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1. 发明申请

WO2021046533A1 ORGANIC POLYMERIC COMPOSITIONS 审中-公开
公开(公告)号：WO2021046533A1
公开(公告)日：2021-03-11
申请号：PCT/US2020/049735
申请日：2020-09-08
申请人： ARNOLD, Michael John
发明人： ARNOLD, Michael John
IPC分类号： C08G61/10 , C08F132/06 , H01G11/48
摘要： A polymer comprising recurring units derived from organic unsaturated planar ring monomers. The recurring units are stacked, linked to one another by linkers, and are capable of undergoing oxidation and/or reduction, and the polymer is electrically conducting.

2. 发明申请

WO1993006005A1 THERMAL ANTI-ICING OF AIRCRAFT STRUCTURES 审中-公开
标题翻译：飞机结构的热防护
公开(公告)号：WO1993006005A1
公开(公告)日：1993-04-01
申请号：PCT/GB1992001710
申请日：1992-09-17
申请人： SHORT BROTHERS PLC , ARNOLD, Michael, John , COLE, Derek
发明人： SHORT BROTHERS PLC
IPC分类号： B64D15/04
CPC分类号： B64D15/04 , B64D33/02 , B64D2033/0206 , B64D2033/0233 , B64D2033/0286 , F02C7/047
摘要： An aircraft structural component comprises a forward compartment (17) formed by a forward bulkhead (19) and a skin structure (21) which extends forwardly of the forward bulkhead (17) and which has an outer surface which requires to be protected from accumulation of ice thereon, and a rear compartment (18) formed between the forward bulkhead (19) and a rear bulkhead (20). A supply duct (25) extends through the rear compartment (18) and into the forward compartment (17) for the delivery thereto of pressurised hot gases for distribution over the inner surface of the skin structure (21) to prevent accumulation of ice on the outer surface of the skin structure (21). A protective shroud duct (31) surrounds the supply duct (25), extends from the rear bulkhead (20) to the forward bulkhead (19) and forms an annular space between the protective shroud duct (31) and the supply duct (25). The annular space is closed off at its rear end at the rear bulkhead (20) and throughout its length within the rear compartment (18) by the protective shroud duct (31) and is open at its forward end to provide gaseous flow communication with the forward compartment (17), whereby leakage of hot gases from the supply duct (25) upon rupture are prevented by the protective shroud duct (31) from entering into the rear compartment (18) and pass into the forward compartment (17). A discharge duct is provided for discharging spent gases from the forward compartment (17) to atmosphere.

3. 发明申请

WO1992018329A1 A STRUCTURAL COMPONENT 审中-公开
标题翻译：一个结构部件
公开(公告)号：WO1992018329A1
公开(公告)日：1992-10-29
申请号：PCT/GB1992000636
申请日：1992-04-09
申请人： SHORT BROTHERS PLC , ARNOLD, Michael, John , DOUGLAS, Charles, Euan , HAMILL, Arthur, Brian
发明人： SHORT BROTHERS PLC
IPC分类号： B32B03/12
CPC分类号： B32B3/12 , B32B5/024 , B32B5/12 , B32B7/12 , B32B15/14 , B32B15/20 , B32B2262/0269 , B32B2262/101 , B32B2262/106 , B32B2305/08 , B32B2307/202 , B32B2307/206 , B32B2311/12 , B32B2311/24 , B32B2605/18 , B64C1/06 , B64C1/068 , B64C2001/0081
摘要： A structural component exposed to lightning strikes comprises a bonded assembly of a first component part (18) which has a cellular structure and a front face (20) and a second component part (22) extending across the front face (20) of the first component part (18), the second component part (22) comprising an electrically conducting first sheet (23), an electrically non-conductive second sheet (25) at the rear of the first sheet (23) and a fibre reinforced composite third sheet (26) at the rear of the second sheet (25) and positioned between the second sheet (25) and the front face (20) of the first component part (18). In one form, the electrically conducting first sheet (23) is a non-ferrous metal or metal alloy expanded foil, the electrically non-conducting second sheet (25) is a glass fibre fabric, the third sheet (26) is a carbon or graphite fibre reinforced composite sheet and the first component part (18) is an aluminium alloy honeycomb core.

4. 发明申请

WO1993024368A1 CLOSURE DEFAULT INDICATOR 审中-公开
标题翻译：闭合默认指示灯
公开(公告)号：WO1993024368A1
公开(公告)日：1993-12-09
申请号：PCT/GB1993001032
申请日：1993-05-20
申请人： SHORT BROTHERS PLC , ARNOLD, Michael, John , JOHNSON, Kenneth, Henry , HALL, Brian, Joseph
发明人： SHORT BROTHERS PLC
IPC分类号： B64D29/06
CPC分类号： B64D29/06 , E05B41/00 , Y10S292/49 , Y10S292/65 , Y10T292/216
摘要： A structural assembly comprises first and second closure parts displaceable between a closed disposition in which they are locked by a locking mechanism and in which they close off the front side of the closure parts from the rear side and an open disposition in which they are spaced apart for access to the rear side of the closure parts and a default indicating device comprising a projection element (34) which is movable to the rear side of the closure parts where it is stowed and which releases when the closure parts move to an open disposition and moves to a projecting position in which it projects from the rear side to the front side of the closure parts to provide a visual warning that the closure parts are not in the closed disposition. The closure parts in one embodiment are fan cowl doors of an aero engine nacelle which are hinged at their upper edges to the upper part of the nacelle and which have bottom edges which move into the closed disposition at the base of the nacelle. The projecting element (34) in the projecting position then depends from the base of the nacelle.
摘要翻译：结构组件包括第一和第二闭合部件，所述第一和第二闭合部件可在闭合位置之间移动，在闭合位置中，它们被锁定机构锁定，并且其中闭合部件从后侧封闭闭合部件的前侧以及打开位置，用于进入封闭部件的后侧以及默认指示装置，该默认指示装置包括突出元件（34），所述突出元件可移动到其收起的封闭部件的后侧，并且当封闭部件移动到开放的配置时释放; 移动到突出位置，在突出位置中，其从封闭部件的后侧突出到前侧，以提供闭合部件不处于闭合位置的视觉警告。一个实施例中的封闭部件是航空发动机机舱的风扇整流罩门，其在其上边缘铰接到机舱的上部，并且具有在机舱底部移动到封闭配置中的底部边缘。突出位置的突出元件（34）然后从机舱的底部延伸。

5. 发明申请

WO1992000183A1 A COMPOSITE STRUCTURAL COMPONENT 审中-公开
标题翻译：复合结构部件
公开(公告)号：WO1992000183A1
公开(公告)日：1992-01-09
申请号：PCT/GB1991001042
申请日：1991-06-27
申请人： SHORT BROTHERS PLC , ARNOLD, Michael, John
发明人： SHORT BROTHERS PLC
IPC分类号： B29C67/14
CPC分类号： B32B3/12 , B29C70/08 , B29C70/224 , B29D24/005 , B29K2105/206 , B29K2305/00 , B32B3/266 , B32B15/08 , B32B37/146 , B32B2260/021 , B32B2260/046 , B32B2262/101 , B32B2262/106 , B32B2305/024 , B32B2307/102 , B32B2307/56 , B32B2398/20 , B64D29/00 , B64D2033/0206 , E04C2/365 , F02C7/24 , G10K11/172 , Y02T50/43 , Y02T50/672 , Y10T428/24149
摘要： PCT No. PCT/GB91/01042 Sec. 371 Date Feb. 28, 1992 Sec. 102(e) Date Feb. 28, 1992 PCT Filed Jun. 27, 1991 PCT Pub. No. WO92/00183 PCT Pub. Date Jan. 9, 1992.Fatigue, the phenomenon of structural or system failure, caused by repeated excitations from high frequency noise or vibration levels, can occur without warning in inlet cowls, fan ducts and thrust reverser translating cowls of aero engines. In modern day nacelle and fan duct design, the use composite structures predominates and a composite structural component is provided which does not suffer or does not suffer the same extent from such potential fatigue problems. The structural component has a front face for exposure to fatigue generating energy and includes a composite frontal region which includes the front face and which comprises a matrix and a high fatigue-strength metal or metal alloy mesh embodied within the matrix or partially embodied within it at the front face. The matrix is in sheet form and comprises or includes a synthetic resin.
摘要翻译： PCT No.PCT / GB91 / 01042 Sec。一九九二年二月二十八日 102（e）1992年2月28日PCT PCT 1991年6月27日PCT公布。出版物WO92 / 00183 日期：1992年1月9日。疲劳，由高频噪声或振动水平重复激发引起的结构或系统故障现象可能会在航空发动机的入口罩，风扇导管和推力反向器翻转罩中发生警告。在现代机舱和风扇风管设计中，使用复合结构占主导地位，并提供了一种复合结构部件，不会受到或不受这种潜在疲劳问题的程度的影响。结构部件具有用于暴露于疲劳产生能量的前表面，并且包括复合正面区域，其包括前表面，并且包括基体和高强度金属或金属合金网格，该金属或金属合金网格体现在基体内或部分地体现在其内前脸基质为片状，包含或包含合成树脂。

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