using a Peltier module consisting of a number of Peltier
EP1215936A2 (en) * 2000-12-15 2002-06-19 Pioneer Corporation Speaker
DE102007036930A1 (en) * 2007-08-04 2009-04-09 Mtu Aero Engines Gmbh Gas-turbine engine e.g. civilian aircraft engine or military aircraft engine, has thermoelectric generator generating electrical energy from temperature difference between hot current via core engine and cold current via bypass channel
EP2061098A1 (en) * 2006-09-05 2009-05-20 Pioneer Corporation Thermal sound generating device
US20090151321A1 (en) * 2007-12-13 2009-06-18 Jarmon David C Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle
US20090159110A1 (en) * 2007-12-21 2009-06-25 Kwok David W Thermoelectric generation system
US20120031067A1 (en) * 2010-08-03 2012-02-09 General Electric Company Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine
WO2016062928A1 (en) * 2014-10-21 2016-04-28 Hutchinson Thermoelectric and thermal insulation device for an aircraft engine nacelle, nacelle and method of manufacture of the device
WO2019207578A1 (en) * 2018-04-25 2019-10-31 Technion Research And Development Foundation Limited Spatially global noise cancellation

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5367890A (en) * 1993-07-13 1994-11-29 Marlow Industries, Inc. Integrated thermoelectric system with full/half wave rectifier control
DE19946806A1 (en) * 1999-09-29 2001-04-05 Klaus Palme Generation of electrical energy from thermal energy by the Seebeck effect e.g. for use with a vehicle combustion engine, involves using a Peltier module consisting of a number of Peltier
EP1215936A2 (en) * 2000-12-15 2002-06-19 Pioneer Corporation Speaker
EP2061098A1 (en) * 2006-09-05 2009-05-20 Pioneer Corporation Thermal sound generating device
DE102007036930A1 (en) * 2007-08-04 2009-04-09 Mtu Aero Engines Gmbh Gas-turbine engine e.g. civilian aircraft engine or military aircraft engine, has thermoelectric generator generating electrical energy from temperature difference between hot current via core engine and cold current via bypass channel
US20090151321A1 (en) * 2007-12-13 2009-06-18 Jarmon David C Flowpath heat exchanger for thermal management and power generation within a hypersonic vehicle
US20090159110A1 (en) * 2007-12-21 2009-06-25 Kwok David W Thermoelectric generation system
US20120031067A1 (en) * 2010-08-03 2012-02-09 General Electric Company Turbulated arrangement of thermoelectric elements for utilizing waste heat generated from turbine engine
WO2016062928A1 (en) * 2014-10-21 2016-04-28 Hutchinson Thermoelectric and thermal insulation device for an aircraft engine nacelle, nacelle and method of manufacture of the device
WO2019207578A1 (en) * 2018-04-25 2019-10-31 Technion Research And Development Foundation Limited Spatially global noise cancellation

Also Published As

Publication number Publication date
GB2601835A (en) 2022-06-15
GB202019731D0 (en) 2021-01-27

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20241214