GB706924A - Improvements in or relating to aircraft - Google Patents
Improvements in or relating to aircraftInfo
- Publication number
- GB706924A GB706924A GB8801/51A GB880151A GB706924A GB 706924 A GB706924 A GB 706924A GB 8801/51 A GB8801/51 A GB 8801/51A GB 880151 A GB880151 A GB 880151A GB 706924 A GB706924 A GB 706924A
- Authority
- GB
- United Kingdom
- Prior art keywords
- oxidant
- april
- fuel
- aircraft
- valves
- 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
- 239000000446 fuel Substances 0.000 abstract 2
- 239000007800 oxidant agent Substances 0.000 abstract 2
- 230000001590 oxidative effect Effects 0.000 abstract 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N Dioxygen Chemical group O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 abstract 1
- 238000002485 combustion reaction Methods 0.000 abstract 1
- 238000007599 discharging Methods 0.000 abstract 1
- 238000002347 injection Methods 0.000 abstract 1
- 239000007924 injection Substances 0.000 abstract 1
- HOQADATXFBOEGG-UHFFFAOYSA-N isofenphos Chemical group CCOP(=S)(NC(C)C)OC1=CC=CC=C1C(=O)OC(C)C HOQADATXFBOEGG-UHFFFAOYSA-N 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Fire-Extinguishing By Fire Departments, And Fire-Extinguishing Equipment And Control Thereof (AREA)
Abstract
706,924. Jet propulsion plant. YATES, G. F. April 10. 1952 [April 16, 1951], No. 8801/51. Class 110(3) [Also in Group XXXIII] A rocket engine for an aircraft of discus form comprises four combustion chambers 69 discharging into a common nozzle 85 fitted with deflector plates 87 and a reheater 86. The oxidant is liquid oxygen and the fuel an alcohol-water mixture. The latter is fed through a jacket surrounding the com-. bustion chamber before injection. Valves control the flow of oxidant and fuel, and the ignition device. All three valves are controlled by a common throttle lever.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8801/51A GB706924A (en) | 1951-04-16 | 1951-04-16 | Improvements in or relating to aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8801/51A GB706924A (en) | 1951-04-16 | 1951-04-16 | Improvements in or relating to aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB706924A true GB706924A (en) | 1954-04-07 |
Family
ID=9859504
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB8801/51A Expired GB706924A (en) | 1951-04-16 | 1951-04-16 | Improvements in or relating to aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB706924A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2939648A (en) * | 1954-03-27 | 1960-06-07 | Paul O Tobeler | Rotating jet aircraft with lifting disc wing and centrifuging tanks |
| US3389879A (en) * | 1965-10-22 | 1968-06-25 | John J. Grebe | Aircraft |
-
1951
- 1951-04-16 GB GB8801/51A patent/GB706924A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2939648A (en) * | 1954-03-27 | 1960-06-07 | Paul O Tobeler | Rotating jet aircraft with lifting disc wing and centrifuging tanks |
| US3389879A (en) * | 1965-10-22 | 1968-06-25 | John J. Grebe | Aircraft |
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