Launching an unmanned aerial vehicle using a hand-held weapon
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
B64F-001/04
B64C-039/02
출원번호
US-0187846
(2014-02-24)
등록번호
US-9611054
(2017-04-04)
발명자
/ 주소
Manasseh, Alexander D.
출원인 / 주소
AAI Corporation
대리인 / 주소
BainwoodHuang
인용정보
피인용 횟수 :
0인용 특허 :
16
초록▼
A technique is directed to launching an unmanned aerial vehicle (UAV). The technique involves attaching a UAV launcher to a hand-held weapon, and installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon. The technique further involves activating the hand-held
A technique is directed to launching an unmanned aerial vehicle (UAV). The technique involves attaching a UAV launcher to a hand-held weapon, and installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon. The technique further involves activating the hand-held weapon to launch the UAV into flight from the UAV launcher. Since a user already may be carrying the hand-held weapon for firing ammunition, the user simply needs to further carry the UAV launcher and the UAV which, in some situations, can be packaged into an easy-to-carry container such as a backpack, a carrying case, and so on.
대표청구항▼
1. A method of launching an unmanned aerial vehicle (UAV), the method comprising: attaching a UAV launcher to a hand-held weapon;installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon; andactivating the hand-held weapon to launch the UAV into flight from th
1. A method of launching an unmanned aerial vehicle (UAV), the method comprising: attaching a UAV launcher to a hand-held weapon;installing a UAV onto the UAV launcher while the UAV launcher is attached to the hand-held weapon; andactivating the hand-held weapon to launch the UAV into flight from the UAV launcher;wherein the hand-held weapon is a firearm including a firearm barrel which defines a firearm bore;wherein the UAV launcher includes a UAV launcher barrel which defines a launcher bore;wherein attaching the UAV launcher to the hand-held weapon includes: connecting the UAV launcher barrel to the firearm barrel, the firearm bore defined by the firearm barrel being aligned with the launcher bore when the UAV launcher barrel is connected to the firearm barrel;wherein connecting the UAV launcher barrel to the firearm barrel includes threading the UAV launcher barrel onto the firearm barrel;wherein the method further comprises: prior to activating the hand-held weapon, loading the firearm with a blank charge which is constructed and arranged to propel the UAV into flight from the UAV launcher in response to firing; andwherein installing the UAV onto the UAV launcher includes: fastening a first end of a projectile member to the UAV; andinserting a second end of the projectile member into the UAV launcher barrel, the second end of the projectile member being opposite the first end of the projective member;wherein the first end of the projectile member (i) has a first diameter which is larger than the UAV launcher barrel and (ii) fits into a cavity of the UAV; andwherein the second end of the projectile member (i) has a second diameter which is narrower than the first diameter and (ii) fits within the launcher bore defined by the UAV launcher barrel. 2. A method as in claim 1 wherein fastening the first end of the projectile member to the UAV includes: coupling the first end of the projectile member to the UAV such that the projectile member disconnects from the UAV after launching. 3. A method as in claim 1 wherein fastening the first end of the projectile member to the UAV includes: coupling the first end of the projectile member to the UAV such that the projectile member rotates relative to the UAV after launching. 4. A method as in claim 1 wherein fastening the first end of the projectile member to the UAV includes: engaging the first end of the projectile member within a cavity of the UAV to attach the projectile member to the UAV; andwherein inserting the second end of the projectile member into the UAV launcher barrel includes:after the projectile member is attached to the UAV, inserting the second end of the projectile member into the UAV launcher barrel through an open end of the UAV launcher barrel. 5. An unmanned aerial vehicle (UAV) launching assembly, comprising: a UAV launcher barrel having (i) a weapon attachment section which is constructed and arranged to attach to a hand-held weapon and (ii) a UAV interface section which is constructed and arranged to support a UAV and release the UAV in response to activation of the hand-held weapon while the weapon attachment section of the UAV launcher barrel is attached to the hand-held weapon, anda projectile member having a first end which fastens to the UAV, and a second end which inserts into the UAV interface section of the UAV launcher barrel, the second end being opposite the first end;wherein the hand-held weapon is a firearm including a firearm barrel which defines a firearm bore;wherein the UAV launcher barrel defines a launcher bore;wherein the launcher bore defined by the UAV launcher barrel coaxially aligns with the firearm bore defined by the firearm barrel when the UAV launcher barrel attaches to the firearm barrel;wherein the weapon attachment section of the UAV launcher barrel is constructed and arranged to thread onto the firearm barrel;wherein the first end of the projectile member (i) has a first diameter which is larger than the UAV launcher barrel and (ii) fits into a cavity of the UAV; andwherein the second end of the projectile member (i) has a second diameter which is narrower than the first diameter and (ii) fits within the launcher bore defined by the UAV launcher barrel. 6. A UAV launching assembly as in claim 5 wherein the UAV launcher barrel further includes a baffled section disposed between the weapon attachment section and the UAV interface section, the baffled section defining a set of baffles to suppress noise during firing of the firearm. 7. A UAV launching assembly as in claim 5 wherein the UAV launcher barrel further includes a muzzle break section disposed between the weapon attachment section and the UAV interface section, the muzzle break section controlling recoil of the firearm during firing of the firearm. 8. A UAV launching assembly as in claim 5, further comprising: a blank charge to be loaded into the firearm, the blank charge being constructed and arranged to propel the UAV into flight from the UAV launcher barrel in response to firing. 9. A UAV launching assembly as in claim 5, further comprising: a UAV base which attaches to the UAV launcher barrel, the UAV base being constructed and arranged to provide a resting surface on which the UAV sits prior to launch. 10. A UAV launching assembly as in claim 9 wherein the UAV base is in the form of a rail which is constructed and arranged to guide the UAV during launch. 11. A UAV launching assembly as in claim 5, further comprising: a blank charge to be loaded into the firearm, the blank charge being constructed and arranged to propel the UAV into flight from the UAV launcher barrel in response to firing; anda UAV base which attaches to the UAV launcher barrel, the UAV base being constructed and arranged to provide a resting surface on which the UAV sits prior to launch and while the projectile member is fastened to the UAV and inserted into the UAV interface section of the UAV launcher barrel. 12. A UAV launching assembly as in claim 5 wherein the projectile member is constructed and arranged to rotate relative to the UAV while the first end of the projectile member fits into the cavity of the UAV. 13. A UAV launching assembly as in claim 5 wherein the projectile member is constructed and arranged to rotate relative to the UAV launcher barrel during launch while absorbing rifling action imparted by the hand-held weapon. 14. A UAV launching assembly as in claim 5 wherein the projectile member is constructed and arranged to rotate relative to (i) the UAV launcher barrel and (ii) the UAV in response to rifling action imparted on the projectile member by firing of the hand-held weapon. 15. A UAV launching assembly as in claim 5, further comprising: a retainer which is disposed between the projectile member and the UAV prior to launching the UAV, the retainer being constructed and arranged to fasten the projectile member to the UAV prior to launching the UAV. 16. A UAV launching assembly as in claim 15 wherein the retainer is disposed within a groove defined by the UAV prior to launching the UAV. 17. An unmanned aerial vehicle (UAV) launching system, comprising: a hand-held weapon which is constructed and arranged to fire ammunition; anda UAV launch assembly which is constructed and arranged to launch a UAV, the UAV launch assembly including a UAV launcher barrel having (i) a weapon attachment section which is constructed and arranged to attach to the hand-held weapon, (ii) a UAV interface section which is constructed and arranged to support the UAV and release the UAV in response to activation of the hand-held weapon while the weapon attachment section of the UAV launcher barrel is attached to the hand-held weapon, and (iii) a projectile member having a first end which fastens to the UAV, and a second end which inserts into the UAV interface section of the UAV launcher barrel, the second end being opposite the first end;wherein the first end of the projectile member (i) has a first diameter which is larger than the UAV launcher barrel and (ii) fits into a cavity of the UAV; andwherein the second end of the projectile member (i) has a second diameter which is narrower than the first diameter and (ii) fits within a launcher bore defined by the UAV launcher barrel. 18. A UAV launching assembly as in claim 17 wherein the hand-held weapon is a firearm; and wherein the UAV launching assembly further includes: a blank charge to be loaded into the firearm in place of the ammunition, the blank charge being constructed and arranged to propel the UAV into flight from the UAV launcher barrel in response to firing while the weapon attachment section of the UAV launcher barrel is attached to the hand-held weapon; anda UAV base which attaches to the UAV launcher barrel, the UAV base being constructed and arranged to provide a resting surface on which the UAV sits prior to launch and while the projectile member is fastened to the UAV and inserted into the UAV interface section of the UAV launcher barrel. 19. A UAV launching system as in claim 18, further comprising: a UAV to be launched into flight from the UAV launcher barrel of the UAV launch assembly, the UAV being constructed and arranged to fasten to the projectile member. 20. A UAV launching system as in claim 17, further comprising: a retainer which is disposed between the projectile member and the UAV prior to launching the UAV, the retainer being constructed and arranged to fasten the projectile member to the UAV prior to launching the UAV, wherein the retainer is disposed within a groove defined by the UAV prior to launching the UAV. 21. An unmanned aerial vehicle (UAV) launching assembly, comprising: a UAV launcher barrel having (i) a weapon attachment section which is constructed and arranged to attach to a hand-held weapon and (ii) a UAV interface section which is constructed and arranged to support a UAV and release the UAV in response to activation of the hand-held weapon while the weapon attachment section of the UAV launcher barrel is attached to the hand-held weapon,a projectile member having a first end which fastens to the UAV, and a second end which inserts into the UAV interface section of the UAV launcher barrel, the second end being opposite the first end, anda retainer which is disposed between the projectile member and the UAV prior to launching the UAV, the retainer being constructed and arranged to fasten the projectile member to the UAV prior to launching the UAV, wherein the retainer is disposed within a groove defined by the UAV prior to launching the UAV;wherein the hand-held weapon is a firearm including a firearm barrel which defines a firearm bore;wherein the UAV launcher barrel defines a launcher bore;wherein the launcher bore defined by the UAV launcher barrel coaxially aligns with the firearm bore defined by the firearm barrel when the UAV launcher barrel attaches to the firearm barrel; andwherein the weapon attachment section of the UAV launcher barrel is constructed and arranged to thread onto the firearm barrel.
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이 특허에 인용된 특허 (16)
Manole, Leon R.; Logsdon, Jr., Ernest L.; Palathingal, Mohan J.; Sebasto, Anthony J., Gun launched hybrid projectile.
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