CN105366052A - Rocket-propelled dropping top nest for stealth aircraft - Google Patents
Rocket-propelled dropping top nest for stealth aircraft Download PDFInfo
- Publication number
- CN105366052A CN105366052A CN201510835968.0A CN201510835968A CN105366052A CN 105366052 A CN105366052 A CN 105366052A CN 201510835968 A CN201510835968 A CN 201510835968A CN 105366052 A CN105366052 A CN 105366052A
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- CN
- China
- Prior art keywords
- face
- fuselage
- aircraft
- crossing
- nest
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F1/00—Ground or aircraft-carrier-deck installations
- B64F1/04—Ground or aircraft-carrier-deck installations for launching aircraft
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U20/00—Constructional aspects of UAVs
- B64U20/10—Constructional aspects of UAVs for stealth, e.g. reduction of cross-section detectable by radars
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64U—UNMANNED AERIAL VEHICLES [UAV]; EQUIPMENT THEREFOR
- B64U70/00—Launching, take-off or landing arrangements
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Mechanical Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Toys (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The present invention discloses a rocket-propelled dropping top nest for a stealth aircraft, and relates to the technical filed of aviation. The rocket-propelled dropping top nest for the stealth aircraft contains a first top surface (4), a second top surface (7), a first side surface (5), a second side surface (8) and a fuselage surface (6). The first top surface (4) and the second top surface (7) intersect to form a top edge (47); the first top surface (4) intersects with the fuselage surface (6) to form a first side top edge (46); the first side top edge (46) is parallel with the first leading edge (11); the second top surface (7) and the fuselage surface (6) form a second top edge (76); the second top edge (76) and a second leading edge (12) are in parallel; the first side surface (5) respectively intersects with the first top surface (4) and the fuselage surface (6); and the second side surface (8) respectively intersects with the second top surface (7) and the fuselage surface (6). The present invention has the advantage of enhancing the stealth performance of the aircraft.
Description
Technical field
The present invention relates to technical field of aerospace, the rocket assist being specifically related to a kind of stealthy aircraft comes off top nest.
Background technology
Rocket booster dropping mechanism is as the key of unmanned aerial plane launching system, and Main Function is: one is ensure that booster does not rock in emission process; Two be launch at the end of make booster self falling.
All kinds of rocket booster dropping mechanisms that in prior art, common unmanned plane is applied at present all do not carry out high stealthing design, like this, when being applied to above high stealthy unmanned plane, the serious Stealth Fighter that have impact on unmanned plane, therefore not easily uses on the stealthy unmanned plane of height.
Summary of the invention
The rocket assist that the object of this invention is to provide a kind of stealthy aircraft comes off top nest, to solve in background technology the problem be not easily applied in by existing dropping mechanism on high stealthy unmanned plane.
The technical solution adopted in the present invention is: provide a kind of rocket assist of stealthy aircraft to come off top nest, comprise the first end face, the second end face, the first side, the second side and fuselage face, wherein, described first end face is crossing with the second end face forms top margin, described first end face formation first crossing with fuselage face side top margin, and the first side top margin is parallel with rim before first; Described second end face and fuselage face form the second top margin, and the second top margin is parallel with rim before second; Described first side is crossing with described first end face and fuselage face respectively; Described second side is crossing with described second end face and fuselage face respectively.
Preferably, described first side is crossing with fuselage face forms first side, and described second side is crossing with fuselage face forms second side, and described first side and second side are parallel to each other.
Preferably, described first end face, the second end face, the first side and the second side are all vertical with fuselage face.
Preferably, described fuselage face has trailing edge, the degree of depth of described top nest is deepened to the direction of top margin gradually from trailing edge.
Preferably, described trailing edge is to aircraft fuselage rounding off.
Beneficial effect of the present invention: described first end face is crossing with the second end face forms top margin, described first end face formation first crossing with fuselage face side top margin, and the first side top margin is parallel with rim before first; Described second end face and fuselage face form the second top margin, and the second top margin is parallel with rim before second; Top nest to the reflection angle of the reflection angle of acquisition radar and aircraft always, not easily by radar detection, enhances the Stealth Fighter of aircraft.
Accompanying drawing explanation
Fig. 1 be the rocket assist of stealthy aircraft of the present invention come off top nest schematic perspective view;
Fig. 2 is that the rocket assist of the stealthy aircraft shown in Fig. 1 comes off top nest birds-eye view on board the aircraft.
Wherein, 1-aircraft, 2-comes off top nest, 4-first end face, 5-first side, 6-fuselage face, 7-second end face, 8-second side, rim before 11-first, rim before 12-second, 46-first side top margin, 47-top margin, 56-first side, 61-trailing edge, 76-second top margin, 86-second side.
Detailed description of the invention
For making object of the invention process, technical scheme and advantage clearly, below in conjunction with the accompanying drawing in the embodiment of the present invention, the technical scheme in the embodiment of the present invention is further described in more detail.In the accompanying drawings, same or similar label represents same or similar element or has element that is identical or similar functions from start to finish.Described embodiment is the present invention's part embodiment, instead of whole embodiments.Be exemplary below by the embodiment be described with reference to the drawings, be intended to for explaining the present invention, and can not limitation of the present invention be interpreted as.Based on the embodiment in the present invention, those of ordinary skill in the art, not making the every other embodiment obtained under creative work prerequisite, belong to the scope of protection of the invention.Below in conjunction with accompanying drawing, embodiments of the invention are described in detail.
In describing the invention; it will be appreciated that; term " " center ", " longitudinal direction ", " transverse direction ", "front", "rear", "left", "right", " vertically ", " level ", " top ", " end " " interior ", " outward " etc. instruction orientation or position relationship be based on orientation shown in the drawings or position relationship; be only the present invention for convenience of description and simplified characterization; instead of instruction or imply indication device or element must have specific orientation, with specific azimuth configuration and operation, therefore can not be interpreted as limiting the scope of the invention.
As shown in Figure 1 and Figure 2, a kind of rocket assist of stealthy aircraft comes off top nest, comprise the first end face 4, second end face 7, first side 8, side 5, second and fuselage face 6, wherein, first end face 4 is crossing with the second end face 7 forms top margin 47, first end face 4 formation first crossing with fuselage face 6 side top margin 46, and the first side top margin 46 is parallel with rim before first 11; Second end face 7 forms the second top margin 76 with fuselage face 6, and the second top margin 76 is parallel with rim before second 12; First side 5 is crossing with the first end face 4 and fuselage face 6 respectively; Second side 8 is crossing with described second end face 7 and fuselage face 6 respectively.
In the present embodiment, the first side 5 is crossing with fuselage face 6 forms that side 8, first side 56, second is crossing with fuselage face 6 forms second side 86, and first side 56 and second side 86 are parallel to each other, and are parallel to navigation direction.
First end face 4, second end face 7, first side 5 and the second side 8 all vertical with fuselage face 6.The top power of line direction before booster can be transmitted to aircraft by the first end face 4 and the second end face 7, first side 5 and the second side 8 can limit booster front end push rod and there will not be swing, meanwhile, booster can by fuselage face 6 to the top power that aircraft transmission upwards flies up.
Fuselage face 6 has trailing edge 61, the degree of depth of top nest is deepened gradually from the direction of trailing edge 61 to top margin 47.Its advantage is: namely booster front end push rod firmly can be fixed, facilitate again coming off of booster push rod.
Trailing edge 61 is to aircraft fuselage rounding off.Be conducive to the Stealth Fighter improving aircraft.
Finally it is to be noted: above embodiment only in order to technical scheme of the present invention to be described, is not intended to limit.Although with reference to previous embodiment to invention has been detailed description, those of ordinary skill in the art is to be understood that: it still can be modified to the technical scheme described in foregoing embodiments, or carries out equivalent replacement to wherein portion of techniques feature; And these amendments or replacement, do not make the essence of appropriate technical solution depart from the spirit and scope of various embodiments of the present invention technical scheme.
Claims (5)
1. the rocket assist of a stealthy aircraft comes off top nest, it is characterized in that: comprise the first end face (4), the second end face (7), the first side (5), the second side (8) and fuselage face (6), wherein
Described first end face (4) is crossing with the second end face (7) forms top margin (47), described first end face (4) and fuselage face (6) crossing formation first side top margin (46), and the first side top margin (46) is parallel with rim before first (11); Described second end face (7) and fuselage face (6) form the second top margin (76), and the second top margin (76) is parallel with rim before second (12);
Described first side (5) is crossing with described first end face (4) and fuselage face (6) respectively;
Described second side (8) is crossing with described second end face (7) and fuselage face (6) respectively.
2. the rocket assist of stealthy aircraft as claimed in claim 1 comes off top nest, it is characterized in that: described first side (5) is crossing with fuselage face (6) forms first side (56), described second side (8) is crossing with fuselage face (6) forms second side (86), and described first side (56) and second side (86) are parallel to each other.
3. the rocket assist of stealthy aircraft as claimed in claim 1 comes off top nest, it is characterized in that: described first end face (4), the second end face (7), the first side (5) and the second side (8) are all vertical with fuselage face (6).
4. the rocket assist of stealthy aircraft as claimed in claim 1 comes off top nest, it is characterized in that: described fuselage face (6) has trailing edge (61), the degree of depth of described top nest is deepened to the direction of top margin (47) gradually from trailing edge (61).
5. the rocket assist of stealthy aircraft as claimed in claim 4 comes off top nest, it is characterized in that: described trailing edge (61) is to aircraft fuselage rounding off.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510835968.0A CN105366052A (en) | 2015-11-25 | 2015-11-25 | Rocket-propelled dropping top nest for stealth aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510835968.0A CN105366052A (en) | 2015-11-25 | 2015-11-25 | Rocket-propelled dropping top nest for stealth aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105366052A true CN105366052A (en) | 2016-03-02 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510835968.0A Pending CN105366052A (en) | 2015-11-25 | 2015-11-25 | Rocket-propelled dropping top nest for stealth aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105366052A (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4471923A (en) * | 1981-08-22 | 1984-09-18 | Vereinigte Flugtechnische Werke Mbb | Unmanned aircraft |
| US4721271A (en) * | 1985-02-14 | 1988-01-26 | The Boeing Company | Devices and method for rocket booster vectoring to provide stability augmentation during a booster launch phase |
| RU2233417C2 (en) * | 2002-08-12 | 2004-07-27 | Открытое акционерное общество "Завод им. В.А.Дегтярёва" | Practice training device |
| US20050230517A1 (en) * | 2004-04-19 | 2005-10-20 | Teledyne Solutions, Inc. | Payload delivery vehicle and method |
| CN104590577A (en) * | 2014-12-25 | 2015-05-06 | 中国人民解放军总参谋部第六十研究所 | Unmanned aerial vehicle launch booster mounting base adjusting and installing platform and usage method thereof |
-
2015
- 2015-11-25 CN CN201510835968.0A patent/CN105366052A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4471923A (en) * | 1981-08-22 | 1984-09-18 | Vereinigte Flugtechnische Werke Mbb | Unmanned aircraft |
| US4721271A (en) * | 1985-02-14 | 1988-01-26 | The Boeing Company | Devices and method for rocket booster vectoring to provide stability augmentation during a booster launch phase |
| RU2233417C2 (en) * | 2002-08-12 | 2004-07-27 | Открытое акционерное общество "Завод им. В.А.Дегтярёва" | Practice training device |
| US20050230517A1 (en) * | 2004-04-19 | 2005-10-20 | Teledyne Solutions, Inc. | Payload delivery vehicle and method |
| CN104590577A (en) * | 2014-12-25 | 2015-05-06 | 中国人民解放军总参谋部第六十研究所 | Unmanned aerial vehicle launch booster mounting base adjusting and installing platform and usage method thereof |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
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| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160302 |