JPS60211296A - Weapon, which can be aimed freely, for aircraft - Google Patents
Weapon, which can be aimed freely, for aircraftInfo
- Publication number
- JPS60211296A JPS60211296A JP22562284A JP22562284A JPS60211296A JP S60211296 A JPS60211296 A JP S60211296A JP 22562284 A JP22562284 A JP 22562284A JP 22562284 A JP22562284 A JP 22562284A JP S60211296 A JPS60211296 A JP S60211296A
- Authority
- JP
- Japan
- Prior art keywords
- weapon
- turret
- aircraft
- ammunition
- axis
- 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.)
- Granted
Links
- 239000004744 fabric Substances 0.000 claims 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 230000010354 integration Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
- B64D7/02—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms
- B64D7/06—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft the armaments being firearms movably mounted
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A23/00—Gun mountings, e.g. on vehicles; Disposition of guns on vehicles
- F41A23/24—Turret gun mountings
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A27/00—Gun mountings permitting traversing or elevating movement, e.g. gun carriages
- F41A27/06—Mechanical systems
- F41A27/18—Mechanical systems for gun turrets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A9/00—Feeding or loading of ammunition; Magazines; Guiding means for the extracting of cartridges
- F41A9/29—Feeding of belted ammunition
- F41A9/34—Feeding of belted ammunition from magazines
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Joints Allowing Movement (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Toys (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
【発明の詳細な説明】
（イ）発明の技術分野
本発明は、航空機、特にヘリコプタ−のための照準自在
な武器に関する。DETAILED DESCRIPTION OF THE INVENTION (a) Technical Field of the Invention The present invention relates to a sightable weapon for aircraft, particularly helicopters.
（０）技術の背景
単に非制限的例として以下に説明する戦術航空機、特に
戦闘ヘリコプタ−には、公知のように、操縦席の下もし
くは他の適当な個所に装着された砲塔上に、多様な高さ
で取り付けられた武器、通常速射砲、より成る照準自在
な武器が装着され、前記砲塔は、通常前記砲塔に対して
前記武器の旋回軸に垂直な自軸周囲で旋回するようにな
っている。(0) BACKGROUND OF THE TECHNOLOGY Tactical aircraft, particularly combat helicopters, as described below by way of non-limiting example only, are equipped with a turret mounted on a turret mounted under the cockpit or other suitable location, as is known in the art. mounted with a freely aimable weapon consisting of a weapon mounted at a height, usually a rapid-fire cannon, said turret being adapted to pivot about its own axis, usually perpendicular to the axis of rotation of said weapon relative to said turret; ing.
（ハ）従来技術と問題点
戦闘ヘリコプタ−では、前記砲塔は、一般に、操縦席前
部の下に装着され、武器自身は、砲塔より隔置され且つ
ヘリコプタ−の胴体と一体連結されるか又は組み込まれ
た弾薬ボックスから弾薬の ゛供給を受ける。(C) Prior Art and Problems In combat helicopters, the turret is generally mounted under the front of the cockpit, and the weapon itself is either spaced apart from the turret and integrally connected to the body of the helicopter, or Receives ammunition supply from built-in ammunition box.
これらの装備はいずれも、第一に戦闘ヘリコプタ−の有
効スペースがほぼ全体的に不足するという点から配置の
面で、第二に弾薬の供給の面で不具合を有する。前記弾
薬ポ・ノクスは武器から一定距離、離れていることから
、可視性の弾薬帯（ｌｉｎｅ）で武器と連結されること
が必要となり、このことは常に、砲塔の自軸を支点とす
る可動範囲を制限する。All of these equipment have deficiencies, firstly in terms of placement due to the almost total lack of usable space on combat helicopters, and secondly in terms of ammunition supply. Since the ammunition po-nox is at a certain distance from the weapon, it is necessary to connect it to the weapon with a visible ammunition line, which always means that it is movable around the axis of the turret. Limit the scope.
さらに、前記弾薬ボックスと砲塔とをヘリコプタ−上に
装着して三者を連結する作業は、非常に時間がかかり、
そのためヘリコプタ−自身の作業能力が損なわれること
にもなる。Furthermore, the work of mounting the ammunition box and turret on the helicopter and connecting the three is extremely time consuming;
This also impairs the helicopter's own working ability.
仁）発明の目的
本発明の目的は、本質的に上記の欠点を全く含まない照
準自在な武器を提供することにある。OBJECTS OF THE INVENTION The object of the invention is to provide an aimable weapon which essentially does not have any of the above-mentioned drawbacks.
０）発明の構成
この目的で、本発明は航空機、特にヘリコプタ−用の照
準自在な武器（ｔｒａｉｎａｂｌｅ ｗｅａｐｏｎ）に
して、前記航空機胴体の外面にそれに対して第−軸を支
点に旋回出来るよう取り付けられた砲塔と、前記砲塔上
にそれに対して第二軸を支点に揺動するよう取り付けら
れた武器と、弾薬ボックスとを含み、前記武器は、前記
弾薬ボックスが前記砲塔と一体結合され、後者と一緒に
前記第一軸周囲を旋回するようにされている。0) Structure of the Invention For this purpose, the present invention provides a trainable weapon for an aircraft, especially a helicopter, which is mounted on the outer surface of the aircraft fuselage so as to be pivotable about a second axis relative to it. a turret, a weapon mounted on the turret so as to swing about a second axis relative to the turret, and an ammunition box, wherein the ammunition box is integrally connected to the turret, They are configured to rotate together around the first axis.
（へ）発明の実施例 以下に、本発明の実施例を図面により説明する。(f) Examples of the invention Embodiments of the present invention will be described below with reference to the drawings.
図に於て、ｌは特にヘリコプタ−（図示せず）への組込
みに適した照準自在な武器である。In the figure, l is a sightable weapon particularly suitable for integration into a helicopter (not shown).
武器１は、本質的に台形で、上部に内歯を有する輪歯車
３を装着した一つのボックス体より成る砲塔２を含んで
いる。作動時には、輪歯車３が、前記ヘリコプタ−上に
装着されて砲塔２を輪歯車３の軸５周囲で旋回させるべ
く働く作動装置（図示せず）上の小歯車４と噛み合う。The weapon 1 comprises a turret 2 which is essentially trapezoidal and consists of a box body fitted with an internally toothed ring gear 3 at the top. In operation, the ring gear 3 meshes with a pinion 4 on an actuator (not shown) mounted on the helicopter and serving to pivot the turret 2 about the axis 5 of the ring gear 3.
砲塔２の細い方のベース端には、速射砲８の後部用７を
収納するスロット６が設けられ、速射砲８は、砲塔２に
対して、軸５と本質的に直交する軸９の周囲で揺動する
ようになっている。The slender base end of the turret 2 is provided with a slot 6 for receiving the rear part 7 of a rapid-fire gun 8, which is arranged relative to the turret 2 around an axis 9 essentially orthogonal to the axis 5. It is designed to oscillate.
砲塔２の大きい方のベース端には、弾薬ボックスｌＯが
着脱自在に装着され、その出口側は、供給帯１１によっ
て弾薬１３用の入口１２と連結され、前記入口１２は、
速射砲８の点火室（図示せず）に隣接する胴７の側部に
形成されている。An ammunition box lO is detachably mounted on the larger base end of the turret 2, the outlet side of which is connected to an inlet 12 for ammunition 13 by a supply belt 11, said inlet 12
It is formed on the side of the barrel 7 adjacent to the ignition chamber (not shown) of the rapid-fire cannon 8 .
従って、照準自在な武器ｌは、基本的には砲塔２と速射
砲８と弾薬ボックス１０とから成り、これらは互いに一
体となって一つの非常にコンパクトな装置を構成し、緊
密装着連結具（ｆａｓｔ−ｆｉｔｃｏｎｐｌｉｎｇｓ
） （図示せず）を用いてヘリコプタ−に簡単に装着す
ることが出来る。さらに、武器１上の弾薬ボックス１０
は、速射砲８と隣接して直接砲塔２に取り付けられてい
るので、ヘリコプタ−内でスペースをとらないばかりか
、弾薬ボックス１０及び砲塔２と共に移動するよう設計
された供給帯１１によって、前記弾薬ボックス１０と速
射砲８とが連結されていることから、砲塔２のその自軸
５周囲の走行を何ら制限しない。The aimable weapon l therefore basically consists of a turret 2, a rapid-fire cannon 8 and an ammunition box 10, which together constitute one very compact device, with a tight mounting connection ( fast-fit components
) (not shown) can be easily attached to a helicopter. In addition, ammunition box 10 on weapon 1
Since it is mounted directly on the turret 2 adjacent to the rapid-fire gun 8, it not only takes up less space inside the helicopter, but also has a supply belt 11 designed to move with the ammunition box 10 and the turret 2, which allows said ammunition to be Since the box 10 and the rapid-fire cannon 8 are connected, there is no restriction on the movement of the turret 2 around its own axis 5.
尚、上記実施例では速射砲について説明したが、これ以
外のものであってもよい。Incidentally, in the above embodiment, a rapid-fire cannon was described, but other types may be used.
（ト）発明の詳細
な説明した如く、本発明によれば、航空機特ニヘリコプ
ターに簡単に装着することができると共に、設置スペー
スが小さくてすむ。また、弾薬の供給が確実に行なえる
。砲塔の可動範囲を制限しない等の利点を有する。(G) As described in detail, according to the present invention, it can be easily mounted on an aircraft, especially a helicopter, and requires only a small installation space. In addition, the supply of ammunition can be ensured. It has the advantage of not restricting the range of movement of the turret.
図面は本発明の代表的な実°施例を示す斜視図である。
１・・・武器、２・・・砲塔、３・・・輪歯車、４・・
・小歯車、５．９・・・軸、８・・・速射砲、１０・・
・弾薬ボックス、１１・・・供給帯。
特許出願人 コストルヂオニ アエロナウティヶジオバ
ソニ アグスタ エソセ・The drawing is a perspective view showing a typical embodiment of the invention. 1... Weapon, 2... Turret, 3... Ring gear, 4...
・Small gear, 5.9...shaft, 8...quick fire gun, 10...
-Ammo box, 11...supply zone. Patent Applicant Costruzioni Aeronauti Gagiobasoni Agusta Esoce
Claims (3)
（ｔｒａｉｎａｂｌｅ ｗｅａｐｏｎ）に於て、前記航
空機胴体の外面にそれに対し第一軸周囲を旋回するよう
装着された砲塔と、前記砲塔上にそれに対して第二軸周
囲を揺動するよう装着された武器（ｉｌｅａｐｏｎ）と
、弾薬ボックスとを含み、且つ、前記弾薬ボックスが前
記砲塔と一体連結され、後者と共に前記第一軸周囲を旋
回するようにされていることを特徴とする前記武器。(1) In a trainable weapon for an aircraft, especially a helicopter, a turret mounted on the outer surface of the aircraft fuselage so as to rotate around a first axis relative to the aircraft fuselage, and a turret mounted on the turret to rotate about a first axis relative to the outer surface of the aircraft fuselage; and an ammunition box, the ammunition box being integrally connected to the turret and pivoting together with the latter about the first axis. The weapon characterized in that:
自在な武器の反対側に配置されていることを特徴とする
特許請求の範囲第１項記載の航空機用照準自在な武器。2. A sightable aircraft weapon according to claim 1, wherein the ammunition box is located on the opposite side of the sightable weapon with respect to the turret.
記武器に連結していることを特徴とする特許請求の範囲
第１項又は第２−項記載の航空機用照準自在な武器。(3) A sightable aircraft weapon according to claim 1 or claim 2, characterized in that an ammunition box is connected to the weapon via an outer cloth that supplies ammunition.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| IT5386183U IT8353861V0 (en) | 1983-10-26 | 1983-10-26 | BRANDABLE WEAPON FOR AIRCRAFTS IN PARTICULAR HELICOPTERS |
| IT53861-B/83 | 1983-10-26 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS60211296A true JPS60211296A (en) | 1985-10-23 |
| JPH057640B2 JPH057640B2 (en) | 1993-01-29 |
Family
ID=11285633
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP22562284A Granted JPS60211296A (en) | 1983-10-26 | 1984-10-26 | Weapon, which can be aimed freely, for aircraft |
Country Status (5)
| Country | Link |
|---|---|
| JP (1) | JPS60211296A (en) |
| DE (1) | DE3438816A1 (en) |
| FR (1) | FR2554222B1 (en) |
| GB (1) | GB2149069B (en) |
| IT (1) | IT8353861V0 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3664960D1 (en) * | 1985-12-31 | 1989-09-14 | Lucas Ind Plc | Feed system for linked ammunition |
| US5206454A (en) * | 1992-03-16 | 1993-04-27 | Sanderson Paul H | Externally mounted aircraft ammunition magazine box structure |
| US5458045A (en) * | 1994-03-25 | 1995-10-17 | Sanderson; Paul H. | Feed chute-to-gun ammunition belt guide adapter for machine guns |
| IT1284722B1 (it) * | 1996-08-02 | 1998-05-21 | Augusta Spa | Dispositivo di alimentazione di munizioni ad un'arma imbarcata su un aeromobile, ed aeromobile provvisto di tale dispositivo. |
| IL220182A (en) * | 2012-06-05 | 2016-12-29 | Rafael Advanced Defense Systems Ltd | Belt/metallic link chain loaded ammunition feeder in remote controlled weapon station |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5875697A (en) * | 1981-08-17 | 1983-05-07 | ゼネラル・エレクトリツク・カンパニイ | Gun carriage |
Family Cites Families (11)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR798815A (en) * | 1935-02-27 | 1936-05-27 | Liore & Olivier Ets | Adjustable cupola and device for its control, more particularly for firing stations on board aircraft |
| GB559478A (en) * | 1937-04-17 | 1938-12-07 | Supermarine Aviat Works Vicker | Improvements in or relating to mountings for guns in aircraft |
| US2414608A (en) * | 1941-05-05 | 1947-01-21 | Bendix Aviat Corp | Gun turret |
| US2379185A (en) * | 1941-07-09 | 1945-06-26 | Bendix Aviat Corp | Gun feed mechanism |
| GB588138A (en) * | 1942-02-04 | 1947-05-15 | Bendix Aviat Corp | Improvements in gun turrets |
| GB574451A (en) * | 1942-02-24 | 1946-01-07 | Boulton Aircraft Ltd | Improvements in and relating to aircraft gun turrets |
| GB580735A (en) * | 1943-03-25 | 1946-09-18 | Bristol Aeroplane Co Ltd | Improvements in or relating to power operated gun turrets for aircraft |
| GB585243A (en) * | 1944-11-03 | 1947-02-03 | John Dudley North | Improvements in and relating to gun turrets |
| DE1940771A1 (en) * | 1968-09-16 | 1970-05-06 | United Aircraft Corp | Aircraft, especially helicopters with rotating gun turrets |
| DE2028992C1 (en) * | 1970-06-12 | 1978-04-27 | Thyssen Industrie Ag, 4300 Essen | Arrangement of a barrel weapon in a stabilized gun turret |
| DE2349184C1 (en) * | 1973-10-01 | 1985-10-10 | Thyssen Industrie Ag, 4300 Essen | Gun mount for a crest-mounted gun of an armored vehicle |
-
1983
- 1983-10-26 IT IT5386183U patent/IT8353861V0/en unknown
-
1984
- 1984-10-11 GB GB08425729A patent/GB2149069B/en not_active Expired
- 1984-10-22 FR FR8416122A patent/FR2554222B1/en not_active Expired
- 1984-10-23 DE DE19843438816 patent/DE3438816A1/en not_active Withdrawn
- 1984-10-26 JP JP22562284A patent/JPS60211296A/en active Granted
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5875697A (en) * | 1981-08-17 | 1983-05-07 | ゼネラル・エレクトリツク・カンパニイ | Gun carriage |
Also Published As
| Publication number | Publication date |
|---|---|
| GB2149069B (en) | 1987-09-09 |
| IT8353861V0 (en) | 1983-10-26 |
| JPH057640B2 (en) | 1993-01-29 |
| FR2554222A1 (en) | 1985-05-03 |
| DE3438816A1 (en) | 1985-05-09 |
| FR2554222B1 (en) | 1989-04-21 |
| GB8425729D0 (en) | 1984-11-14 |
| GB2149069A (en) | 1985-06-05 |
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