GB587512A - Improvements relating to exhaust systems of jet propulsion installations in aircraft - Google Patents
Improvements relating to exhaust systems of jet propulsion installations in aircraftInfo
- Publication number
- GB587512A GB587512A GB6525/42A GB652542A GB587512A GB 587512 A GB587512 A GB 587512A GB 6525/42 A GB6525/42 A GB 6525/42A GB 652542 A GB652542 A GB 652542A GB 587512 A GB587512 A GB 587512A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pipe
- aircraft
- jet
- exhaust pipe
- jet propulsion
- 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
Links
Classifications
-
- 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
- F02K1/80—Couplings or connections
-
- 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)
- Jet Pumps And Other Pumps (AREA)
Abstract
587,512. Jet propulsion of aircraft. WHITTLE, F. May 13, 1942, No. 6525. [Class 110 (iii)] The exhaust pipe of a power unit is connected to the propulsion jet pipe so as to leave a gap through which air may flow into the pipe. In the form shown, the exhaust pipe 1 has a short cylindrical extension 5, secured to it by bolted flanges 6, 7 which enters a sleeve 4 having a packing ring 3 free to slide on the jet pipe 2. The sleeve is adjustably secured to the exhaust pipe by eyed ends of the flange bolts 9. The power unit is anchored at its upstream end and the jet pipe at its down-stream end and the connection shown permits relative movement due to thermal expansion. Ribs or dimples may be formed on one of the parts 4, 5 to keep them concentric.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6525/42A GB587512A (en) | 1942-05-13 | 1942-05-13 | Improvements relating to exhaust systems of jet propulsion installations in aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB6525/42A GB587512A (en) | 1942-05-13 | 1942-05-13 | Improvements relating to exhaust systems of jet propulsion installations in aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB587512A true GB587512A (en) | 1947-04-29 |
Family
ID=9816091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB6525/42A Expired GB587512A (en) | 1942-05-13 | 1942-05-13 | Improvements relating to exhaust systems of jet propulsion installations in aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB587512A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2722801A (en) * | 1949-05-24 | 1955-11-08 | Rolls Royce | Exhaust ducting arrangements for gas-turbine engines |
US3756629A (en) * | 1971-10-01 | 1973-09-04 | Victaulic Co Of America | Stud system of joining pipe and couplings for same |
EP0080404A1 (en) * | 1981-11-19 | 1983-06-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Assembly of two joined rotationally symmetrical objects made of materials with differing co-efficients of dilatation |
GB2259954A (en) * | 1991-09-27 | 1993-03-31 | Short Brothers Plc | Ducted fan turbine engine nozzle assembly |
US5395505A (en) * | 1991-10-31 | 1995-03-07 | Monitoring Technology Limited | Cation-selective polymeric electrodes |
-
1942
- 1942-05-13 GB GB6525/42A patent/GB587512A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2722801A (en) * | 1949-05-24 | 1955-11-08 | Rolls Royce | Exhaust ducting arrangements for gas-turbine engines |
US3756629A (en) * | 1971-10-01 | 1973-09-04 | Victaulic Co Of America | Stud system of joining pipe and couplings for same |
EP0080404A1 (en) * | 1981-11-19 | 1983-06-01 | Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." | Assembly of two joined rotationally symmetrical objects made of materials with differing co-efficients of dilatation |
US4452038A (en) * | 1981-11-19 | 1984-06-05 | S.N.E.C.M.A. | System for attaching two rotating parts made of materials having different expansion coefficients |
GB2259954A (en) * | 1991-09-27 | 1993-03-31 | Short Brothers Plc | Ducted fan turbine engine nozzle assembly |
GB2259954B (en) * | 1991-09-27 | 1994-12-14 | Short Brothers Plc | Ducted fan turbine engine nozzle assembly |
US5603471A (en) * | 1991-09-27 | 1997-02-18 | Short Brothers Plc | Ducted fan turbine engine nozzle assembly |
US5395505A (en) * | 1991-10-31 | 1995-03-07 | Monitoring Technology Limited | Cation-selective polymeric electrodes |
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