(12) Patent Application Publication (10) Pub. No.: US 2002/0035945A1 1
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US 20020035945A1 (19) United States (12) Patent Application Publication (10) Pub. No.: US 2002/0035945A1 Knowlton et al. (43) Pub. Date: Mar. 28, 2002 (54) HEAT TRANSFER INITIATOR Publication Classification (76) Inventors: Gregory D. Knowlton, Higley, AZ (51) Int. Cl." ................................ C06C 5700; CO6C 5/04 (US); Christian Salafia, Mesa, AZ (52) U.S. Cl. .......................................................... 102/275.3 (US); Bruce B. Anderson, Mountain View, CA (US); Theodore B. Gortemoller, Shalimar, FL (US) (57) ABSTRACT Correspondence Address: Alan P. Force A non-detonating heat transfer initiator. A representative Greenberg Traurig LLP heat transfer initiator is in the form of a heat transfer control medium, having a heat input portion and a heat output 21st floor portion, and a non-detonating autoignition material, having 885 Third Avenue an autoignition temperature, in thermal contact with the heat New York, NY 10022 (US) output portion. When heat is applied to the heat input (21) Appl. No.: 09/933,441 portion, a transfer of heat through the heat transfer control medium to the heat output portion results, heating the heat (22) Filed: Aug. 20, 2001 output portion, Such that, upon application of a Sufficient amount of heat to the heat input portion, the heat output Related U.S. Application Data portion is heated to the autoignition temperature of the non-detonating autoignition material, igniting the non-deto (63) Continuation-in-part of application No. 09/428,329, nating autoignition material ignites, thus producing a non filed on Oct. 27, 1999, now Pat. No. 6,298,784. detonating thermal output. 1 Patent Application Publication Mar. 28, 2002. Sheet 1 of 11 US 2002/0035945 A1 iss r r br .. 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Sheet 7 of 11 US 2002/0035945 A1 Patent Application Publication Mar. 28, 2002 Sheet 8 of 11 US 2002/0035945 A1 Fig. 9 Patent Application Publication Mar. 28, 2002. Sheet 9 of 11 US 2002/0035945 A1 Fig. 10 Patent Application Publication Mar. 28, 2002 Sheet 10 of 11 US 2002/0035945 A1 97 93 95 Patent Application Publication Mar. 28, 2002 Sheet 11 of 11 US 2002/0035945A1 US 2002/0035945 A1 Mar. 28, 2002 HEAT TRANSFER INITIATOR Sirable in many applications where the explosion and shock wave can damage equipment, or where an output of heat CROSS REFERENCE TO RELATED and/or flame is required. APPLICATIONS 0007 Similarly, U.S. Pat. No. 4,503,773 discloses a 0001. This application is a continuation-in-part of co through bulkhead initiator for use with a rocket motor. The pending U.S. application Ser. No. 09/428,329, filed Oct. 27, initiator consists of a thin metal bulkhead with a small 1999, the teaching of which is incorporated herein in its explosive charge on either side of the bulkhead. The first entirety by reference. explosive charge is detonated by a confined detonating fuse, producing a shock wave that passed through the bulkhead FIELD OF THE INVENTION without breaking the bulkhead. The shock wave then deto nates the Second explosive charge on the other Side of the 0002 The present invention is directed to heat transfer bulkhead, initiating combustion of a flame output charge. initiators for propellant, pyrotechnic, and explosive devices. In particular, the present invention is directed to initiators 0008 Pyrotechnic, electronic, and mechanical initiators that utilize heat transfer to ignite an non-detonating autoi that control the time to function of propellant, pyrotechnic, gnition material to act as a thermal Switch to reliably and and explosive devices are known as delays, and are fre precisely control the time to function of propellant, pyro quently used to control functions of munitions, Such as technic, and explosive devices, and may also be used to Self-destruct and Self-disable, and the propellant ignition reliably and precisely control the time to function of Such time of a rocket or rocket assisted projectile, where the devices. The initiators of the present invention are particu timing of the ignition of the propellant is critical in achieving larly useful as through-bulkhead initiators. maximum range. Pyrotechnic initiators that provide a delay time generally rely on the controlled burning of a pyrotech BACKGROUND OF THE INVENTION nic material, acting essentially as a fuse, Such that the length of the column of pyrotechnic material and the burning rate 0.003 Various initiators that are actuated by a pyrotech of the material determine the time of the delay. That is, the nic, electronic, or mechanical input are known in the art for delay time is the time between the ignition of the pyrotech the control of the function of propellant, pyrotechnic, and nic column and the ignition of the propellant, pyrotechnic, explosive devices. Initiators are used in a variety of appli and explosive device by the heat and/or flame output gen cations, including, but not limited to, passive vehicular erated by the combustion of the pyrotechnic column. For Safety Systems, fire Suppression Systems, rockets, and muni example, in a projectile having a range extending propellant, tions. When actuated, the initiator provides a thermal output, the initial end of a pyrotechnic delay column/ignition train typically, in the form of heat, hot gas, hot particulates, and/or is ignited as the Shell is fired. The range extending propellant flame. Actuation of a prior art initiator is typically achieved grain is then ignited by the heat and/or flame output of the electrically, or mechanically. pyrotechnic delay column/ignition train when the burning 0004. In many applications, where a reliable electrical portion of the delay column/ignition train reaches the pro actuation Signal is available, Such as in vehicular air bag pellant. The delay time is then the time between the ignition Systems, a pyrotechnic Squib may be used as an initiator. of the pyrotechnic delay column/ignition train and the Pyrotechnic Squibs such as those disclosed in U.S. Pat. No. ignition of the range extending propellant grain by the 6,168,202 to Stevens, are well known in the art. A typical output of the pyrotechnic delay column/ignition train. pyrotechnic Squib includes a pair of electrical leads, con 0009 Such pyrotechnic initiators that provide delays nected by a bridge wire, which is in thermal contact with an typically require a rapid burn rate for reliability. Slower ignition composition. Passing an electrical Signal through burning pyrotechnics are harder to ignite than fast burning the electrical leads and the bridge wire, heats the bridge pyrotechnics, and, typically, do not burn at a constant rate. wire, and ignites the ignition composition. The thermal Therefore, the delay time of Slow burning pyrotechnicS is output from the reaction or combustion of the ignition leSS reliable than faster burning pyrotechnic delays, and compound ignites a pyrotechnic material within the Squib reliable longer delay times are not easily obtained. that provides the desired thermal output used to initiate function of a main propellant, pyrotechnic, or explosive 0010 Control of the delay time of reliable, fast burning charge. Pyrotechnic Squibs will only function properly in pyrotechnic delayS is achieved by determining the burn rate applications where an electrical actuation Signal is reliably of the pyrotechnic material and the length of pyrotechnic available. material that is needed to burn for the required time. As a result, the use of pyrotechnic delays in timing munition 0005. A mechanically actuated initiator is disclosed in events is primarily limited by the Space requirements of the U.S. Pat. No. 5,913,807 to Bak. The disclosed initiator uses munition, i.e., by the length of the column that will fit in the a percussion primer, of the type used in bullets, which, when munition. Therefore, extended delay times are difficult to Struck ignites a Second charge that provides the desired achieve because of the excessive length of pyrotechnic thermal output. However, Such mechanical actuation SyS material required and/or the need for a slow burning pyro tems can be complicated and unreliable. technic material. Typical size limitations for pyrotechnic 0006 U.S. Pat. No. 3,945,322 to Carlson et al. discloses delays using burn rate and column length to control the delay a through-bulkhead initiator for causing an explosion on one are driven by a nominal lower burn rate of about 0.1 inch Side of a bulkhead by initiating an explosion on the other (2.5 mm) per Second for pyrotechnic columns having a cross Side of the bulkhead, and transmitting the Shock wave from section of about /s inch (3 mm) for columns up to about 3's the first explosion through the bulkhead. However, the use inch (9.1 mm), with cross-sections of about 4 inch (6.4 mm) of an explosion and the resulting Shockwave may be unde for longer columns.