GB1322186A - Extendable strut assemblies - Google Patents
Extendable strut assembliesInfo
- Publication number
- GB1322186A GB1322186A GB5438970A GB1322186DA GB1322186A GB 1322186 A GB1322186 A GB 1322186A GB 5438970 A GB5438970 A GB 5438970A GB 1322186D A GB1322186D A GB 1322186DA GB 1322186 A GB1322186 A GB 1322186A
- Authority
- GB
- United Kingdom
- Prior art keywords
- keys
- keyways
- members
- extended position
- strut
- 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.)
- Expired
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G99/00—Subject matter not provided for in other groups of this subclass
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tents Or Canopies (AREA)
- Aerials With Secondary Devices (AREA)
- Photovoltaic Devices (AREA)
Abstract
1322186 Boom for artificial satellite BRITISH AIRCRAFT CORP Ltd 5 Oct 1971 [16 Nov 1970] 54389/70 Heading B7W [Also in Divisions E2 and F2] An extendable strut assembly comprises a rigid strut member 5 pivotally connected to another rigid strut member 10 for movement between a folded position, Fig. 1, and a generally coaxial extended position, Fig. 5 (not shown), with a spring biasing the struts towards the extended position, there being means for locking the members in the extended position. The connected ends of the members are formed as lugs 8, 9 pivotable on a shaft 11, one having a pair of upstanding keys (13), (14), Fig. 2 (not shown), and the other a complementary pair of keyways (16), (17), Fig. 3 (not shown). To deploy the assembly, elastic retaining cord 30 is released, and coil springs 20, 21 urge the member 10 to rotate and urge the lugs together. Following engagement of the keys in the keyways, spring-loaded plungers 26, Fig. 4, held in holes 29 in the shaft 11 are released to lock the lugs together. The keys and the surface surrounding the keyways may be covered with layers 18, 19 of an anti-friction material such as PTFE. To allow a greater angle of rotation, two keys (36), (37), Fig. 7 (not shown), of different sizes may be provided together with two matching keyways (39), (40). Strut member 5 may be pivotally mounted on a spacecraft 4, and the member 10 may carry at its other end an experimental device 31, solar cells or aerial; alternatively the assembly may comprise more than two strut members.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB5438970 | 1970-11-16 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1322186A true GB1322186A (en) | 1973-07-04 |
Family
ID=10470853
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB5438970A Expired GB1322186A (en) | 1970-11-16 | 1970-11-16 | Extendable strut assemblies |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1322186A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4030209A (en) * | 1974-03-07 | 1977-06-21 | Andre Dreiding | Molecular models |
DE3610283A1 (en) * | 1985-03-30 | 1986-10-02 | Aisin Seiki K.K., Kariya, Aichi | JOINT CONNECTION |
GB2187229A (en) * | 1986-03-01 | 1987-09-03 | Jackson Engineering | A latching mechanism |
CN113772123A (en) * | 2021-08-27 | 2021-12-10 | 哈尔滨工业大学 | Novel steering locking device |
-
1970
- 1970-11-16 GB GB5438970A patent/GB1322186A/en not_active Expired
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4030209A (en) * | 1974-03-07 | 1977-06-21 | Andre Dreiding | Molecular models |
DE3610283A1 (en) * | 1985-03-30 | 1986-10-02 | Aisin Seiki K.K., Kariya, Aichi | JOINT CONNECTION |
GB2187229A (en) * | 1986-03-01 | 1987-09-03 | Jackson Engineering | A latching mechanism |
GB2187229B (en) * | 1986-03-01 | 1989-11-15 | Jackson Engineering | Connector having a latching mechanism |
CN113772123A (en) * | 2021-08-27 | 2021-12-10 | 哈尔滨工业大学 | Novel steering locking device |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1162659A (en) | Closed Loop Supporting Structure | |
US2176461A (en) | Aircraft landing gear | |
GB1322186A (en) | Extendable strut assemblies | |
GB1127836A (en) | Satellite with adjustable solar cell surfaces | |
GB624852A (en) | Improvements in or relating to releasing devices | |
GB1344210A (en) | Model aeroplanes | |
GB2140365A (en) | Landing gear for an aircraft structure | |
GB1218037A (en) | A retractable fuselage undercarriage for an aircraft | |
GB1518575A (en) | Retracting mechanism | |
GB1094424A (en) | Antenna for space vehicle | |
GB1230627A (en) | ||
DEWEY | Problems encountered in nap of the earth flying and their effect on aircraft design mission performance(Flying safety factors in close to ground operational design of XH-51 helicopter) | |
GB829412A (en) | Improvements in aerials | |
BERNSTEIN | Satellite communication and navigation for mobile users(Satellites for mobile aircraft and ship communications) | |
LICHTEN | Parameters of oh-4 a light helicopter, based on the concepts of minimum cost, acceptable mission capability, and high reliability | |
DAWSON et al. | Theoretical analysis of swing-pad bearings with small imperfections[Interim Report, Jan. 1976- Dec. 1977] | |
GB592591A (en) | Improvements in locking devices | |
KINDT et al. | The design of the ranger television system to obtain high-resolution photographs of the lunar surface(Ranger television system design to obtain high resolution lunar surface photographs including ground recovery and flight systems) | |
NANEVICZ et al. | Precipitation static interference on aircraft in the Mach 1 to Mach 4 speed range(All-weather aircraft operating in Mach 1 to Mach 4 range studied for radio interference generation, noting charge imparted to aircraft decreases with increasing speed) | |
BARRETT | On the application of electric propulsion to satellite orbit adjustment and station keeping(Satellite orbit adjustment, stationkeeping and attitude control of typical earth- and sun- synchronous satellites by electric propulsion systems) | |
BECKER | Spacelab environmental control system development as demonstrated in in-flight configuration | |
FAULDERS et al. | The effect of aerodynamic characteristics on the flare and landing of low L/D glide vehicles(Flare and landing performance of glide vehicles with low lift-drag ratio, noting aerodynamic characteristics effect) | |
Rosenbach | Engineering aspects with satellite communication terminals in aircraft | |
HARRIS et al. | Spectrometer observations in the region near the bow shock on March 12, 1968(Directed proton fluxes measurements in bow shock, magnetosheath and solar wind by OGO 5 satellite ion spectrometer) | |
SCHULZ et al. | The influence of ground effects on the secondary forces on a VTOL aircraft during hovering and transitional flight(Ground effects influence on VTOL aircraft secondary forces during hovering and transitional flight, discussing component dynamic coefficients in wind tunnel) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |