会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 2. 发明专利
    • An improved motive mechanism for a flapping-wing aerial machine
    • GB237094A
    • 1925-07-23
    • GB1704624
    • 1924-07-16
    • JOHN DICKSON BATTEN
    • B64C33/00
    • 237,094. Batten, J. D. July 16, 1924. Ornithopters; propelling; land wheels and skid.s.-The main spars of a Rapping wing machine are assisted on the downstroke by the resilience of twisted skeins of silk hemp, steel bands or other tensile substance. The main wing spars d are connected by cords to ausiliax‹y spars c and both main and auxiliary spars are passed through crossed tubes s at the centres of the twisted skeins which are secured to the framework by similar cross-heads q and tensioning bolts. The inner ends of the spars d are connected to vertical rods f guided by pivoted links g. Crossed members h pivoted to one another at j and to the rods f at j are guided at their lower ends by rollers, k engaging the rods f. The pivots j support a saddle for the pilot who grasps hand rails m on the rods f, shoulder straps, not shown, also being connected to the rods m. The main spars are strengthened at their pivots by sheaths. The downstroke of the wings is effected by the pilot pressing his feet against a platform l on the main frame, and the upstroke is effected by allowing his weight to come on the saddle. Small wheels are carried on levers 111 which engage hooks o on the rods f as the machine alights in order to raise the wings. Main landing wheels p and a tail skid are provided. Specification 209,807 is referred to. The Provisional Specification describes a wing spar acted upon by a single twisted skein.
    • 3. 发明专利
    • An improved motive mechanism for a man-power flapping-wing aerial machine
    • GB209807A
    • 1924-01-14
    • GB2793022
    • 1922-10-14
    • JOHN DICKSON BATTEN
    • B64C33/00
    • 209,807. Batten, J. D. Oct. 14, 1922. Propelling-The downstroke of the wings of a flapping machine is effected by the pilot extending his legs with the assistance of rubber and helical springs acting on the wings to move them in the same direction, the upstroke taking place without anv muscular or mechanical assistance. The Figure shows one form of the apparatus in which wing-spars i, pivoted to the main frame at h, have stayed brackets k at their inner ends acted upon by opposed tension springs n and compression springs o. Rubber springs r also act upon the spars in the same sense. The inner ends of the springs o, n bear against a fixed plate q. A rod p passing through the compression springs o slides in slots in the ends of the brackets k. A spar s, connected to the wing spars i by rods or cables w and to the rear part of the frame by links t, is pressed down during the downstroke by the legs of the pilot, who is provided with a sling seat f and shoulder straps g secured to the frame. According to the Provisional Specification, the inner ends of the wing spars are extended inwards and are acted upon by vertical tension and compression springs placed respectively above and below the spars.