CH331332A - Afterburner on an aircraft jet engine - Google Patents

Afterburner on an aircraft jet engine

Info

Publication number: CH331332A
Authority: CH; Switzerland
Prior art keywords: afterburner; jet engine; aircraft jet; aircraft; engine
Prior art date: 1954-02-23

Application number

Other languages

German (de)

Inventor

Albert Benson John

Wallace Crosby Gilbert

Original Assignee

Gen Electric

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.)

1954-02-23

Filing date

1955-03-17

Publication date

1958-07-15

1954-03-18 Priority claimed from US417192A external-priority patent/US2874536A/en

1955-03-17 Application filed by Gen Electric filed Critical Gen Electric

1958-07-15 Publication of CH331332A publication Critical patent/CH331332A/en

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
- F23R3/002—Wall structures
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/78—Other construction of jet pipes
- F02K1/82—Jet pipe walls, e.g. liners
- F02K1/822—Heat insulating structures or liners, cooling arrangements, e.g. post combustion liners; Infrared radiation suppressors
- 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)
Gas Burners (AREA)
Exhaust Silencers (AREA)
Spray-Type Burners (AREA)
Turbine Rotor Nozzle Sealing (AREA)

CH331332D 1954-02-23 1955-03-17 Afterburner on an aircraft jet engine CH331332A (en)

Applications Claiming Priority (2)

Application Number	Priority Date	Filing Date	Title
US803813XA	1954-02-23	1954-02-23
US417192A US2874536A (en)	1954-03-18	1954-03-18	Cooling means for tailpipe

Publications (1)

Publication Number	Publication Date
CH331332A true CH331332A (en)	1958-07-15

Family

ID=26763440

Family Applications (2)

Application Number	Title	Priority Date	Filing Date
CH335303D CH335303A (en)	1954-02-23	1955-02-22	Afterburner for aircraft jet engines
CH331332D CH331332A (en)	1954-02-23	1955-03-17	Afterburner on an aircraft jet engine

Family Applications Before (1)

Application Number	Title	Priority Date	Filing Date
CH335303D CH335303A (en)	1954-02-23	1955-02-22	Afterburner for aircraft jet engines

Country Status (4)

Country	Link
BE (1)	BE535906A (en)
CH (2)	CH335303A (en)
DE (2)	DE1021208B (en)
GB (2)	GB803813A (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3085401A (en) *	1959-01-22	1963-04-16	Rolls Royce	Reheat combustion equipment of gas-turbine engines
DE1221053B (en) *	1960-06-11	1966-07-14	Rolls Royce	Turbine jet engine
DE1210628B (en) *	1962-02-08	1966-02-10	Rolls Royce	Jet pipe for recoil engines, for example for the gas turbine jet engine of an aircraft
GB1102572A (en) *	1964-06-06	1968-02-07	Bristol Siddeley Engines Ltd	Jet propulsion engines
US3307354A (en) *	1965-10-01	1967-03-07	Gen Electric	Cooling structure for overlapped panels
GB1157930A (en) *	1966-12-28	1969-07-09	Rolls Royce	Gas Turbine Jet Propulsion Engine
US4833881A (en) *	1984-12-17	1989-05-30	General Electric Company	Gas turbine engine augmentor
US20060137352A1 (en) *	2004-12-29	2006-06-29	United Technologies Corporation	Augmentor liner

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
CH214477A (en) *	1939-01-30	1941-04-30	Bbc Brown Boveri & Cie	Cooling device on pipes, containers, housings or the like through which hot gases flow or which include them.
US2458497A (en) *	1945-05-05	1949-01-11	Babcock & Wilcox Co	Combustion chamber
FR962862A (en) *	1946-10-26	1950-06-22
CH255541A (en) *	1947-05-12	1948-06-30	Bbc Brown Boveri & Cie	Cooled metal combustion chamber for generating heating and propellant gases.
NL72931C (en) *	1948-02-21
US2508420A (en) *	1948-09-21	1950-05-23	Westinghouse Electric Corp	Combustion apparatus
US2547619A (en) *	1948-11-27	1951-04-03	Gen Electric	Combustor with sectional housing and liner
US2632299A (en) *	1949-06-17	1953-03-24	United Aircraft Corp	Precombustion chamber
DE825777C (en) *	1949-08-19	1951-12-20	Canadian Patents Dev	Flame tube of combustion chambers, especially for gas turbines
GB700004A (en) *	1949-12-12	1953-11-25	Babcock & Wilcox Ltd	Improvements in or relating to combustion apparatus
DE889240C (en) *	1950-10-17	1953-09-10	Canadian Patents Dev	Flame tube of combustion chambers, especially for gas turbine engines
US2651912A (en) *	1950-10-31	1953-09-15	Gen Electric	Combustor and cooling means therefor
FR1002312A (en) *	1951-04-01	1952-03-05		Combustion chamber for thermo-propellants, turbo-engines or the like

0
- BE BE535906D patent/BE535906A/xx unknown
1955
- 1955-02-21 DE DEG16538A patent/DE1021208B/en active Pending
- 1955-02-21 DE DEG16537A patent/DE1045180B/en active Pending
- 1955-02-22 CH CH335303D patent/CH335303A/en unknown
- 1955-02-23 GB GB5476/55A patent/GB803813A/en not_active Expired
- 1955-02-23 GB GB5477/55A patent/GB802370A/en not_active Expired
- 1955-03-17 CH CH331332D patent/CH331332A/en unknown

Also Published As

Publication number	Publication date
GB802370A (en)	1958-10-01
CH335303A (en)	1958-12-31
DE1045180B (en)	1958-11-27
DE1021208B (en)	1957-12-19
BE535906A (en)
GB803813A (en)	1958-11-05

Publication	Publication Date	Title
CH327869A (en)	1958-02-15	Thrust nozzle device for jet engines
CH372877A (en)	1963-10-31	Thrust nozzle for jet engine
CH320188A (en)	1957-03-15	Recoil engine in an airplane
FR1204592A (en)	1960-01-27	Rocket engine
FR1194723A (en)	1959-11-12	Rocket engine
CH388029A (en)	1965-02-15	Jet deflection device for aircraft engines
CH319835A (en)	1957-02-28	Airplane with gas turbine engine
CH331332A (en)	1958-07-15	Afterburner on an aircraft jet engine
CH326061A (en)	1957-11-30	Propulsion device on an aircraft
CH313234A (en)	1956-03-31	Thrust nozzle device on jet engine
FR1128730A (en)	1957-01-09	Rocket engine
FR1073268A (en)	1954-09-21	Aircraft
FR1112264A (en)	1956-03-12	Aircraft upgrades
CH365910A (en)	1962-11-30	Afterburner on a jet engine
CH320884A (en)	1957-04-15	Rocket with propulsion charge
AT199777B (en)	1958-09-25	Aircraft turbo-engine fuel mixture
CH331882A (en)	1958-08-15	Launching device for rocket projectiles on aircraft
FR1118469A (en)	1956-06-06	Advanced parachute
CA501071A (en)	1954-03-30	Turbo jet engines
FR1115450A (en)	1956-04-24	Airplane type flight apparatus
FR1107418A (en)	1955-12-30	Jet engines
FR1117806A (en)	1956-05-28	Advanced aircraft
FR1108903A (en)	1956-01-19	Aircraft upgrades
CA508618A (en)	1954-12-28	Operation of jet engines
FR1099386A (en)	1955-09-05	Aircraft fairing device