CN105882957A - Carrier-borne vertical takeoff and landing unmanned attacker - Google Patents
Carrier-borne vertical takeoff and landing unmanned attacker Download PDFInfo
- Publication number
- CN105882957A CN105882957A CN201510023973.1A CN201510023973A CN105882957A CN 105882957 A CN105882957 A CN 105882957A CN 201510023973 A CN201510023973 A CN 201510023973A CN 105882957 A CN105882957 A CN 105882957A
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- CN
- China
- Prior art keywords
- carrier
- attacker
- borne
- vertical takeoff
- unmanned
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- 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.)
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Abstract
The invention provides a carrier-borne vertical takeoff and landing unmanned attacker. An unmanned aircraft is an important means in future wars. The main difficulty for the carrier-borne unmanned attacker lies in safe landing on a carrier. It is the ideal selection for the carrier-borne unmanned attacker to realize safe vertical takeoff and landing and high-speed flight.
Description
Technical field: aviation aircraft
Background technology: unmanned aerial vehicle is a kind of important means of future war, the main bugbear of carrier-borne UCAV be safety warship.Can safe vertical lift, again can high-speed flight, this is the optimal selection of carrier-borne UCAV.
Summary of the invention: the agent structure mode of carrier-borne vertical lift UCAV
Accompanying drawing illustrates:
Fig. 1, carrier-borne vertical lift UCAV schematic diagram
1, propeller shielding cabin
2, propeller blade
Fig. 2, vertical lift normal flight schematic diagram
1, vertical lift schematic diagram
2, propeller is released and is opened
3, gear is put down
4, normal flight schematic diagram
5, propeller is retracted into cabin
6, gear is regained.
Claims (1)
- The agent structure mode of the most carrier-borne vertical lift UCAV.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510023973.1A CN105882957A (en) | 2015-01-19 | 2015-01-19 | Carrier-borne vertical takeoff and landing unmanned attacker |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510023973.1A CN105882957A (en) | 2015-01-19 | 2015-01-19 | Carrier-borne vertical takeoff and landing unmanned attacker |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105882957A true CN105882957A (en) | 2016-08-24 |
Family
ID=56999590
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510023973.1A Withdrawn CN105882957A (en) | 2015-01-19 | 2015-01-19 | Carrier-borne vertical takeoff and landing unmanned attacker |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105882957A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720562A (en) * | 2018-12-04 | 2019-05-07 | 北京空天技术研究所 | Double dynamical reuse high-speed aircraft and its application method |
| CN109849604A (en) * | 2019-03-29 | 2019-06-07 | 熊子见 | Folding rotor triphibian |
-
2015
- 2015-01-19 CN CN201510023973.1A patent/CN105882957A/en not_active Withdrawn
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109720562A (en) * | 2018-12-04 | 2019-05-07 | 北京空天技术研究所 | Double dynamical reuse high-speed aircraft and its application method |
| CN109849604A (en) * | 2019-03-29 | 2019-06-07 | 熊子见 | Folding rotor triphibian |
| CN109849604B (en) * | 2019-03-29 | 2023-10-13 | 熊子见 | Folding rotor triphibian aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20160824 |
|
| WW01 | Invention patent application withdrawn after publication |