CN106500550A - Escape tower trouserss booster rocket with the remote control hang gliding tail vane wing - Google Patents
Escape tower trouserss booster rocket with the remote control hang gliding tail vane wing Download PDFInfo
- Publication number
- CN106500550A CN106500550A CN201611157918.2A CN201611157918A CN106500550A CN 106500550 A CN106500550 A CN 106500550A CN 201611157918 A CN201611157918 A CN 201611157918A CN 106500550 A CN106500550 A CN 106500550A
- Authority
- CN
- China
- Prior art keywords
- trouserss
- wing
- booster rocket
- escape tower
- hang
- 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.)
- Pending
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/04—Stabilising arrangements using fixed fins
- F42B10/06—Tail fins
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- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Emergency Lowering Means (AREA)
Abstract
The present invention relates to rocketry field, escape tower with the remote control hang gliding tail vane wing, trouserss, booster rocket is related specifically to.It is characterized in that in escape tower, trouserss, a pair of hang glidings are respectively equipped with booster rocket, in escape tower, trouserss, the vertical fin wing is equipped with booster rocket, the vertical fin wing is arranged on the vertical symmetry central plane of a pair of hang glidings, the afterbody of a pair of hang glidings is provided with glide attitude balance wing, the afterbody of the vertical fin wing is provided with the tail vane wing, escape tower, trouserss, receiver of remote-control sytem and corresponding robot drive mechanism and position signalling wireless transmitter is respectively arranged with booster rocket, escape tower can be controlled by ground control centre, trouserss, booster rocket lands according to specified place during gliding of falling.This invention greatly reduces escape tower, trouserss, the recovery difficult of booster rocket remains and cost recovery, can also avoid the danger brought at village of dropping.
Description
Technical field
The present invention relates to rocketry field, escape tower with the remote control hang gliding tail vane wing, rectification is related specifically to
Cover, booster rocket.
Background technology
Prostatitis of the space rocket technology of China already in the world, rocket launching technology are important the one of Space Science and Technology
Ring.The annual rocket launching number of times of China is also that position is at the forefront in the world, but the escape tower after rocket launching, trouserss, helps
It is falling down for freely falling body to push away rocket and falling for a booster-missile combination.Drop point however in remote, thickly forested mountains, otherwise be possible to
Fall and cause unnecessary prestige to do harm in village, fall and huge difficulty is brought in remote, thickly forested mountains to the recovery of remains, expend substantial amounts of people
The cost recovery of power material resources is high.How customer service the deficiencies in the prior art, when making escape tower, trouserss, booster rocket fall, able person is
Be controlled by fall a little, there is provided the escape tower, trouserss, booster rocket with the remote control hang gliding tail vane wing is just into the present invention
Research topic.
Content of the invention
Present invention aim to customer service the deficiencies in the prior art, when enabling escape tower, trouserss, booster rocket to fall
Artificial it is controlled by falling a little, there is provided escape tower, trouserss with the remote control hang gliding tail vane wing, booster rocket.
The present invention is achieved through the following technical solutions.With the escape tower of the remote control hang gliding tail vane wing, trouserss,
Booster rocket, including escape tower, trouserss, booster rocket it is characterized in that being set on escape tower, trouserss, booster rocket respectively
There are a pair of hang glidings, the vertical fin wing being equipped with escape tower, trouserss, booster rocket, the vertical fin wing is arranged on a pair of glidings
On the vertical symmetry central plane of the wing, the afterbody of a pair of hang glidings is provided with glide attitude balance wing, and the afterbody of the vertical fin wing is provided with tail
The rudder wing, is respectively arranged with receiver of remote-control sytem and corresponding robot drive mechanism and position on escape tower, trouserss, booster rocket
Signal wireless transmitter, ground control centre according to monitor escape tower, trouserss, booster rocket position send remote control in real time
Instruction, the receiver of remote-control sytem on escape tower, trouserss, booster rocket go to drive corresponding robot after receiving telecommand
Drive mechanism, so as to drive the action of glide attitude balance wing and the tail vane wing, to reach control escape tower, trouserss, boosting fire
Arrow lands according to specified place during gliding of falling.
Further, bone is done using light-weight metal or carbonic acid fiber in order to mitigate hang gliding and the vertical fin wing described in weight
Frame, aerofoil are made using flame retardant fabric.
Can see from above-mentioned concrete technical scheme, the technology as a result of the present invention makes escape tower, rectification
Cover, booster rocket when falling can artificial control fall a little, significantly reduce escape tower, trouserss, booster rocket remains
Recovery difficult and cost recovery, the danger brought at village of dropping can also be avoided.
In order to the present invention is better described, do furtherly with reference to specific embodiment and embodiment accompanying drawing
Bright.
Description of the drawings
Fig. 1 is that the present invention is specifically applied on rocket the whole structure figure after region of interest.
Fig. 2 is the left view of Fig. 1.
Fig. 3 is that escape tower loads onto hang gliding, the structure chart of the tail vane wing.
Fig. 4 is the left view of Fig. 3.
Fig. 5 is that trouserss load onto hang gliding, the structure chart of the tail vane wing.
Fig. 6 is the left view of Fig. 5.
Fig. 7 is that booster rocket loads onto hang gliding, the structure chart of the tail vane wing.
Fig. 8 is the left view of Fig. 7.
Fig. 9 is present invention control schematic diagram in this world.
In figure：1- escape towers；2- hang glidings；The 3- vertical fin wings；The 4- tail vane wings；5- glide attitude balance wings；6- trouserss；7-
Booster rocket；8- one-stage rockets；9- booster-missile combinations；10- ground control centres；11- receivers of remote-control sytem；12- position signallings are wireless
Emitter；The left balance wing motor of 13- glide attitudes；The right balance wing motor of 14- glide attitudes；The 15- tail vanes wing drives
Motor.
Specific embodiment
From Fig. 1 ~ Fig. 8, escape tower 1, trouserss 6 with the 2 tail vane wing 4 of remote control hang gliding, booster rocket 7, including
Escape tower 1, trouserss 6,7 body of booster rocket, on escape tower 1, trouserss 6, booster rocket 7 are equipped with a pair and are symmetrical arranged
Hang gliding 2, be equipped with the vertical fin wing 3 on escape tower 1, trouserss 6, booster rocket 7, and the vertical fin wing 3 be arranged on a pair symmetrical
On the vertical symmetry central plane of the hang gliding 2 of setting, the afterbody of a pair symmetrically arranged hang glidings 2 is provided with glide attitude balance
The wing 5, the afterbody of the vertical fin wing 3 are provided with the tail vane wing 4, are respectively arranged with 11 and of receiver of remote-control sytem on escape tower 1, trouserss 6, booster rocket 7
Corresponding robot drive mechanism and position signalling wireless transmitter 12, ground control centre 10 is according to monitoring escape tower
1st, trouserss 6, the position of booster rocket 7 send telecommand in real time, and the remote control on escape tower 1, trouserss 6, booster rocket 7 connects
Receive and go to drive glide attitude left-right balance wing motor 13,14 and tail vane wing motor after device 11 receives telecommand
15, so as to drive 4 action of glide attitude balance wing 5 and the tail vane wing, existed with reaching control escape tower 1, trouserss 6, booster rocket 7
Fall.Above-described hang gliding 2 and the vertical fin wing 3 adopt aluminum alloy framework,
Aerofoil is made using flame retardant fabric.
Can see from above-mentioned specific embodiment, as a result of the escape tower 1, whole that makes of technology of the present invention
Stream cover 6, booster rocket 7 when falling can artificial control fall a little, significantly reduce escape tower 1, trouserss 6, boosting fire
The recovery difficult of 7 remains of arrow and cost recovery, can also avoid the danger brought at village of dropping.The technology of the present invention can also
It is applied on a booster-missile combination.
Specific embodiment listed above, one kind only therein cannot be enumerated, all protection domains under this invention
The modification extension that is made belongs to protection scope of the present invention.
Claims (2)
1. escape tower with the remote control hang gliding tail vane wing, trouserss, booster rocket, including escape tower, trouserss, booster rocket
It is characterized in that a pair of hang glidings are respectively equipped with escape tower, trouserss, booster rocket, in escape tower, trouserss, boosting fire
The vertical fin wing is equipped with arrow, and the vertical fin wing is arranged on the vertical symmetry central plane of a pair of hang glidings, a pair of hang glidings
Afterbody is provided with glide attitude balance wing, and the afterbody of the vertical fin wing is provided with the tail vane wing, is respectively arranged with escape tower, trouserss, booster rocket
Receiver of remote-control sytem and corresponding robot drive mechanism and position signalling wireless transmitter.
2. escape tower with the remote control hang gliding tail vane wing according to claim 1, trouserss, booster rocket, its feature
It is that the hang gliding and the vertical fin wing do skeleton using light-weight metal or carbonic acid fiber, aerofoil is made using flame retardant fabric.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611157918.2A CN106500550A (en) | 2016-12-15 | 2016-12-15 | Escape tower trouserss booster rocket with the remote control hang gliding tail vane wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611157918.2A CN106500550A (en) | 2016-12-15 | 2016-12-15 | Escape tower trouserss booster rocket with the remote control hang gliding tail vane wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106500550A true CN106500550A (en) | 2017-03-15 |
Family
ID=58331063
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611157918.2A Pending CN106500550A (en) | 2016-12-15 | 2016-12-15 | Escape tower trouserss booster rocket with the remote control hang gliding tail vane wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106500550A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107152896A (en) * | 2017-05-26 | 2017-09-12 | 合肥凯石投资咨询有限公司 | A kind of recyclable main boost motor |
| CN107192305A (en) * | 2017-05-26 | 2017-09-22 | 合肥凯石投资咨询有限公司 | A kind of recyclable auxiliary boost motor |
| CN107300343A (en) * | 2017-06-12 | 2017-10-27 | 合肥凯石投资咨询有限公司 | A kind of recyclable boost motor |
| CN112124625A (en) * | 2020-08-27 | 2020-12-25 | 上海宇航系统工程研究所 | Ship and rocket integrated shuttle aircraft and flight control method |
| CN114963867A (en) * | 2022-06-16 | 2022-08-30 | 陕西空天动力研究院有限公司 | Vacuum high-speed launching system of combined power rocket and launching and recovering method thereof |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1107114A (en) * | 1993-01-14 | 1995-08-23 | 埃尔诺航空技术有限公司 | Apparatus for controling |
| US20080061188A1 (en) * | 2005-09-09 | 2008-03-13 | General Dynamics Ordnance And Tactical Systems, Inc. | Projectile trajectory control system |
| CN205034355U (en) * | 2015-10-12 | 2016-02-17 | 李爱兵 | Posture adjustment device is retrieved in rocket propulsion cabin |
| CN106225605A (en) * | 2016-07-05 | 2016-12-14 | 李卓 | A kind of recovery system of multistep rocket |
| CN206269681U (en) * | 2016-12-15 | 2017-06-20 | 福州幻科机电科技有限公司 | Escape tower radome fairing booster rocket with the remote control hang gliding tail vane wing |
-
2016
- 2016-12-15 CN CN201611157918.2A patent/CN106500550A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1107114A (en) * | 1993-01-14 | 1995-08-23 | 埃尔诺航空技术有限公司 | Apparatus for controling |
| US20080061188A1 (en) * | 2005-09-09 | 2008-03-13 | General Dynamics Ordnance And Tactical Systems, Inc. | Projectile trajectory control system |
| CN205034355U (en) * | 2015-10-12 | 2016-02-17 | 李爱兵 | Posture adjustment device is retrieved in rocket propulsion cabin |
| CN106225605A (en) * | 2016-07-05 | 2016-12-14 | 李卓 | A kind of recovery system of multistep rocket |
| CN206269681U (en) * | 2016-12-15 | 2017-06-20 | 福州幻科机电科技有限公司 | Escape tower radome fairing booster rocket with the remote control hang gliding tail vane wing |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN107152896A (en) * | 2017-05-26 | 2017-09-12 | 合肥凯石投资咨询有限公司 | A kind of recyclable main boost motor |
| CN107192305A (en) * | 2017-05-26 | 2017-09-22 | 合肥凯石投资咨询有限公司 | A kind of recyclable auxiliary boost motor |
| CN107152896B (en) * | 2017-05-26 | 2019-01-29 | 合肥凯石投资咨询有限公司 | A kind of recyclable main boost motor |
| CN107300343A (en) * | 2017-06-12 | 2017-10-27 | 合肥凯石投资咨询有限公司 | A kind of recyclable boost motor |
| CN107300343B (en) * | 2017-06-12 | 2018-11-13 | 合肥凯石投资咨询有限公司 | A kind of recyclable boost motor |
| CN112124625A (en) * | 2020-08-27 | 2020-12-25 | 上海宇航系统工程研究所 | Ship and rocket integrated shuttle aircraft and flight control method |
| CN114963867A (en) * | 2022-06-16 | 2022-08-30 | 陕西空天动力研究院有限公司 | Vacuum high-speed launching system of combined power rocket and launching and recovering method thereof |
| CN114963867B (en) * | 2022-06-16 | 2023-12-29 | 陕西空天动力研究院有限公司 | Vacuum high-speed emission system of combined power rocket and emission and recovery method thereof |
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| C06 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20170315 |
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| WD01 | Invention patent application deemed withdrawn after publication |