专利检索_ 枪的固定例如在车辆上;在车辆上枪的配置专利检索_ 枪的固定例如在车辆上;在车辆上枪的配置专利检索查询

子分类：

序号	专利名	申请号	申请日	公开（公告）号	公开（公告）日	发明人
101	Gun mount	US46561642	1942-11-14	US2415340A	1947-02-04	D ARDENNE WALTER H; JENKINTOWN MANOR; MEINEL WILLIAM J; DE VORE WEBER; WOLF ROBERT W

102	Gun turret seat	US42463741	1941-12-27	US2400812A	1946-05-21	ALFRED CORTE

103	Wing gun mount	US40275041	1941-07-17	US2331033A	1943-10-05	LA PORTE ROLAND M

104	Adjustable seat	US66116233	1933-03-16	US1933197A	1933-10-31	NEVILLE WALLIS BARNES

105	Carriage for antiaircraft guns	US23794527	1927-12-05	US1700902A	1929-02-05	LE PRIEUR YVES PAUL GASTON

106	Flexible gun mount	US63577123	1923-04-30	US1592490A	1926-07-13	INGLIS HENRY B

107	Mount for flexible synchronized guns	US55542222	1922-04-18	US1568089A	1926-01-05	RUSSELL HERBERT O; LEIGH PAULUS CHARLES

108	Brake control	US74085924	1924-09-30	US1567221A	1925-12-29	ZIMMERMAN HARRY C

109	Gun carriage	US52013221	1921-12-05	US1447085A	1923-02-27	JOYCE BRYAN P

110	Attachment for firearms	US24583118	1918-07-20	US1387308A	1921-08-09	POST TRUMAN W

111	Heavy artillery	US2386915	1915-04-26	US1375491A	1921-04-19	KENNEDY DOUGAN

112	Firearm	US22390518	1918-03-22	US1359726A	1920-11-23	JAMES MORRISON WILLIAM

113	Andrew noble	US413241D		US413241A	1889-10-22

114	Line-of-sight apparatus locking arrangement	US15311308	2014-05-15	US10151552B2	2018-12-11	Gustav Heurlin
The present invention regards a line-of-sight apparatus locking arrangement for demountably securing a line-of-sight apparatus to said arrangement, comprising a locking device for locking the apparatus to the arrangement comprising a handle member adapted for attachment to a rotation mechanism coupled to a translation mechanism adapted for, during maneuver of the locking device, converting rotational motion into translator motion, a pressing portion of the translation mechanism is provided for abutment against an abutment area of the apparatus. The translation mechanism comprising a resilient member provided for urging said pressing portion against the abutment area.
115	HIGH ALTITUDE SPACE LAUNCHER	US15869334	2018-01-12	US20180134414A1	2018-05-17	ABBAS ALIKOUHI
Disclosed is a high altitude space launcher system for transferring payloads from surface to orbit at a significantly lower cost than conventional rockets. It comprises a aerostat lifted one stage light gas gun operating in stratosphere that shoots rocket assisted projectiles containing payload at near orbital velocities to a low angle trajectory. Alternatively, to launch acceleration sensitive payloads such as astronauts the light gas gun is replaced with a muzzle loaded conventional gun that shoots a single stage rocket at a much lower velocity. The system is mostly static structure, attached to a tether-elevator that moors it to land or a ship and provided it with electricity and lifts the projectiles to the gun.
116	LINE-OF-SIGHT APPARATUS LOCKING ARRANGEMENT	US15311308	2014-05-15	US20170108305A1	2017-04-20	Gustav HEURLIN
The present invention regards a line-of-sight apparatus locking arrangement for demountable securing a line-of-sight apparatus to said arrangement, comprising a locking device for locking the apparatus to the arrangement comprises a handle member adapted for attachment to a rotation mechanism coupled to a translation mechanism adapted for, during manoeuvre of the locking device, converting rotational motion into translator motion, a pressing portion of the translation mechanism is provided for abutment against an abutment area of the apparatus. The translation mechanism comprises a resilient member provided for urging said pressing portion against the abutment area.
117	Shooting rests	US14953388	2015-11-29	US09557131B1	2017-01-31	Allan W. Antell
A shooting rest includes first and second poles each having a length, and a gun rest assembly for holding the first and second poles in selected angular relationships and at selected locations along the lengths thereof. The gun rest assembly includes a swivel connecting a first rest component mounted to the first pole for reciprocal movement along the length thereof, and a second rest component mounted to the second pole for reciprocal movement along the length thereof. A first clamp assembly is carried by the first rest component and a second clamp assembly is carried by the second rest component. The first and second clamp assemblies are configured for independently locking and releasing the respective first and second rest components relative to the respective first and second poles.
118	Shooting rests	US14078826	2013-11-13	US09200859B2	2015-12-01	Allan W. Antell
A shooting rest includes first and second poles each having a length, and a gun rest assembly for holding the first and second poles in selected angular relationships and at selected locations along the lengths thereof. The gun rest assembly includes a swivel connecting a first rest component mounted to the first pole for reciprocal movement along the length thereof, and a second rest component mounted to the second pole for reciprocal movement along the length thereof. A first clamp assembly is carried by the first rest component and a second clamp assembly is carried by the second rest component. The first and second clamp assemblies are configured for independently locking and releasing the respective first and second rest components relative to the respective first and second poles.
119	Apparatus and method for archery recoil stabilization	US13773186	2013-02-21	US08662064B1	2014-03-04	Charles Campbell
The invention disclosed is an apparatus and method for stabilizing an archery bow and reducing recoil during arrow draw and release. The apparatus comprises an adjustable arm clamp assembly; a rod; a support body for attaching the arm clamp assembly to the rod; and a mounting block for attaching the rod to an archery bow. The archery recoil stabilizer is lightweight, adjustable and relies on bracing the arm from the forearm position to restrict translational and rotational movement of the bow as well as minimize recoil impacts. It supports the arm by bracing the forearm relative to the bow, and reduces or eliminates bow hand torque, providing improved stabilization during both arrow draw and release. Additionally, this invention reduces the stress and recoil on the arm of the archer that can cause pain or injury, or can compromise the flight of the arrow and the accuracy of the shot.
120	Integral Powered Winged Aircraft for Infantry and Artillery Mobilization and Front Line Combat	US13118509	2011-05-30	US20120049009A1	2012-03-01	Waldemar F. Kissel, JR.
Disclosed is a Powered Wing Aircraft. A generalized stabilizer/directional vent is used for providing a standard range of aeronautical control. It controls cross winds, directional velocity, directional control, and torque balancing in one simple easy to control device. It is attached to the axles. These improvements can apply to both military and civilian applications.

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