GB1157119A - Process for temporarily Facilitating the Manoeuvering of an Aircraft, and device for Implementing said process - Google Patents
Process for temporarily Facilitating the Manoeuvering of an Aircraft, and device for Implementing said processInfo
- Publication number
- GB1157119A GB1157119A GB32412/66A GB3241266A GB1157119A GB 1157119 A GB1157119 A GB 1157119A GB 32412/66 A GB32412/66 A GB 32412/66A GB 3241266 A GB3241266 A GB 3241266A GB 1157119 A GB1157119 A GB 1157119A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fuel
- heated
- water
- aircraft
- july
- 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 4
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 abstract 3
- 239000003570 air Substances 0.000 abstract 1
- 239000012080 ambient air Substances 0.000 abstract 1
- 239000012530 fluid Substances 0.000 abstract 1
- 239000002828 fuel tank Substances 0.000 abstract 1
- 239000007789 gas Substances 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 230000001141 propulsive effect Effects 0.000 abstract 1
- 230000008016 vaporization Effects 0.000 abstract 1
- 238000009834 vaporization Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
- B64D27/02—Aircraft characterised by the type or position of power plants
- B64D27/023—Aircraft characterised by the type or position of power plants of rocket type, e.g. for assisting taking-off or braking
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
- B64C23/005—Influencing air flow over aircraft surfaces, not otherwise provided for by other means not covered by groups B64C23/02 - B64C23/08, e.g. by electric charges, magnetic panels, piezoelectric elements, static charges or ultrasounds
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/38—Jet flaps
-
- 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
- Y02T50/10—Drag reduction
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
Abstract
1,157,119. Controlling aircraft. CONSERVATOIRE NATIONAL DES ARTS ET METIERS. 19 July, 1966 [19 July, 1965], No. 32412/66. Heading B7G. [Also in Divisions F1 and F2] A device to provide auxiliary temporary jet thrust to aid control of an aircraft comprises an insulated tank 8 of water or fuel heated to above its vaporization temperature whence it is led through narrow ducts 9, to be released when required through jets 11. The water or fuel may be heated either on the ground from an auxiliary source, or from an electrical resistance heater, or from a heat exchanger 12 heated by the engine exhaust gases. The ejection of the heated water, which immediately vaporizes, may be used to either augment the propulsive thrust, or augment lift, or entrain some other fluid (e.g. fuel fron the fuel tanks to jettison it) or assist control. The heated liquid may be ejected either into internal air passages in the main area, or over control areas to correct boundary layer breakaway, or to reduce drag. In the event of an engine failure, the device may be used to eject into the jet engine nozzles, possibly with entrained fuel or ambient air, to provide sufficient energy to avoid an accident.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR3221A FR1453944A (en) | 1965-07-19 | 1965-07-19 | Method for temporarily facilitating the upgrades of an aerodyne and device for implementing this method |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB1157119A true GB1157119A (en) | 1969-07-02 |
Family
ID=8569188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB32412/66A Expired GB1157119A (en) | 1965-07-19 | 1966-07-19 | Process for temporarily Facilitating the Manoeuvering of an Aircraft, and device for Implementing said process |
Country Status (2)
| Country | Link |
|---|---|
| FR (1) | FR1453944A (en) |
| GB (1) | GB1157119A (en) |
-
1965
- 1965-07-19 FR FR3221A patent/FR1453944A/en not_active Expired
-
1966
- 1966-07-19 GB GB32412/66A patent/GB1157119A/en not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR1453944A (en) | 1966-07-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PS | Patent sealed | ||
| PLNP | Patent lapsed through nonpayment of renewal fees |