CN201463737U - Low-resistance bullet - Google Patents

Low-resistance bullet Download PDF

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Publication number
CN201463737U
CN201463737U CN2009200917848U CN200920091784U CN201463737U CN 201463737 U CN201463737 U CN 201463737U CN 2009200917848 U CN2009200917848 U CN 2009200917848U CN 200920091784 U CN200920091784 U CN 200920091784U CN 201463737 U CN201463737 U CN 201463737U
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CN
China
Prior art keywords
bullet
low
afterbody
holder
lower resistance
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
Application number
CN2009200917848U
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Chinese (zh)
Inventor
赵泽晨
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to CN2009200917848U priority Critical patent/CN201463737U/en
Application granted granted Critical
Publication of CN201463737U publication Critical patent/CN201463737U/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)

Abstract

A low-resistant bullet belongs to the field of ammunition used by weapon. An existing bullet head has a flat-bottom bullet tail, and the structure causes comparatively large flight resistance and reduces flight performance of the bullet head. The low-resistant bullet meets the principle of aerodynamics by adopting a pointed bullet tail, and ensures that gunpowder gas can effectively act on the bullet and produce enough thrust by additionally arranging a separated sabot, thereby improving flight performance of the bullet. The low-resistance bullet also has the advantages of simple structure, low cost and the like, and is mainly adaptable to bullets used by light weapons.

Description

The lower resistance bullet
Technical field
The utility model relates to a kind of weapons and ammunitions, particularly relates to a kind of bullet that can reduce flight resistance.
Background technology
Present employed bullet bullet afterbody is flat shape substantially, and adopting this structure mainly is the propulsive efficiency of powder gases in order to improve bullet and to move in gun barrel.But this structure can make bullet produce bigger eddy resistance when high-speed flight, influences the flying quality of bullet.
The utility model content
Technical problem to be solved in the utility model is the defective that overcomes above-mentioned prior art, and a kind of bullet that can reduce flight resistance is provided, and improves the flying quality of bullet.
The lower resistance bullet comprises bullet, shell case, the fire in a stove before fuel is added, propellant powder, it is characterized in that: the head of bullet and afterbody are pointed; The bullet afterbody is equipped with at least two bullet holders.
Between described bullet head and the afterbody cylindrical section is arranged.
Described bullet holder inner surface and bullet afterbody fit tightly.
Described bullet depend on short round end to end the end place be concave panel.
The nonmetallic materials manufacturing is adopted in described bullet holder.
During the bullet emission, powder gases at first acts on the bullet holder.Because the bullet holder is subjected to the constraint of gun barrel wall in gun barrel, so the bullet holder can't break away from bullet, can only promote bullet and advance.When gun barrel was flown away from bullet and bullet holder, the bullet holder lost constraint, cooperated at centrifugal force, air drag, with bullet under the acting in conjunction of the external force such as component that the inclined-plane produces, and separated with bullet, and bullet then continues flight separately.
The utility model compared with prior art has the following advantages and good effect: because the bullet afterbody has adopted sharp structure, effectively reduce the eddy resistance that produces in-flight, improved the flying quality of bullet.The application of separate type bullet holder, but guaranteed that the powder gases useful effect is in bullet and produce enough thrust.The utility model is simple in structure, and is with low cost, is adapted to be mounted within on the various bullets to use.
Description of drawings
Fig. 1 is a schematic diagram of the present utility model
Fig. 2 is the structural representation of a kind of embodiment bullet of the utility model holder
Among the figure: 1, bullet 2, bullet holder 3, shell case 4, propellant powder 5, the fire in a stove before fuel is added
The specific embodiment
The lower resistance bullet comprises bullet 1, bullet holder 2, shell case 3, propellant powder 4, the fire in a stove before fuel is added 5, and the head of bullet 1 and afterbody are pointed, between a cylindrical section is arranged.The bullet afterbody is equipped with at least two bullet holders 2, forms an approximate circle cylinder.Bullet holder 2 is a concave panel near bullet tail end place, and bullet holder 2 inner surfaces and bullet 1 afterbody fit tightly.
During the bullet emission, powder gases at first acts on bullet holder 2. because bullet holder 2 is subjected to the constraint of gun barrel wall in gun barrel, therefore bullet holder 2 can't break away from bullet 1, can only promote bullet 1 advances. when gun barrel is flown away from bullet 1 and bullet holder 2, bullet holder 2 loses constraint, at centrifugal force, air drag, cooperate with bullet under the acting in conjunction of the external force such as component that the inclined-plane produces, separate with bullet 1,1 of bullet continues flight separately. because the head and the afterbody of bullet 1 are pointed, the aerodynamic principle, reduce the eddy resistance of bullet 1, improved the serviceability of ammunition.
Bullet holder 2 can be adopted the nonmetallic materials manufacturing.Because nonmetallic materials are easily deformable, can play certain sealing function, further reduce the leakage of powder gases.

Claims (5)

1. the lower resistance bullet comprises bullet, shell case, the fire in a stove before fuel is added, propellant powder, it is characterized in that: the head of bullet and afterbody are pointed; The bullet afterbody is equipped with at least two bullet holders.
2. lower resistance bullet according to claim 1 is characterized in that: a cylindrical section is arranged between bullet head and the afterbody.
3. lower resistance bullet according to claim 1 is characterized in that: bullet holder inner surface and bullet afterbody fit tightly.
4. lower resistance bullet according to claim 1 is characterized in that: bullet depend on short round end to end the end place be concave panel.
5. lower resistance bullet according to claim 1 is characterized in that: the nonmetallic materials manufacturing is adopted in the bullet holder.
CN2009200917848U 2009-06-10 2009-06-10 Low-resistance bullet Expired - Fee Related CN201463737U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009200917848U CN201463737U (en) 2009-06-10 2009-06-10 Low-resistance bullet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009200917848U CN201463737U (en) 2009-06-10 2009-06-10 Low-resistance bullet

Publications (1)

Publication Number Publication Date
CN201463737U true CN201463737U (en) 2010-05-12

Family

ID=42391088

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009200917848U Expired - Fee Related CN201463737U (en) 2009-06-10 2009-06-10 Low-resistance bullet

Country Status (1)

Country Link
CN (1) CN201463737U (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107238331A (en) * 2017-07-27 2017-10-10 董兰田 Biphase rectification bullet shells
WO2022112632A1 (en) * 2020-11-30 2022-06-02 Viera Leon Pedro Aerodynamic flying projectile

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107238331A (en) * 2017-07-27 2017-10-10 董兰田 Biphase rectification bullet shells
WO2022112632A1 (en) * 2020-11-30 2022-06-02 Viera Leon Pedro Aerodynamic flying projectile

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20100512

Termination date: 20120610