GB1133415A - Combustion chamber for a rocket - Google Patents
Combustion chamber for a rocketInfo
- Publication number
- GB1133415A GB1133415A GB36079/67A GB3607967A GB1133415A GB 1133415 A GB1133415 A GB 1133415A GB 36079/67 A GB36079/67 A GB 36079/67A GB 3607967 A GB3607967 A GB 3607967A GB 1133415 A GB1133415 A GB 1133415A
- Authority
- GB
- United Kingdom
- Prior art keywords
- wire
- turns
- combustion chamber
- section
- cross
- 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
- Gas Burners (AREA)
Abstract
1,133,415. Rocket combustion chambers. BÍLKOW G.m.b.H. Aug. 7, 1967 [Aug. 12, 1966], No.36079/67. Headings F1J and F1L. In a rocket combustion chamber having an internal wall with cooling channels extending longitudinally on its external surface and with an external wall covering the cooling channels, the external wall being formed by a continuously wound wire with adjacent turns connected to each other and to the internal wall, the cross-section of the wire is such that the turns are positively connected to each other in the longitudinal direction of the combustion chamber. The cross-section of the wire may be of the double-hook form shown in Fig. 7, providing an interlocking engagement between adjacent turns of the winding. In addition, the turns are connected together by adhesive or by soldering, welding or the like. As shown, the turns may form continuous upper and lower surfaces 8, 9. Instead of being oblique as shown, the central part 13 and the two free ends 12 of the wire cross-section may be upright. Instead of being rounded as shown, the free ends 12 may be rectangular or trapezoidal. An S-shaped crosssection may be used. There may be several layers of wire, which may be of different materials.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DEB0088452 | 1966-08-12 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1133415A true GB1133415A (en) | 1968-11-13 |
Family
ID=6984300
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB36079/67A Expired GB1133415A (en) | 1966-08-12 | 1967-08-07 | Combustion chamber for a rocket |
Country Status (3)
Country | Link |
---|---|
US (1) | US3507449A (en) |
DE (1) | DE1303377B (en) |
GB (1) | GB1133415A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2690472C1 (en) * | 2018-07-30 | 2019-06-03 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | Solid-propellant charge for starting jet engines |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3630449A (en) * | 1970-05-11 | 1971-12-28 | Us Air Force | Nozzle for rocket engine |
US4071194A (en) * | 1976-10-28 | 1978-01-31 | The United States Of America As Represented By The Secretary Of The Navy | Means for cooling exhaust nozzle sidewalls |
US4477024A (en) * | 1983-04-05 | 1984-10-16 | The United States Of America As Represented By The Secretary Of The Air Force | Carbon/carbon rocket motor exit cone reinforcement |
US4740357A (en) * | 1986-06-27 | 1988-04-26 | International Fuel Cells | Radiation shield for reformer apparatus |
US7596940B2 (en) * | 2005-03-22 | 2009-10-06 | Pratt & Whitney Rocketdyne, Inc. | Rocket engine nozzle and method of fabricating a rocket engine nozzle using pressure brazing |
DE102005059540A1 (en) * | 2005-08-19 | 2007-06-14 | Bauer, Jörg R. | Reliably fastened to each other, flat components, and component |
US10527003B1 (en) | 2015-04-12 | 2020-01-07 | Rocket Lab Usa, Inc. | Rocket engine thrust chamber, injector, and turbopump |
FR3042542B1 (en) * | 2015-10-20 | 2017-12-01 | Snecma | PROPULSIVE CHAMBER AND METHOD OF MANUFACTURE |
Family Cites Families (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
BE538923A (en) * | ||||
DE526049C (en) * | 1931-06-02 | Mathias Varnhagen | Butt joint of components made of wood or similar flexible materials | |
US2288094A (en) * | 1939-01-28 | 1942-06-30 | Gen Motors Corp | Method of making tubing |
US3044257A (en) * | 1958-06-02 | 1962-07-17 | Thiokol Chemical Corp | Combustion chamber outer jacket |
US3035333A (en) * | 1959-01-09 | 1962-05-22 | Edward F Baehr | Method of making a regeneratively cooled combustion chamber |
US3162012A (en) * | 1961-05-04 | 1964-12-22 | Casey J Blaze | Formed metal ribbon wrap |
US3254487A (en) * | 1963-01-04 | 1966-06-07 | Edward F Baehr | Rocket motor casing |
US3289843A (en) * | 1964-03-19 | 1966-12-06 | Dorr Oliver Inc | Apparatus for centrifugal screening |
-
0
- DE DEB88452A patent/DE1303377B/de not_active Withdrawn
-
1967
- 1967-08-07 GB GB36079/67A patent/GB1133415A/en not_active Expired
- 1967-08-08 US US659078A patent/US3507449A/en not_active Expired - Lifetime
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2690472C1 (en) * | 2018-07-30 | 2019-06-03 | Федеральное казенное предприятие "Государственный научно-исследовательский институт химических продуктов" (ФКП "ГосНИИХП") | Solid-propellant charge for starting jet engines |
Also Published As
Publication number | Publication date |
---|---|
DE1303377B (en) | 1971-09-16 |
US3507449A (en) | 1970-04-21 |
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