AU5988686A - Impact bar for a comminuting rotor - Google Patents

Impact bar for a comminuting rotor

Info

Publication number
AU5988686A
AU5988686A AU59886/86A AU5988686A AU5988686A AU 5988686 A AU5988686 A AU 5988686A AU 59886/86 A AU59886/86 A AU 59886/86A AU 5988686 A AU5988686 A AU 5988686A AU 5988686 A AU5988686 A AU 5988686A
Authority
AU
Australia
Prior art keywords
impact bar
comminuting rotor
comminuting
rotor
impact
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.)
Granted
Application number
AU59886/86A
Other versions
AU575490B2 (en
Inventor
Hermann Schrodl
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Publication of AU5988686A publication Critical patent/AU5988686A/en
Application granted granted Critical
Publication of AU575490B2 publication Critical patent/AU575490B2/en
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/60—Support structures; Attaching or mounting means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/002—Wall structures
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04—Air inlet arrangements
    • F23R3/06—Arrangement of apertures along the flame tube
    • F23R3/08—Arrangement of apertures along the flame tube between annular flame tube sections, e.g. flame tubes with telescopic sections
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00—Function
    • F05B2260/20—Heat transfer, e.g. cooling
    • F05B2260/202—Heat transfer, e.g. cooling by film cooling
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Gas Burners (AREA)
  • Supercharger (AREA)
  • Valve Device For Special Equipments (AREA)
AU59886/86A 1985-07-17 1986-07-09 Impact bar for a comminuting rotor Ceased AU575490B2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19853535442 DE3535442A1 (en) 1985-10-04 1985-10-04 RING COMBUSTION CHAMBER FOR GAS TURBINE ENGINES
DE3535442 1985-10-04

Publications (2)

Publication Number Publication Date
AU5988686A true AU5988686A (en) 1987-01-22
AU575490B2 AU575490B2 (en) 1988-07-28

Family

ID=6282747

Family Applications (1)

Application Number Title Priority Date Filing Date
AU59886/86A Ceased AU575490B2 (en) 1985-07-17 1986-07-09 Impact bar for a comminuting rotor

Country Status (4)

Country Link
EP (1) EP0219723B1 (en)
JP (1) JPS6287732A (en)
AU (1) AU575490B2 (en)
DE (2) DE3535442A1 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2951496A (en) * 1958-02-11 1960-09-06 Yarnall Waring Co Steam trap
FR2646880A1 (en) * 1989-05-11 1990-11-16 Snecma THERMAL PROTECTION SHIRT FOR POST-COMBUSTION CHANNEL OR TRANSITION OF TURBOREACTOR
FR2708086B1 (en) * 1993-06-30 1995-09-01 Snecma Sectorized tubular structure working on implosion.
FR2710968B1 (en) * 1993-10-06 1995-11-03 Snecma Double wall combustion chamber.
US11867402B2 (en) 2021-03-19 2024-01-09 Rtx Corporation CMC stepped combustor liner
CN113154453B (en) * 2021-05-06 2022-07-08 中国航发湖南动力机械研究所 Tangential tilting type annular membrane diverging and cooling structure
CN115507391B (en) * 2022-09-16 2023-10-20 中国航发湖南动力机械研究所 Ceramic-based flame tube

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH255541A (en) * 1947-05-12 1948-06-30 Bbc Brown Boveri & Cie Cooled metal combustion chamber for generating heating and propellant gases.
US2544538A (en) * 1948-12-01 1951-03-06 Wright Aeronautical Corp Liner for hot gas chambers
GB715910A (en) * 1952-02-01 1954-09-22 Rolls Royce Improvements in or relating to combustion equipment of gas-turbine engines
US2747803A (en) * 1952-07-09 1956-05-29 Pettibone Mulliken Corp Hammer rotor for hammermills
CH428324A (en) * 1964-05-21 1967-01-15 Prvni Brnenska Strojirna Combustion chamber
AT289522B (en) * 1968-03-14 1971-04-26 Franz Wageneder Impact mill
US4480436A (en) * 1972-12-19 1984-11-06 General Electric Company Combustion chamber construction
US4236378A (en) * 1978-03-01 1980-12-02 General Electric Company Sectoral combustor for burning low-BTU fuel gas
US4414816A (en) * 1980-04-02 1983-11-15 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Combustor liner construction
US4302941A (en) * 1980-04-02 1981-12-01 United Technologies Corporation Combuster liner construction for gas turbine engine
US4373678A (en) * 1980-06-30 1983-02-15 Reitter Guenther W Rotary impact crusher having a continuous rotary circumference

Also Published As

Publication number Publication date
DE3661863D1 (en) 1989-02-23
DE3535442C2 (en) 1987-10-22
AU575490B2 (en) 1988-07-28
JPH0378535B2 (en) 1991-12-16
EP0219723B1 (en) 1989-01-18
JPS6287732A (en) 1987-04-22
DE3535442A1 (en) 1987-04-09
EP0219723A1 (en) 1987-04-29

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