CN2188544Y - Flying disc - Google Patents
Flying disc Download PDFInfo
- Publication number
- CN2188544Y CN2188544Y CN94207726U CN94207726U CN2188544Y CN 2188544 Y CN2188544 Y CN 2188544Y CN 94207726 U CN94207726 U CN 94207726U CN 94207726 U CN94207726 U CN 94207726U CN 2188544 Y CN2188544 Y CN 2188544Y
- Authority
- CN
- China
- Prior art keywords
- engine
- flying saucer
- spout
- change
- change spout
- 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 - Fee Related
Links
- 229910052734 helium Inorganic materials 0.000 claims abstract description 10
- 239000001307 helium Substances 0.000 claims abstract description 10
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 claims abstract description 10
- 240000002836 Ipomoea tricolor Species 0.000 claims description 21
- 238000007789 sealing Methods 0.000 claims description 4
- 229910052724 xenon Inorganic materials 0.000 claims description 4
- FHNFHKCVQCLJFQ-UHFFFAOYSA-N xenon atom Chemical compound [Xe] FHNFHKCVQCLJFQ-UHFFFAOYSA-N 0.000 claims description 4
- VNWKTOKETHGBQD-UHFFFAOYSA-N methane Chemical compound C VNWKTOKETHGBQD-UHFFFAOYSA-N 0.000 abstract 2
- 239000007789 gas Substances 0.000 abstract 1
- 239000003345 natural gas Substances 0.000 abstract 1
- 239000003208 petroleum Substances 0.000 abstract 1
- 239000000567 combustion gas Substances 0.000 description 5
- 239000004593 Epoxy Substances 0.000 description 2
- 239000000446 fuel Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000005259 measurement Methods 0.000 description 2
- 230000001105 regulatory effect Effects 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229920003369 Kevlar® 49 Polymers 0.000 description 1
- 238000004026 adhesive bonding Methods 0.000 description 1
- 230000004888 barrier function Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 238000009924 canning Methods 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
Images
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)
- Lubrication Details And Ventilation Of Internal Combustion Engines (AREA)
- Toys (AREA)
Abstract
The utility model relates to a flying disc, comprising a propelling system (13), a wing compartment (8), a center compartment (9) and a cockpit (11). Lifting force is provided by Helium gas in the wing compartment (8), propelling force for a propelling system (14) is provided by an engine, and the flight of the flying disc is controlled by the rotation of rotary spouts and the transfer of guide vanes. The utility model can be used for tourism, short-distance passenger carrying, long-distance transportation, offshore patrol, airborne early warning, mine clearance, photography, magnetic exploration, geodetic survey, petroleum exploitation and natural gas exploitation.
Description
The utility model relates to a kind of new aircraft---flying saucer of being made up of propulsion system, wing tank, middle deck, driving compartment.
Flying saucer also claims the UFO(UFO), a large amount of both at home and abroad at present its discoveries of report, it may be present in extraterrestrial, and the flying saucer profile has takes a large amount of photos.
The purpose of this utility model is that a kind of new aircraft---flying saucer will be provided, and is used to go sightseeing, short distance carrying, long-distance transport, patrol on the sea, air-borne early warning, clearance, photograph, magnetic spy, geodesic measurement, exploitation oil, natural fuels.
The purpose of this utility model is achieved in that this flying saucer is a kind of aircraft that is lighter than air, and flying saucer has four wing tanks, is sealing member independently separately, is filled with helium in it, and the helium in the wing tank provides lift, and flying saucer can be floated in the air; Middle deck has two air bags, is filled with helium in it, is used for regulating the load-carrying of flying saucer.Aero-engine provides thrust, controls flight by the transfer of the rotation that can change spout and breather vane.Propulsion system is made up of both wings driving engine, aft engine, and driving engine can be used fanjet, Turbofan with Afterburner, afterburning turbojet engine, piston engine; Driving engine shunting jet pipe is the combustion gas change aspect that makes ejection by the transfer of commutation valve and the rotation that can change spout, breather vane, thus the flight of control flying saucer.At the flying saucer supporting region driving compartment and main cabin are arranged, xenon long-arc lamp and xenon short-act lamp are equipped with in the flying saucer bottom.
This flying saucer is used to go sightseeing, short distance carrying, long-distance transport, patrol on the sea, air-borne early warning, clearance, photograph, magnetic spy, geodesic measurement, exploitation oil, natural fuels.
The concrete structure of flying saucer is provided by following embodiment and accompanying drawing thereof.
Fig. 1, flying saucer wing tank structure side view.
Fig. 2, flying saucer wing tank structure birds-eye view.
Wing tank is by skeleton, bulkhead, shell, cabin be every forming in length and breadth; The formation of skeleton: a longeron (1) that stands on dish body center, the support (2) of fourth officer "+" font, longeron (1) are on the center-point of "+" font support (2) (3), and the fourth officer support respectively has a secondary round ring stand (4) outward.Vertically bulkhead (5) places between ring stand and the ring stand, and laterally bulkhead (6) places between vertical bulkhead and the vertical bulkhead.At ring stand (4) and vertically bulkhead (5), horizontal gluing one deck shell outside the bulkhead (6); The cabin is that position according to support (2) place vertically is divided into the dish body four wing tanks (8) every (7), (seeing that from Fig. 2 the cabin is overlapping with support (2) every (7)), each wing tank (8) all is an independently sealing member, it is equipped with the helium valve.Skeleton, bulkhead, canning material in length and breadth: carbon/epoxy, cabin barrier material: Kevlar 49/ epoxy.
Fig. 3, middle deck, supporting region site plan.
Middle deck (9) is connected into every cold bonding by six cabins, and middle deck (9) center is longeron (1), and two air bags are arranged in the middle deck (9), fills helium in it, is used for regulating the flying saucer load-carrying; When charging into helium in the air bag, the air in the middle deck is discharged from the dish body.The air bag mouth has the helium valve, and the bilge has exhausr port; Supporting region (13) is made up of driving compartment (11) and main cabin (12) below wing tank (8) and middle deck (9).
Fig. 4, propulsion system site plan
The hole of a circle is arranged in wing tank (8) lining, and wing tank (8) itself is a sealing member, and driving engine is installed in the hole; Driving engine (13) is installed in the both wings position and afterbody has driving engine (14).
Fig. 5, both wings engine structure scheme drawing
Both wings and aft engine in the propulsion system, available four kinds of driving engines as fanjet (15), can also be Turbofan with Afterburner, afterburning turbojet engine, piston engine, dividing turbine engine and piston engine two classes, is that example illustrates with the fanjet; The structure of shunting jet pipe (16): can change it has on spout (17), down can change spout (18), after can change spout (19), pipeline (20), jet pipe (21), valve (22), breather vane (23) commutate; Its mode of operation: if make the flight of flying saucer parallel lines, to change earlier and be transferred to parallel with jet pipe (21) with valve (22), combustion gas from after can change spout (19) ejection, can change rotatable 360 ° of spout, breather vane (23) turns 80 ° of angles, breather vane (23) is transferred to parallel with jet pipe (21).Flying saucer with piston engine is to drive the Pyatyi fan by piston engine to produce thrust, and shunting jet pipe structure is identical.
Fig. 6, aft engine structural representation.
The radical function of aft engine is the control heading, turns because the air-flow of aft engine ejection is easy to make flying saucer to produce the angle of attack and is easy to wide-angle; Its second function is to produce flight thrust, and the structure of aft engine is identical with the both wings driving engine, and different is that aft engine admission port (24) is by feeding in the flying disk body.
Fig. 7, flight control scheme drawing.
As making flying saucer to the 45 ° of flights in front lower place, transfer commutation valve (22), make combustion gas from can change spout (17) ejection, rotate to go up and can change spout (17) and transfer breather vane (23), make breather vane (23) 45 °, air flow line (32) towards the back upper place; When taking off vertically, combustion gas under can change spout and vertically spray; During vertical landing, combustion gas from can change spout and vertically spray; More than work and finish by the both wings driving engine.
Claims (2)
1, a kind of new aircraft-flying saucer is characterized in that it has four wing tanks, and is sealing member independently separately, in fill helium, middle deck (9) is that six cabins are connected into every cold bonding, and two air bags are arranged in the middle deck, in fill helium; Propulsion system is made up of both wings driving engine (13), aft engine (14), and flying saucer engine is turbine engine or piston engine, and piston engine drives the Pyatyi fan and produces thrust; Shunting jet pipe (16) by on can change spout (17), down can change spout (18), after can change spout (19), pipeline (20), jet pipe (21), commutation valve (22), breather vane (23) constitutes, can change spout can 360 ° of rotations, and breather vane can 80 ° of transfers; Xenon short-act lamp and xenon long-arc lamp are equipped with in the flying saucer bottom.
2, flying saucer according to claim 1 is characterized in that turbine engine can be with fanjet or Turbofan with Afterburner or afterburning turbojet engine.
Priority Applications (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN94207726U CN2188544Y (en) | 1994-04-09 | 1994-04-09 | Flying disc |
| PCT/CN1995/000026 WO1995027652A1 (en) | 1994-04-09 | 1995-04-04 | Saucer-shaped aircraft |
| AU21342/95A AU2134295A (en) | 1994-04-09 | 1995-04-04 | Saucer-shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN94207726U CN2188544Y (en) | 1994-04-09 | 1994-04-09 | Flying disc |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2188544Y true CN2188544Y (en) | 1995-02-01 |
Family
ID=5045261
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN94207726U Expired - Fee Related CN2188544Y (en) | 1994-04-09 | 1994-04-09 | Flying disc |
Country Status (3)
| Country | Link |
|---|---|
| CN (1) | CN2188544Y (en) |
| AU (1) | AU2134295A (en) |
| WO (1) | WO1995027652A1 (en) |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101875397B (en) * | 2009-04-28 | 2012-12-05 | 同济大学 | Duct structure for airship |
| CN103640701A (en) * | 2013-09-21 | 2014-03-19 | 张宝海 | Basic structure and basic flying principle of flying saucer |
| CN104828242A (en) * | 2015-05-03 | 2015-08-12 | 李彦征 | Jetting system on tailpipe nozzle of jet airplane |
| CN105363204A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Manufacturing method of gold flying saucer with negative weight |
| CN105363205A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Gold flying saucer with negative weight |
| CN105363203A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Using method of gold flying saucer with negative weight |
| CN108715223A (en) * | 2014-02-10 | 2018-10-30 | 林月洪 | Efficient aircraft power source |
| CN108945484A (en) * | 2018-07-02 | 2018-12-07 | 山东理工大学 | A kind of two-way air injection aerial vehicle |
| CN109866908A (en) * | 2019-03-06 | 2019-06-11 | 重庆理工大学 | A kind of high pressure gas is the Dished aircraft of power |
| CN110481760A (en) * | 2019-07-15 | 2019-11-22 | 陈云桥 | No blade rotates air duct engine aircraft engine |
Families Citing this family (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP2537743B1 (en) | 2006-10-20 | 2014-02-19 | LTA Corporation | Lenticular airship |
| EA024007B1 (en) | 2007-08-09 | 2016-08-31 | ЭлТиЭй КОРПОРЕЙШН | Systems and method for displaying attitude information associated with an airship |
| US8894002B2 (en) | 2010-07-20 | 2014-11-25 | Lta Corporation | System and method for solar-powered airship |
| USD670638S1 (en) | 2010-07-20 | 2012-11-13 | Lta Corporation | Airship |
| US8596571B2 (en) | 2011-03-31 | 2013-12-03 | Lta Corporation | Airship including aerodynamic, floatation, and deployable structures |
| WO2015108607A2 (en) | 2013-11-04 | 2015-07-23 | Lta Corporation | Cargo airship |
| CN114228994B (en) * | 2021-12-03 | 2024-08-20 | 太仓点石航空动力有限公司 | Propulsion-control integrated power device for individual flying wing type flight knapsack |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3155342A (en) * | 1961-05-25 | 1964-11-03 | Bolkow Entwicklungen Kg | Vtol aircraft construction |
| DE1993361U (en) * | 1968-04-25 | 1968-09-05 | Ver Flugtechnische Werke G M B | DEFLECTION DEVICE FOR IN PARTICULAR HOT EXHAUST JETS AT AIRCRAFT ENGINES. |
| US3873962A (en) * | 1973-11-28 | 1975-03-25 | Symbolic Displays Inc | Aircraft warning lamp system |
| GB2196587B (en) * | 1980-10-31 | 1988-08-24 | Rolls Royce | Jet pipe for jet propulsion in aircraft |
| US4606515A (en) * | 1984-05-29 | 1986-08-19 | Hickey John J | Hybrid annular airship |
| US4798328A (en) * | 1987-05-22 | 1989-01-17 | United Technologies Corporation | Area controlled, thrust vectoring vane cascade with nutating control vane |
| SE464753B (en) * | 1987-08-20 | 1991-06-10 | Bruno Winzell | DEVICE FOR HEIGHT ADJUSTMENT OF AIRCRAFT |
| US4901948A (en) * | 1988-11-04 | 1990-02-20 | Panos Peter M | Control system for jet propelled vehicle |
| US5080304A (en) * | 1990-07-30 | 1992-01-14 | Grumman Aerospace Corporation | Aircraft hold-down device |
-
1994
- 1994-04-09 CN CN94207726U patent/CN2188544Y/en not_active Expired - Fee Related
-
1995
- 1995-04-04 AU AU21342/95A patent/AU2134295A/en not_active Withdrawn
- 1995-04-04 WO PCT/CN1995/000026 patent/WO1995027652A1/en active Application Filing
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN101875397B (en) * | 2009-04-28 | 2012-12-05 | 同济大学 | Duct structure for airship |
| CN103640701A (en) * | 2013-09-21 | 2014-03-19 | 张宝海 | Basic structure and basic flying principle of flying saucer |
| CN108715223B (en) * | 2014-02-10 | 2021-08-10 | 林月洪 | Aircraft power source |
| CN108715223A (en) * | 2014-02-10 | 2018-10-30 | 林月洪 | Efficient aircraft power source |
| CN104828242A (en) * | 2015-05-03 | 2015-08-12 | 李彦征 | Jetting system on tailpipe nozzle of jet airplane |
| CN105363203B (en) * | 2015-11-20 | 2018-03-30 | 郑州中德美游乐设备有限公司 | The application method of golden flying saucer |
| CN105363203A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Using method of gold flying saucer with negative weight |
| CN105363205B (en) * | 2015-11-20 | 2018-10-12 | 郑州中德美游乐设备有限公司 | Golden flying saucer |
| CN105363205A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Gold flying saucer with negative weight |
| CN105363204A (en) * | 2015-11-20 | 2016-03-02 | 郑州中德美游乐设备有限公司 | Manufacturing method of gold flying saucer with negative weight |
| CN108945484A (en) * | 2018-07-02 | 2018-12-07 | 山东理工大学 | A kind of two-way air injection aerial vehicle |
| CN109866908A (en) * | 2019-03-06 | 2019-06-11 | 重庆理工大学 | A kind of high pressure gas is the Dished aircraft of power |
| CN109866908B (en) * | 2019-03-06 | 2021-06-22 | 重庆理工大学 | Disc-shaped aircraft taking high-pressure gas as power |
| CN110481760A (en) * | 2019-07-15 | 2019-11-22 | 陈云桥 | No blade rotates air duct engine aircraft engine |
Also Published As
| Publication number | Publication date |
|---|---|
| WO1995027652A1 (en) | 1995-10-19 |
| AU2134295A (en) | 1995-10-30 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |