JPWO2019192750A5 - - Google Patents
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- Publication number
- JPWO2019192750A5 JPWO2019192750A5 JP2020506220A JP2020506220A JPWO2019192750A5 JP WO2019192750 A5 JPWO2019192750 A5 JP WO2019192750A5 JP 2020506220 A JP2020506220 A JP 2020506220A JP 2020506220 A JP2020506220 A JP 2020506220A JP WO2019192750 A5 JPWO2019192750 A5 JP WO2019192750A5
- Authority
- JP
- Japan
- Prior art keywords
- jet engine
- propulsion jet
- aircraft
- preliminary auxiliary
- auxiliary 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.)
- Granted
Links
- 239000000446 fuel Substances 0.000 claims 8
- 230000001681 protective Effects 0.000 claims 6
- 230000001141 propulsive Effects 0.000 claims 1
Claims (5)
前記第２の燃料供給源は前記第１の燃料供給源から完全に分離され、前記予備補助推進ジェットエンジンのみを供給するための専用であり、
前記予備補助推進ジェットエンジンは、前記主推進ジェットエンジンとは独立してスイッチオンすることができる航空機であって、
前記航空機は、飛行中に前記予備補助推進ジェットエンジンの吸気および排気開口部を覆い、かつ、飛行中に開放されるように制御可能な保護カバー要素を更に備え、前記保護
カバー要素は、前記予備補助推進ジェットエンジンを保護する通常の保護位置と、前記予備補助推進ジェットエンジンの開口部を覆わない開放位置と、を有し、
前記航空機は、前記主推進ジェットエンジンが使用され、かつ、前記予備補助推進ジェットエンジンは、全ての運転中のエンジンに影響を及ぼす劇的な事象が発生したときに作動の準備ができたままであることを保証するために使用されず、前記保護カバー要素は通常の保護位置にある、通常飛行モードを有し、及び、
前記航空機は、全ての前記主推進ジェットエンジンが故障した場合に、前記保護カバー要素が開放位置にあり、前記予備補助推進ジェットエンジンが前記航空機の降下角度を低減させる推進力を提供する、緊急飛行モードを有する、
航空機。 It has a primary fuel source for a main propulsion jet engine and said main propulsion jet engine, and a second fuel source for a spare auxiliary propulsion jet engine and said preliminary auxiliary propulsion jet engine.
The second fuel source is completely separate from the first fuel source and is dedicated to supplying only the preliminary auxiliary propulsion jet engine.
The preliminary auxiliary propulsion jet engine is an aircraft that can be switched on independently of the main propulsion jet engine.
The aircraft further comprises a protective cover element that covers the intake and exhaust openings of the preliminary auxiliary propulsion jet engine during flight and is controllable to be open during flight.
The cover element has a normal protective position that protects the preliminary auxiliary propulsion jet engine and an open position that does not cover the opening of the preliminary auxiliary propulsion jet engine.
The aircraft uses the main propulsion jet engine, and the preliminary auxiliary propulsion jet engine remains ready to operate in the event of a dramatic event affecting all operating engines. Not used to ensure that the protective cover element is in a normal protective position, has a normal flight mode, and
The aircraft is an emergency flight in which the protective cover element is in the open position and the preliminary auxiliary propulsion jet engine provides propulsion to reduce the descent angle of the aircraft in the event of failure of all the main propulsion jet engines. Has a mode,
aircraft.
前記補助動力ユニットは、前記予備補助推進ジェットエンジンとは異なる燃料消費エンジンから構成され、前記第２の燃料供給源とは異なる燃料供給源から燃料を供給される、
請求項１～３のいずれか一項に記載の航空機。 Further equipped with an auxiliary power unit and a generator that generates electric power by the auxiliary power unit,
The auxiliary power unit is composed of a fuel consumption engine different from the preliminary auxiliary propulsion jet engine, and is supplied with fuel from a fuel supply source different from the second fuel supply source.
The aircraft according to any one of claims 1 to 3 .
前記主推進ジェットエンジンから提供される推進力により、前記予備補助推進ジェットエンジンが切られた状態で、通常飛行モードで航空機を運航するステップと、
全ての前記主推進ジェットエンジンが故障した場合に、前記保護カバー要素を飛行中に通常の保護位置から解放位置に変位させて、前記予備補助推進ジェットエンジンによって提供される推進力を用いて緊急飛行モードで航空機を運航するステップと、
を含む、方法。 The method for operating the aircraft according to any one of claims 1 to 4 .
A step of operating an aircraft in a normal flight mode with the preliminary auxiliary propulsion jet engine turned off by the propulsive force provided by the main propulsion jet engine.
In the event of failure of all the main propulsion jet engines, the protective cover element is displaced from the normal protection position to the open position during flight and emergency flight is performed using the propulsion force provided by the preliminary auxiliary propulsion jet engine. Steps to operate an aircraft in mode and
Including, how.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| NL1042808A NL1042808B1 (en) | 2018-04-03 | 2018-04-03 | Airplane with improved safety |
| NL1042808 | 2018-04-03 | ||
| PCT/EP2019/000103 WO2019192750A1 (en) | 2018-04-03 | 2019-04-01 | Airplane with improved safety |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| JP2021517532A JP2021517532A (en) | 2021-07-26 |
| JPWO2019192750A5 true JPWO2019192750A5 (en) | 2022-01-25 |
| JP7180957B2 JP7180957B2 (en) | 2022-11-30 |
Family
ID=66776288
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP2020506220A Active JP7180957B2 (en) | 2018-04-03 | 2019-04-01 | safety enhancement aircraft |
Country Status (10)
| Country | Link |
|---|---|
| US (1) | US11396379B2 (en) |
| EP (1) | EP3630611B1 (en) |
| JP (1) | JP7180957B2 (en) |
| CN (1) | CN111051204A (en) |
| BR (1) | BR112020007522A2 (en) |
| CA (1) | CA3076089C (en) |
| NL (1) | NL1042808B1 (en) |
| RU (1) | RU2020102719A (en) |
| SG (1) | SG11202000211XA (en) |
| WO (1) | WO2019192750A1 (en) |
Family Cites Families (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3529793A (en) * | 1969-03-27 | 1970-09-22 | Zaharias Krongos | Airplane with emergency propeller and detachable wings |
| US4932609A (en) * | 1989-02-27 | 1990-06-12 | United Technologies Corporation | Fuel transfer system for aircraft |
| JP3522371B2 (en) * | 1995-01-19 | 2004-04-26 | 綾子 大塚 | Safety aircraft |
| CA2507280A1 (en) * | 2005-05-24 | 2006-11-24 | Alfred L. Mathieu | Auxiliary, rotatable, independent jet engines on plane fuselage |
| US7549604B2 (en) * | 2006-10-26 | 2009-06-23 | Hutterer Joseph A | Fuel efficient fixed wing aircraft |
| US8528312B1 (en) * | 2013-01-08 | 2013-09-10 | Ali A. A. J. Shammoh | Turbojet engine inlet and exhaust covers |
| FR3001442B1 (en) | 2013-01-29 | 2016-05-20 | Microturbo | ARCHITECTURE FOR PROVIDING IMPROVED ELECTRIC POWER SUPPLY IN AN AIRCRAFT |
| US20210214093A1 (en) * | 2020-01-15 | 2021-07-15 | Jocelyn Bruno | Mini-jet engine, in-flight safety measure |
-
2018
- 2018-04-03 NL NL1042808A patent/NL1042808B1/en not_active IP Right Cessation
-
2019
- 2019-04-01 SG SG11202000211XA patent/SG11202000211XA/en unknown
- 2019-04-01 CA CA3076089A patent/CA3076089C/en active Active
- 2019-04-01 WO PCT/EP2019/000103 patent/WO2019192750A1/en unknown
- 2019-04-01 CN CN201980003613.1A patent/CN111051204A/en not_active Withdrawn
- 2019-04-01 RU RU2020102719A patent/RU2020102719A/en unknown
- 2019-04-01 JP JP2020506220A patent/JP7180957B2/en active Active
- 2019-04-01 US US16/629,529 patent/US11396379B2/en active Active
- 2019-04-01 BR BR112020007522-1A patent/BR112020007522A2/en not_active IP Right Cessation
- 2019-04-01 EP EP19728870.7A patent/EP3630611B1/en active Active
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